fractalloadingmodelofthejointinterfaceconsideringstrain ...nep2 kh×1.4988a −0.1021 nec a 1.1021...
TRANSCRIPT
Research ArticleFractal Loading Model of the Joint Interface Considering StrainHardening of Materials
Yanhui Wang 12 Xueliang Zhang 1 Shuhua Wen1 and Yonghui Chen1
1School of Mechanical Engineering Taiyuan University of Science and Technology Taiyuan 030024 China2Department of Mechanical and Electrical Engineering Shanxi Institute of Energy Jinzhong 030600 China
Correspondence should be addressed to Xueliang Zhang zhang_xue_lsinacom
Received 2 August 2018 Revised 7 December 2018 Accepted 6 February 2019 Published 3 March 2019
Academic Editor Fabio Minghini
Copyright copy 2019 YanhuiWang et alis is an open access article distributed under the Creative Commons Attribution Licensewhich permits unrestricted use distribution and reproduction in any medium provided the original work is properly cited
Based on fractal geometry theory the deformation state of the four stages of the asperity elastic first elastoplastic secondelastoplastic and fully plastic deformation and comprehensively considering the hardness of the asperity changes with the amountof deformation in elastoplastic deformation stage due to strain hardening are considered thereby establishing a single-loadingmodel of the joint interface By introducing the pushing coefficient and the asperity frequency exponent each critical frequencyexponents of asperity is obtained and the relationship between the normal contact load and the contact area of the firstelastoplastic deformation phase and the second elastoplastic deformation phase of the single asperity in the case of taking intoaccount the change in hardness is inferred eventually deducing the relationship between the total contact load of the jointinterface and the contact area e analysis results show that in the elastoplastic deformation stage when the deformation isconstant the asperity load considering the hardness change is smaller than the unconsidered load and the difference increaseswith the increase of the deformation amount e establishment of the model provides a theoretical basis for further research onthe elastoplastic contact of joint interfaces
1 Introduction
e joint formed by assembly of mechanical parts is calledthe joint interface which plays an important role in thetransmission of motion load and energy in the normaloperation of mechanical system e joint interface presentsa series of different curvature radius and the height asperitiesat the microscopic scale e contact between the jointinterface is discontinuous and only occurs at higher asperitylead to the real contact area accounts for only a small part ofthe nominal contact area resulting in the situation of largeload on a small contact area As a result researches on theproperties of interfacial contact and stress analysis are verycomplex [1] erefore to study the deformation behaviorand the accurate modeling of joint interface is an importantissue for in-depth understanding of the mechanism offriction wear lubrication heat conduction etc
Statistical and fractal contact models for solving contactproblems on joint interface have been used widely in this
field Statistical contact model was originally put forward byGreenwood and Williamson (GW model) and improved bymany subsequent researchers [2ndash4] Zhao et al deduced anew elastoplastic contact model of joint interface whichdescribing a long transition period from elastic deformationto fully plastic deformation of joint interface It is shown thatthe elastoplastic contact of the asperity plays an importantrole in the microscopic contact behavior of the joint in-terface [5] Kogut and Etsion established the contact modelbetween a single asperity and a rigid flat by means of finiteelement analysis and obtained the relationship betweencontact area and contact load of a single asperity duringloading and unloading [6 7] Kadin et al applied theconclusion of Etsion to the whole joint interface and got astatistical model of single loading and unloading of jointinterface According to his conclusion plastic deformationand residual stress may occur in the process of loading andunloading e actual contact area of the asperity duringunloading is larger than the actual contact area of the loading
HindawiAdvances in Materials Science and EngineeringVolume 2019 Article ID 2108162 14 pageshttpsdoiorg10115520192108162
process [8 9] However the value of statistical parametersdepends largely on the filter or resolution of the roughnessmeasuring instrument so it is not unique for a jointinterface
e fractal model was first proposed by Majumdar andBhushan (MB model) in 1990 e model holds that thedeformation of microconvex body changes from plasticdeformation to elastic deformation with the increase ofload contrary to the traditional contact study [10ndash12]Many scholars put forward many kinds of fractal modelsbased on MB fractal model and obtained more accuratecontact mechanical properties of joint interface Wang et almodified the area distribution density function of asperityin MB model and obtained the modified model of MBelastic and plastic contact [13 14] Morag and Etsionestablished the elastoplastic contact fractal model of asingle asperity and explained the contradiction between thedeformation sequence of asperity from plastic deformationto elastic deformation in MB model and the classical Hertzcontact theory [15] Tian et al modified the model furthertaking into account the change of material hardness withthe change of surface depth in elastoplastic stage andestablished a new single-loading model of joint interfaceHowever the model only takes into account the transitionfrom elastic to elastoplastic and elastoplastic to fully plasticdeformation stage of the asperity e description of theelastoplastic deformation stage is seldom involved in themodel [16] Yuan et al proposed an improved model of thefractal elastoplastic contact model of rough surface basedon the MB model so as to deduce a model of the totalcontact load and the total actual contact area [17] How-ever the model does not take into account the strainhardening phenomenon of the joint interface material thatis the hardness of the material is no longer a constantvalue but will change with the increase of the amount ofdeformation Hardness is an important index to charac-terize the mechanical properties of materials such aselasticity plasticity strength and toughness e change ofhardness value is directly related to the accuracy of cal-culation According to the strain hardening criterion theaverage hardness increases with the increase of de-formation e degree of plastic deformation increases thedegree of work hardening and dislocation strengtheningincreases and the hardness of the material increases Basedon the above research results and fractal theory a newhardness change function is expected to be constructed inthis paper considering that the hardness of the materialchanges with the deformation amount of the asperity in theelastoplastic deformation stage In this paper the criticalconditions of elastic elastoplastic and plastic deformationof asperity are studied and the four deformation ranges arerevised and a fractal theoretical model describing the singleloading of the joint interface is proposed It is expected thatthe microscopic and macroscopic contact state of thesurface of the interface can be more scientifically andreasonably described in order to provide some theoreticalbasis for the research of contact friction wear and lu-brication on the surface of mechanical parts
2 Fractal Model of a Single Asperity
Majumdar et al show that the contours of joint interfacetopography in practical engineering have fractal charac-teristics mathematical characteristics are continuity non-differentiability and self-affinity [10 11] e joint interfaceprofile can be described by theWeierstrassndashMandelbrot (W-M) function which is expressed as
Z(x) G(Dminus1)
1113944
infin
nnmin
cos 2πcnx( 1113857
c(2minusD)n (1ltDlt 2 cgt 1) (1)
where x is the horizontal coordinate of the profile functionof the joint interface and the corresponding function valueis the height of the profile D is the fractal dimension of thesurface profile (for a physically continuous surface1ltDlt 2) G is the length scale parameter of the surfacewhich reflects the amplitude of Z(x) and is the measure-ment constant nmin is the lowest frequency exponent cor-responding to the profile and cn determines the spectrum ofsurface roughness which is the frequency density controlparameter cgt 1 e actual surface profile has an unstablerandomness [18] and its lowest frequency is related to thesample length which is given by cnmin 1L In order tosatisfy the requirements for high spectral density and forphase randomization c 15
21 Elastic Deformation of a Single Asperity On the mi-croscopic scale the contact between the two joint interfacesis essentially a contact between the asperity and the asperitywhich can be simplified as a contact between a series ofequivalent asperities on the joint interface and a rigid flatsurface Assuming that the joint interface is isotropic thereis no interaction between the asperity and the asperityduring the contact process and no large deformation willoccur e equation before deformation of the asperity withfrequency exponent n is obtained as follows
zn(x) GDminus1cos πcnx( 1113857
c(2minusD)nminus
12cnltxlt
12cn
1113888 1113889 (2)
Figure 1 shows an asperity in equivalent joint interfacecontacts with a rigid flat surface e height of the asperity ishn the interference of the asperity is ωn during the loadingprocess and the size of the substrate of the asperity is lnAccording to equation (2) the curvature radius of an as-perity with frequency exponent n at any point x is obtainedas follows
ρn(x) 1 + dzn(x)dx1113858 1113859
21113966 1113967
32
d2zn(x)dx2
11138681113868111386811138681113868111386811138681113868111386811138681113868
11138681113868111386811138681113868111386811138681113868111386811138681113868
1 + π2G2(Dminus1)c2(1minusD)n( 1113857sin2 πcnx( 11138571113960 1113961
32
minus π2GDminus1cminusDn( 1113857cos πcnx( 11138571113868111386811138681113868
1113868111386811138681113868
(3)
When x 0 the curvature radius of asperity isminimum
2 Advances in Materials Science and Engineering
ρnmin(x) Rn cminusn D
π2GDminus1(4)
e height before deformation of the asperity is
hn zn(0) GDminus1
c(2minusD)n (5)
In the loading process of asperity the deformation willincrease with the increase of normal contact load Accordinglyasperity will change from elastic deformation to elastoplasticdeformation and then to fully plastic deformation
e elastic critical interference of asperity at initial yieldis [16]
ωnec 3πKH
4Eprime1113874 1113875
2R (6)
where K 0454 + 041υ υ is the Poisson ratio of the softermaterial H is the hardness of the softer material H 28Yand Eprime is the equivalent elastic modulus (1Eprime)
(1minus υ1primeE1) + (1minus υ2primeE2) E1 and E2 are respectively elasticmodulus of two objects in contact with each other υ1prime and υ2primeare respectively the corresponding Poisson ratios
When ωn ltωnec an lt anec the asperity is in a state ofelastic deformation According to Hertz theory the contactarea of the asperity is
an πRωn (7)
Substituting equation (6) in equation (7) the criticalcontact area of the elastic asperity is
anec πRωnec π3πKH
4Eprime1113874 1113875
2R2
1π
3KHcminusn D
4G(Dminus1)Eprime1113888 1113889
2
(8)
According to the Hertz contact theory the normal loadon a single asperity is
fne 43EprimeR12
n ω32n (9)
Substituting equations (4) and (7) in equation (9) we canobtain
fne 4Eprimea32
n π12GDminus1
3cminusDn (10)
According to equations (6) (8) and (9) we can get thecritical contact load of the elastic asperity
fnec K middot H middot anec (11)
22 Elastic-Plastic Deformation of a Single AsperityLiterature [6] through the finite element analysis of a singleasperity it is concluded that when the asperity actual de-formation is greater than the elastic critical interference(ωn gtωnec) the yield phenomenon begins to appear and theelastoplastic deformation of the asperity occurs Accordingto the results of [6] the elastoplastic deformation of asperitycan be divided into two different stages according to theratio ωnωnec namely the first elastoplastic deformationstage when 1ltωnωnec le 6 and the second elastoplasticdeformation stage when 6ltωnωnec le 110 Define ωnepc
6ωnec as the first elastoplastic critical interference where theactual contact area is anepc e actual deformation of as-perity ωnpc 110ωnec is defined as the second elastoplasticcritical interference and the actual contact area is anpc erelationship between contact area-deformation and contactload-deformation in the elastoplastic deformation stage ofasperity is [6]
an
anec 093
ωn
ωnec1113888 1113889
1136
fnep1
fnec 103
ωn
ωnec1113888 1113889
1425
ωnec ltωn le 6ωnec( 1113857
an
anec 094
ωn
ωnec1113888 1113889
1146
fnep2
fnec 140
ωn
ωnec1113888 1113889
1263
6ωnec ltωn le 110ωnec( 1113857
(12)
From the above equations we can get
X
ln
h n
w n
O
Z
Figure 1 Diagram of single asperity loading
Advances in Materials Science and Engineering 3
anepc 71197anec
fnep1 KH times 11282aminus02544nec a
12544n anec lt an lt anepc1113872 1113873
(13)
anpc 2053827anec
fnep2 KH times 14988aminus01021nec a
11021n anepc lt an lt anpc1113872 1113873
(14)
where fnec is contact load for ω ωnec and fnep1 and fnep2are contact loads in the first elastoplastic stage and thesecond elastoplastic stage respectively Both fnep1 and fnep2obtained above are related to the hardness (H) of thematerial However according to the plastic strengtheningprinciple the hardness is not a constant when the materialyields but a function related to the deformation that is itchanges with the deformation erefore it is not accurateto describe elastoplastic deformation by the above formulaIn order to express the characteristics of elastoplastic de-formation more accurately the concept of limit meangeometric hardness is introduced
According to equations (13) and (14) HG(a) is fittedinto the following segmented relations
e first elastoplastic deformation stage is
HG1 an( 1113857 c1Yan
anec1113888 1113889
c2
anec lt an le anepc1113872 1113873 (15)
e second elastoplastic deformation stage is
HG2 an( 1113857 c3Yan
anec1113888 1113889
c4
anepc lt an le anpc1113872 1113873 (16)
where c1 c2 c3 and c4 are the coefficients to be solved
(1) Equation (15) should satisfy two limiting conditions
HG1 anec( 1113857 pea anec( 1113857 (17)
HG1 anepc1113872 1113873 pepa1 anepc1113872 1113873 (18)
where pea(a) is the average contact pressure of theasperity in elastic stage which is given bypea(a) (fnea) pepa1(a) is the average contactpressure of the asperity in the first elastoplastic de-formation stage and is given by pepa1(a) (fnep1a)Substituting equations (11) and (15) in equation (17)we can obtain
c1Y KH (19)
c1 28K (20)
Substituting equations (13) and (15) in equation (18)we can obtain
KH times 11282aminus02544nec times 71197anec( 1113857
02544 28KY times 71197c2
(21)
Derived from equation (21)
c2 ln 11282 times 7119702544( 1113857
ln 71197 (22)
Considering the change of hardness the normal con-tact load of a single asperity in the first elastoplasticstage is
fnep1prime HG1(a) middot an (23)
Substituting equations (15) (20) and (22) in equation(23) new equations are yielded
fnep1prime 28KYaminusc2neca
c2+1n (24)
(2) Equation (16) should satisfy two limiting conditions
HG2 anepc1113872 1113873 pepa1 anepc1113872 1113873 (25)
HG2 anpc1113872 1113873 pepa2 anpc1113872 1113873 (26)
where pepa2(a) (fnep2a) is the average contactpressure of the asperity in the second elastoplastic stageSubstituting equations (13) and (16) in equation (25)we can obtain
c3(71197)c4 K times 28 times 11282 times(71197)
02544 (27)
Substituting equations (14) and (16) in equation (26)we can obtain
c3(2053827)c4 K times 28 times 14988 times(2053827)
01021
(28)
Simultaneous equations (27) and (28) obtained
c4 ln 11282 + 02544 ln 71197minus ln 14988minus 01021 ln 2053827
ln 71197minus ln 2053827
(29)
Substituting equation (29) in equation (27) we canobtain
c3 K times 315896 times(71197)02544minusc4 (30)
Considering the change of hardness the normal con-tact load of a single asperity in the second elastoplasticstage is
fnep2prime HG2(a) middot an K times 315896 times(71197)02544minusc4Y
middot aminusc4nec middot a
c4+1n
(31)
23 Full Plastic Deformation of a Single Asperity As thedeformation continues to increase when ωn gt 110ωnec thecontact area an gt anpc and the asperity enters the stage of fullplastic deformation At this stage the hardness of the ma-terial is no longer affected by the deformation and can beregarded as a constant When the hardness of the material is
4 Advances in Materials Science and Engineering
given according to literature [7] the contact load andcontact area of the asperity at this stage can be expressed as
fnp Han
an 2πRnωn(32)
In conclusion with the increase of load and deformationthe contact area of the same asperity increases graduallyie anec lt anepc lt anpc With the increase of the load andcontact area the asperity underwent elastic deformationfirst elastoplastic deformation second elastoplastic de-formation and full plastic deformation successively Underconstant load and deformation the actual contact area of theasperity is related to the radius of curvature at the vertex ofthe asperity
24 Asperityrsquos Frequency Exponent n When using W-Mfunction to describe the surface profile of an asperity theprofile function is related to the asperityrsquos frequency ex-ponent In other words the radius of curvature at the vertexof the asperity and the height of the asperity vary with thefrequency exponent when the load is constant According tothe equations (5)ndash(7) it was found that the value of hn Rnand ωnec correlated with the frequency exponent When thefrequency exponent is constant the deformation of theasperity is not greater than the height of the asperityunder the action of the load In order to obtain the criticalvalue of the frequency exponent we take hn ωnec ie(GDminus1c(2minusD)nec) (3KH4Eprime)2 middot (cminusnecDGDminus1)
e elastic critical frequency exponent can be obtainedas follows
nec intln 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (33)
where int is the integer part of the value in the parenthesisSimilarly the first elastoplastic critical frequency expo-
nent can be obtained
nepc intln 6 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (34)
e second elastoplastic critical frequency exponent canbe obtained
npc intln 110 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (35)
From the above when the asperity frequency exponent isnmin lt nle nec elastic deformation only takes place in theseasperities under contact load When nec lt nle nepc elasticdeformation or the first elastoplastic deformation can takeplace in these asperities When nepc lt nle npc elastic de-formation the first elastoplastic deformation or the secondelastoplastic deformation can take place in these asperities and
full plastic deformation never occur When npc lt nle nmaxelastic deformation elastoplastic deformation or full plasticdeformation can take place in these asperities
3 Actual Contact Area and Normal ContactLoad of Joint Interface
According to reference [10] when the asperity frequencyexponent is n the area distribution density function of theasperity on the joint interface is defined as
nn(a) 12
D middotaD2nl
a(D+2)2 0lt ale anl 1ltDlt 2( 1113857 (36)
where anl represents the largest contact area when theasperityrsquos frequency exponent is n
In order to simplify equation (36) we define the areadistribution function of the asperity of any frequency ex-ponent as nn(a) Mn(a) According to reference [17] theactual contact area of joint interface is
Ar 1113944
nmax
nnmin
1113946anl
0nn(a)a da M 1113944
nmax
nnmin
1113946anl
0n(a)a da (37)
where M (al1113936nmaxnnmin
anl)(nmin le nle nmax al max anl1113864 1113865)
31 When the Frequency Exponent Belongs to nmin lt nle necWhen the frequency exponent belongs to nmin lt nle nec evenif these asperities are completely deformed only elasticdeformation will occur and anl lt anec In this case the actualcontact area of the joint interface is defined as Ar1
Ar1 1113944
nec
nnmin
1113946anl
0Mn(a)ada
MD
2minusD1113944
nec
nnmin
anl (38)
In this case the contact load of the joint interface is asfollows
Fr1 1113944
nec
nnmin
1113946anl
0fneMn(a)da (39)
Substituting equation (11) in equation (39) we canobtain
Fr1 MD
3minusD1113944
nec
nnmin
4Eπ12G(Dminus1)
3cminusDna32nl (40)
32 When the Frequency Exponent Belongs to nec lt nle nepcWhen the frequency exponent belongs to nec lt nle nepc forthe case anec lt anl le anepc elastic deformation or the firstelastoplastic deformation may take place in these asperitiesAt this point the actual contact area of the joint interfaceconsists of two parts the elastic deformation stage and thefirst elastoplastic deformation stage
Advances in Materials Science and Engineering 5
Ar2 Are + Arep1 (41)
Are 1113944
nepc
nnec+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nepc
nnec+1a
(2minusD)2nec a
D2nl
(42)
For the determined frequency exponent the maximumactual contact area of the asperity appears at the maximumdeformation amount ωn where the maximum value of theelastic deformation phase ωn appears at ωnec whereuponformula (42) is simplified to
Are MD
2minusD1113944
nepc
nnec+1anec
MD
(2minusD)π1113944
nepc
nnec+1
3KHcminusDn
4G(Dminus 1)Eprime1113888 1113889
2
Arep1 1113944
nepc
nnec+11113946
anl
anec
Mn(a)ada MD
2minusD
middot 1113944
nepc
nnec+1a
(2minusD)2nl minus a
(2minusD)2nec1113960 1113961a
D2nl
(43)
e contact load is given by
Fr2 Fre + Frep1 (44)
Fre 1113944
nepc
nnec+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572
middot 1113944
nepc
nnec+1cminus2 Dn
(45)
Frep1 1113944
nepc
nnec+11113946
anl
anec
fnep1prime Mn(a)da (46)
Substituting equations (24) and (36) in equation (46) wecan obtain
Frep1 28KYMD
2c2 minusD + 21113944
nepc
nnec+1aminusc2neca
c2+1nl minus a
(2minusD)2nec a
D2nl1113960 1113961 (47)
33 When the Frequency Exponent Belongs to nepc lt nle npcWhen the frequency exponent belongs to nepc lt nle npc forthe case anepc lt anl le anpc elastic deformation the firstelastoplastic deformation or the second elastoplastic de-formation may take place in these asperities At this point
the actual contact area of the joint interface consists ofthree parts the elastic deformation stage the first elas-toplastic deformation stage and the second elastoplasticdeformation stage
Ar3 Are + Arep1 + Arep2
Are 1113944
npc
nnepc+11113946
anec
0Mn(a)ada
MD
(2minusD)π
middot 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep1 1113944
npc
nnepc+11113946
anepc
anec
Mn(a)ada
MD
π(2minusD)71197minus 71197D2
1113872 1113873 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep2 1113944
npc
nnepc+11113946
anl
anepc
Mn(a)ada
MD
(2minusD)1113944
npc
nnepc+1a
(2minusD)2nl minus 71197anec( 1113857
(2minusD)21113960 1113961a
D2nl
(48)
In this case the contact load of the joint interface is asfollows
Fr3 Fre + Frep1 + Frep2
Fre 1113944
npc
nnepc+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572 1113944
npc
nnepc+1cminus2 Dn
Frep1 28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873
middot 1113944
npc
nnepc+1
1π
3KHcminusDn
4GDminus 1Eprime1113888 1113889
2
(49)
When the second elastoplastic deformation occurs thenormal contact load of the joint interface is as follows
6 Advances in Materials Science and Engineering
Frep2 1113944
npc
nnepc+11113946
anl
anepc
fnep2prime Mn(a)da (50)
Substituting equations (31) and (38) in equation (46) wecan obtain
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
npc
nnepc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
(D2)nl1113872 1113873
(51)
34 When the Frequency Exponent Belongs to npc lt nWhen the frequency exponent belongs to npc lt n elasticdeformation elastoplastic deformation or full plastic de-formation may take place in these asperities e actualcontact area of the joint interface can be evaluated as
Ar4 Are + Arep1 + Arep2 + Arp
Are 1113944
nmax
nnpc+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1anec
Arep1 1113944
nmax
nnpc+11113946
anepc
anec
Mn(a)ada
MD
2minusD71197minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Arep2 1113944
nmax
nnpc+11113946
anpc
anepc
Mn(a)ada
MD
2minusD2053827minus 711971minus(D2)
middot 2053827D21113872 1113873 1113944
nmax
nnpc+1anec
Arp 1113944
nmax
nnpc+11113946
anl
anpc
Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1a
(2minusD)2nl minus 2053827anec( 1113857
(2minusD)21113960 1113961a
D2nl
(52)
In this case the contact load of the joint interface is asfollows
Fr4 Fre + Frep1 + Frep2 + Frp
Fre 1113944
nmax
nnpc+11113946
anec
0fneMn(a)da
MDKH
(3minusD)π1113944
nmax
nnpc+1anec
Frep1 1113944
nmax
nnpc+11113946
anepc
anec
fnep1prime Mn(a)da
28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
nmax
nnpc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
D2nl1113872 1113873
2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 2053827c4+1 minus 2053827D2middot 71197c4minus(D2)+1
1113872 1113873
middot 1113944
nmax
nnpc+1anec
Frp 1113944
nmax
nnpc+11113946
anl
anpc
fnpMn(a)da
MHD
2minusD1113944
nmax
nnpc+1a
D2nl a
1minus(D2)nl minus 2053827anec( 1113857
1minus(D2)1113960 1113961
(53)
For all frequency exponents the total actual contact areaof the joint interface is
Ar Ar1 + Ar2 + Ar3 + Ar4 (54)
e total contact load of the joint interface is
Fr Fr1 + Fr2 + Fr3 + Fr4 (55)
e total real contact area and the total contact load in anondimensional form can be written as follows
Alowastr
Ar
Aa
Flowastr
Fr
AaE
(56)
where Aa is the nominal contact area and is given byAa L2L 1cnmin
Advances in Materials Science and Engineering 7
4 Results Analysis
In order to further analyze the above calculation results theparameters of equivalent joint interface are taken as shownin Table 1 [16]
Figure 2 shows the relation between all critical contactareas and frequency exponents of single asperity whenD 15 It can be seen from the figure that as for one definiteasperity when frequency exponent n is certain elastic criticalcontact area is minimum followed by the first elastoplasticcritical contact area and the second elastoplastic criticalcontact area is maximum With gradual increase of contactload the contact area increases e single asperity is firstlysubject to elastic deformation followed by the first elasto-plastic deformation the second elastoplastic deformation andfully plastic deformation successively which is consistent withtypical contact mechanics theory As for different asperitieswith increase of frequency exponent all critical contact areasdecrease correspondingly which shows that elastic criticalcontact area the first elastoplastic critical contact area and thesecond elastoplastic critical contact area are all related tofrequency exponent n
Figure 3 shows the relation curve between fractal di-mension D and critical frequency exponent n of asperityWhen fractal dimension is definite elastic critical frequencyexponent nec the first elastoplastic critical frequency ex-ponent nepc and the second elastoplastic critical frequencyexponent npc increase gradually As shown in Figure 3 whenDlt 106 nec nepc and npc are all negative As for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation and fully plasticdeformation will all occur When D 113 nec and nepc arenegative and npc is positive At this time as for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation will occur exceptfully plastic deformation
For D 15 G 25 times 10minus9 m H 55 times 109 Nm2 wecan obtain the elastic critical frequency exponent nec 32the first elastoplastic critical frequency exponent nepc 36and the second elastoplastic critical frequency exponentnpc 43 ese asperities whose frequency exponents rangefrom 20 to 32 are only under elastic deformation Elasticdeformation and the first elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 33 to 36 Elastic deformation the first elastoplasticdeformation and the second elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 37 to 43 When frequency exponents range from 43 to50 all deformations types can occur in these asperities
Figure 4 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the first elastoplastic stage ecomparison diagram is simulation result when n 33 It canbe seen from the figure that with gradual increase of contactarea with contact area of single asperity over 32 times 10minus13 m2contact load of the same asperity with hardness change willbe less than that without hardness change In addition as theamount of deformation increases the difference betweenthem tends to increase
Figure 5 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the second elastoplastic stagee comparison diagram is simulation result when n 37 Itcan be seen from the figure that when the deformation is
Table 1 e parameters of equivalent joint interface
Parameters ValuesEquivalent elastic modulus Eprime 72 times 1010 Nm2
Poissonrsquos ratio υ 017Initial hardness H 55 times 109 Nm2
Profile scale parameter G 25 times 10minus9 mFractal dimension D 1ltDlt 2Frequency exponent n 20sim50
20 25 30 35 40 45 5010ndash1510ndash1410ndash1310ndash1210ndash1110ndash1010ndash910ndash810ndash710ndash610ndash510ndash410ndash3
Criti
cal c
onta
ct ar
eas
of a
singl
e asp
erity
(am
2 )
Asperity levels (n)
Second elastoplastic critical contact areaFirst elastoplastic critical contact areaElastic critical contact area
Figure 2 e relationship between critical contact area and fre-quency exponent of a single asperity
10 11 12 13 14 15 16 17 18 19 20ndash140
ndash120
ndash100
ndash80
ndash60
ndash40
ndash20
0
20
40
Asp
erity
freq
uenc
y ex
pone
nts (n)
e fractal dimension (D)
Elastic critical frequency exponentsFirst elastoplastic critical frequency exponentsSecond elastoplastic critical frequency exponents
Figure 3 e relationship between fractal dimension D andcritical frequency exponent n of a single asperity
8 Advances in Materials Science and Engineering
definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
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Submit your manuscripts atwwwhindawicom
process [8 9] However the value of statistical parametersdepends largely on the filter or resolution of the roughnessmeasuring instrument so it is not unique for a jointinterface
e fractal model was first proposed by Majumdar andBhushan (MB model) in 1990 e model holds that thedeformation of microconvex body changes from plasticdeformation to elastic deformation with the increase ofload contrary to the traditional contact study [10ndash12]Many scholars put forward many kinds of fractal modelsbased on MB fractal model and obtained more accuratecontact mechanical properties of joint interface Wang et almodified the area distribution density function of asperityin MB model and obtained the modified model of MBelastic and plastic contact [13 14] Morag and Etsionestablished the elastoplastic contact fractal model of asingle asperity and explained the contradiction between thedeformation sequence of asperity from plastic deformationto elastic deformation in MB model and the classical Hertzcontact theory [15] Tian et al modified the model furthertaking into account the change of material hardness withthe change of surface depth in elastoplastic stage andestablished a new single-loading model of joint interfaceHowever the model only takes into account the transitionfrom elastic to elastoplastic and elastoplastic to fully plasticdeformation stage of the asperity e description of theelastoplastic deformation stage is seldom involved in themodel [16] Yuan et al proposed an improved model of thefractal elastoplastic contact model of rough surface basedon the MB model so as to deduce a model of the totalcontact load and the total actual contact area [17] How-ever the model does not take into account the strainhardening phenomenon of the joint interface material thatis the hardness of the material is no longer a constantvalue but will change with the increase of the amount ofdeformation Hardness is an important index to charac-terize the mechanical properties of materials such aselasticity plasticity strength and toughness e change ofhardness value is directly related to the accuracy of cal-culation According to the strain hardening criterion theaverage hardness increases with the increase of de-formation e degree of plastic deformation increases thedegree of work hardening and dislocation strengtheningincreases and the hardness of the material increases Basedon the above research results and fractal theory a newhardness change function is expected to be constructed inthis paper considering that the hardness of the materialchanges with the deformation amount of the asperity in theelastoplastic deformation stage In this paper the criticalconditions of elastic elastoplastic and plastic deformationof asperity are studied and the four deformation ranges arerevised and a fractal theoretical model describing the singleloading of the joint interface is proposed It is expected thatthe microscopic and macroscopic contact state of thesurface of the interface can be more scientifically andreasonably described in order to provide some theoreticalbasis for the research of contact friction wear and lu-brication on the surface of mechanical parts
2 Fractal Model of a Single Asperity
Majumdar et al show that the contours of joint interfacetopography in practical engineering have fractal charac-teristics mathematical characteristics are continuity non-differentiability and self-affinity [10 11] e joint interfaceprofile can be described by theWeierstrassndashMandelbrot (W-M) function which is expressed as
Z(x) G(Dminus1)
1113944
infin
nnmin
cos 2πcnx( 1113857
c(2minusD)n (1ltDlt 2 cgt 1) (1)
where x is the horizontal coordinate of the profile functionof the joint interface and the corresponding function valueis the height of the profile D is the fractal dimension of thesurface profile (for a physically continuous surface1ltDlt 2) G is the length scale parameter of the surfacewhich reflects the amplitude of Z(x) and is the measure-ment constant nmin is the lowest frequency exponent cor-responding to the profile and cn determines the spectrum ofsurface roughness which is the frequency density controlparameter cgt 1 e actual surface profile has an unstablerandomness [18] and its lowest frequency is related to thesample length which is given by cnmin 1L In order tosatisfy the requirements for high spectral density and forphase randomization c 15
21 Elastic Deformation of a Single Asperity On the mi-croscopic scale the contact between the two joint interfacesis essentially a contact between the asperity and the asperitywhich can be simplified as a contact between a series ofequivalent asperities on the joint interface and a rigid flatsurface Assuming that the joint interface is isotropic thereis no interaction between the asperity and the asperityduring the contact process and no large deformation willoccur e equation before deformation of the asperity withfrequency exponent n is obtained as follows
zn(x) GDminus1cos πcnx( 1113857
c(2minusD)nminus
12cnltxlt
12cn
1113888 1113889 (2)
Figure 1 shows an asperity in equivalent joint interfacecontacts with a rigid flat surface e height of the asperity ishn the interference of the asperity is ωn during the loadingprocess and the size of the substrate of the asperity is lnAccording to equation (2) the curvature radius of an as-perity with frequency exponent n at any point x is obtainedas follows
ρn(x) 1 + dzn(x)dx1113858 1113859
21113966 1113967
32
d2zn(x)dx2
11138681113868111386811138681113868111386811138681113868111386811138681113868
11138681113868111386811138681113868111386811138681113868111386811138681113868
1 + π2G2(Dminus1)c2(1minusD)n( 1113857sin2 πcnx( 11138571113960 1113961
32
minus π2GDminus1cminusDn( 1113857cos πcnx( 11138571113868111386811138681113868
1113868111386811138681113868
(3)
When x 0 the curvature radius of asperity isminimum
2 Advances in Materials Science and Engineering
ρnmin(x) Rn cminusn D
π2GDminus1(4)
e height before deformation of the asperity is
hn zn(0) GDminus1
c(2minusD)n (5)
In the loading process of asperity the deformation willincrease with the increase of normal contact load Accordinglyasperity will change from elastic deformation to elastoplasticdeformation and then to fully plastic deformation
e elastic critical interference of asperity at initial yieldis [16]
ωnec 3πKH
4Eprime1113874 1113875
2R (6)
where K 0454 + 041υ υ is the Poisson ratio of the softermaterial H is the hardness of the softer material H 28Yand Eprime is the equivalent elastic modulus (1Eprime)
(1minus υ1primeE1) + (1minus υ2primeE2) E1 and E2 are respectively elasticmodulus of two objects in contact with each other υ1prime and υ2primeare respectively the corresponding Poisson ratios
When ωn ltωnec an lt anec the asperity is in a state ofelastic deformation According to Hertz theory the contactarea of the asperity is
an πRωn (7)
Substituting equation (6) in equation (7) the criticalcontact area of the elastic asperity is
anec πRωnec π3πKH
4Eprime1113874 1113875
2R2
1π
3KHcminusn D
4G(Dminus1)Eprime1113888 1113889
2
(8)
According to the Hertz contact theory the normal loadon a single asperity is
fne 43EprimeR12
n ω32n (9)
Substituting equations (4) and (7) in equation (9) we canobtain
fne 4Eprimea32
n π12GDminus1
3cminusDn (10)
According to equations (6) (8) and (9) we can get thecritical contact load of the elastic asperity
fnec K middot H middot anec (11)
22 Elastic-Plastic Deformation of a Single AsperityLiterature [6] through the finite element analysis of a singleasperity it is concluded that when the asperity actual de-formation is greater than the elastic critical interference(ωn gtωnec) the yield phenomenon begins to appear and theelastoplastic deformation of the asperity occurs Accordingto the results of [6] the elastoplastic deformation of asperitycan be divided into two different stages according to theratio ωnωnec namely the first elastoplastic deformationstage when 1ltωnωnec le 6 and the second elastoplasticdeformation stage when 6ltωnωnec le 110 Define ωnepc
6ωnec as the first elastoplastic critical interference where theactual contact area is anepc e actual deformation of as-perity ωnpc 110ωnec is defined as the second elastoplasticcritical interference and the actual contact area is anpc erelationship between contact area-deformation and contactload-deformation in the elastoplastic deformation stage ofasperity is [6]
an
anec 093
ωn
ωnec1113888 1113889
1136
fnep1
fnec 103
ωn
ωnec1113888 1113889
1425
ωnec ltωn le 6ωnec( 1113857
an
anec 094
ωn
ωnec1113888 1113889
1146
fnep2
fnec 140
ωn
ωnec1113888 1113889
1263
6ωnec ltωn le 110ωnec( 1113857
(12)
From the above equations we can get
X
ln
h n
w n
O
Z
Figure 1 Diagram of single asperity loading
Advances in Materials Science and Engineering 3
anepc 71197anec
fnep1 KH times 11282aminus02544nec a
12544n anec lt an lt anepc1113872 1113873
(13)
anpc 2053827anec
fnep2 KH times 14988aminus01021nec a
11021n anepc lt an lt anpc1113872 1113873
(14)
where fnec is contact load for ω ωnec and fnep1 and fnep2are contact loads in the first elastoplastic stage and thesecond elastoplastic stage respectively Both fnep1 and fnep2obtained above are related to the hardness (H) of thematerial However according to the plastic strengtheningprinciple the hardness is not a constant when the materialyields but a function related to the deformation that is itchanges with the deformation erefore it is not accurateto describe elastoplastic deformation by the above formulaIn order to express the characteristics of elastoplastic de-formation more accurately the concept of limit meangeometric hardness is introduced
According to equations (13) and (14) HG(a) is fittedinto the following segmented relations
e first elastoplastic deformation stage is
HG1 an( 1113857 c1Yan
anec1113888 1113889
c2
anec lt an le anepc1113872 1113873 (15)
e second elastoplastic deformation stage is
HG2 an( 1113857 c3Yan
anec1113888 1113889
c4
anepc lt an le anpc1113872 1113873 (16)
where c1 c2 c3 and c4 are the coefficients to be solved
(1) Equation (15) should satisfy two limiting conditions
HG1 anec( 1113857 pea anec( 1113857 (17)
HG1 anepc1113872 1113873 pepa1 anepc1113872 1113873 (18)
where pea(a) is the average contact pressure of theasperity in elastic stage which is given bypea(a) (fnea) pepa1(a) is the average contactpressure of the asperity in the first elastoplastic de-formation stage and is given by pepa1(a) (fnep1a)Substituting equations (11) and (15) in equation (17)we can obtain
c1Y KH (19)
c1 28K (20)
Substituting equations (13) and (15) in equation (18)we can obtain
KH times 11282aminus02544nec times 71197anec( 1113857
02544 28KY times 71197c2
(21)
Derived from equation (21)
c2 ln 11282 times 7119702544( 1113857
ln 71197 (22)
Considering the change of hardness the normal con-tact load of a single asperity in the first elastoplasticstage is
fnep1prime HG1(a) middot an (23)
Substituting equations (15) (20) and (22) in equation(23) new equations are yielded
fnep1prime 28KYaminusc2neca
c2+1n (24)
(2) Equation (16) should satisfy two limiting conditions
HG2 anepc1113872 1113873 pepa1 anepc1113872 1113873 (25)
HG2 anpc1113872 1113873 pepa2 anpc1113872 1113873 (26)
where pepa2(a) (fnep2a) is the average contactpressure of the asperity in the second elastoplastic stageSubstituting equations (13) and (16) in equation (25)we can obtain
c3(71197)c4 K times 28 times 11282 times(71197)
02544 (27)
Substituting equations (14) and (16) in equation (26)we can obtain
c3(2053827)c4 K times 28 times 14988 times(2053827)
01021
(28)
Simultaneous equations (27) and (28) obtained
c4 ln 11282 + 02544 ln 71197minus ln 14988minus 01021 ln 2053827
ln 71197minus ln 2053827
(29)
Substituting equation (29) in equation (27) we canobtain
c3 K times 315896 times(71197)02544minusc4 (30)
Considering the change of hardness the normal con-tact load of a single asperity in the second elastoplasticstage is
fnep2prime HG2(a) middot an K times 315896 times(71197)02544minusc4Y
middot aminusc4nec middot a
c4+1n
(31)
23 Full Plastic Deformation of a Single Asperity As thedeformation continues to increase when ωn gt 110ωnec thecontact area an gt anpc and the asperity enters the stage of fullplastic deformation At this stage the hardness of the ma-terial is no longer affected by the deformation and can beregarded as a constant When the hardness of the material is
4 Advances in Materials Science and Engineering
given according to literature [7] the contact load andcontact area of the asperity at this stage can be expressed as
fnp Han
an 2πRnωn(32)
In conclusion with the increase of load and deformationthe contact area of the same asperity increases graduallyie anec lt anepc lt anpc With the increase of the load andcontact area the asperity underwent elastic deformationfirst elastoplastic deformation second elastoplastic de-formation and full plastic deformation successively Underconstant load and deformation the actual contact area of theasperity is related to the radius of curvature at the vertex ofthe asperity
24 Asperityrsquos Frequency Exponent n When using W-Mfunction to describe the surface profile of an asperity theprofile function is related to the asperityrsquos frequency ex-ponent In other words the radius of curvature at the vertexof the asperity and the height of the asperity vary with thefrequency exponent when the load is constant According tothe equations (5)ndash(7) it was found that the value of hn Rnand ωnec correlated with the frequency exponent When thefrequency exponent is constant the deformation of theasperity is not greater than the height of the asperityunder the action of the load In order to obtain the criticalvalue of the frequency exponent we take hn ωnec ie(GDminus1c(2minusD)nec) (3KH4Eprime)2 middot (cminusnecDGDminus1)
e elastic critical frequency exponent can be obtainedas follows
nec intln 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (33)
where int is the integer part of the value in the parenthesisSimilarly the first elastoplastic critical frequency expo-
nent can be obtained
nepc intln 6 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (34)
e second elastoplastic critical frequency exponent canbe obtained
npc intln 110 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (35)
From the above when the asperity frequency exponent isnmin lt nle nec elastic deformation only takes place in theseasperities under contact load When nec lt nle nepc elasticdeformation or the first elastoplastic deformation can takeplace in these asperities When nepc lt nle npc elastic de-formation the first elastoplastic deformation or the secondelastoplastic deformation can take place in these asperities and
full plastic deformation never occur When npc lt nle nmaxelastic deformation elastoplastic deformation or full plasticdeformation can take place in these asperities
3 Actual Contact Area and Normal ContactLoad of Joint Interface
According to reference [10] when the asperity frequencyexponent is n the area distribution density function of theasperity on the joint interface is defined as
nn(a) 12
D middotaD2nl
a(D+2)2 0lt ale anl 1ltDlt 2( 1113857 (36)
where anl represents the largest contact area when theasperityrsquos frequency exponent is n
In order to simplify equation (36) we define the areadistribution function of the asperity of any frequency ex-ponent as nn(a) Mn(a) According to reference [17] theactual contact area of joint interface is
Ar 1113944
nmax
nnmin
1113946anl
0nn(a)a da M 1113944
nmax
nnmin
1113946anl
0n(a)a da (37)
where M (al1113936nmaxnnmin
anl)(nmin le nle nmax al max anl1113864 1113865)
31 When the Frequency Exponent Belongs to nmin lt nle necWhen the frequency exponent belongs to nmin lt nle nec evenif these asperities are completely deformed only elasticdeformation will occur and anl lt anec In this case the actualcontact area of the joint interface is defined as Ar1
Ar1 1113944
nec
nnmin
1113946anl
0Mn(a)ada
MD
2minusD1113944
nec
nnmin
anl (38)
In this case the contact load of the joint interface is asfollows
Fr1 1113944
nec
nnmin
1113946anl
0fneMn(a)da (39)
Substituting equation (11) in equation (39) we canobtain
Fr1 MD
3minusD1113944
nec
nnmin
4Eπ12G(Dminus1)
3cminusDna32nl (40)
32 When the Frequency Exponent Belongs to nec lt nle nepcWhen the frequency exponent belongs to nec lt nle nepc forthe case anec lt anl le anepc elastic deformation or the firstelastoplastic deformation may take place in these asperitiesAt this point the actual contact area of the joint interfaceconsists of two parts the elastic deformation stage and thefirst elastoplastic deformation stage
Advances in Materials Science and Engineering 5
Ar2 Are + Arep1 (41)
Are 1113944
nepc
nnec+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nepc
nnec+1a
(2minusD)2nec a
D2nl
(42)
For the determined frequency exponent the maximumactual contact area of the asperity appears at the maximumdeformation amount ωn where the maximum value of theelastic deformation phase ωn appears at ωnec whereuponformula (42) is simplified to
Are MD
2minusD1113944
nepc
nnec+1anec
MD
(2minusD)π1113944
nepc
nnec+1
3KHcminusDn
4G(Dminus 1)Eprime1113888 1113889
2
Arep1 1113944
nepc
nnec+11113946
anl
anec
Mn(a)ada MD
2minusD
middot 1113944
nepc
nnec+1a
(2minusD)2nl minus a
(2minusD)2nec1113960 1113961a
D2nl
(43)
e contact load is given by
Fr2 Fre + Frep1 (44)
Fre 1113944
nepc
nnec+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572
middot 1113944
nepc
nnec+1cminus2 Dn
(45)
Frep1 1113944
nepc
nnec+11113946
anl
anec
fnep1prime Mn(a)da (46)
Substituting equations (24) and (36) in equation (46) wecan obtain
Frep1 28KYMD
2c2 minusD + 21113944
nepc
nnec+1aminusc2neca
c2+1nl minus a
(2minusD)2nec a
D2nl1113960 1113961 (47)
33 When the Frequency Exponent Belongs to nepc lt nle npcWhen the frequency exponent belongs to nepc lt nle npc forthe case anepc lt anl le anpc elastic deformation the firstelastoplastic deformation or the second elastoplastic de-formation may take place in these asperities At this point
the actual contact area of the joint interface consists ofthree parts the elastic deformation stage the first elas-toplastic deformation stage and the second elastoplasticdeformation stage
Ar3 Are + Arep1 + Arep2
Are 1113944
npc
nnepc+11113946
anec
0Mn(a)ada
MD
(2minusD)π
middot 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep1 1113944
npc
nnepc+11113946
anepc
anec
Mn(a)ada
MD
π(2minusD)71197minus 71197D2
1113872 1113873 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep2 1113944
npc
nnepc+11113946
anl
anepc
Mn(a)ada
MD
(2minusD)1113944
npc
nnepc+1a
(2minusD)2nl minus 71197anec( 1113857
(2minusD)21113960 1113961a
D2nl
(48)
In this case the contact load of the joint interface is asfollows
Fr3 Fre + Frep1 + Frep2
Fre 1113944
npc
nnepc+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572 1113944
npc
nnepc+1cminus2 Dn
Frep1 28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873
middot 1113944
npc
nnepc+1
1π
3KHcminusDn
4GDminus 1Eprime1113888 1113889
2
(49)
When the second elastoplastic deformation occurs thenormal contact load of the joint interface is as follows
6 Advances in Materials Science and Engineering
Frep2 1113944
npc
nnepc+11113946
anl
anepc
fnep2prime Mn(a)da (50)
Substituting equations (31) and (38) in equation (46) wecan obtain
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
npc
nnepc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
(D2)nl1113872 1113873
(51)
34 When the Frequency Exponent Belongs to npc lt nWhen the frequency exponent belongs to npc lt n elasticdeformation elastoplastic deformation or full plastic de-formation may take place in these asperities e actualcontact area of the joint interface can be evaluated as
Ar4 Are + Arep1 + Arep2 + Arp
Are 1113944
nmax
nnpc+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1anec
Arep1 1113944
nmax
nnpc+11113946
anepc
anec
Mn(a)ada
MD
2minusD71197minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Arep2 1113944
nmax
nnpc+11113946
anpc
anepc
Mn(a)ada
MD
2minusD2053827minus 711971minus(D2)
middot 2053827D21113872 1113873 1113944
nmax
nnpc+1anec
Arp 1113944
nmax
nnpc+11113946
anl
anpc
Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1a
(2minusD)2nl minus 2053827anec( 1113857
(2minusD)21113960 1113961a
D2nl
(52)
In this case the contact load of the joint interface is asfollows
Fr4 Fre + Frep1 + Frep2 + Frp
Fre 1113944
nmax
nnpc+11113946
anec
0fneMn(a)da
MDKH
(3minusD)π1113944
nmax
nnpc+1anec
Frep1 1113944
nmax
nnpc+11113946
anepc
anec
fnep1prime Mn(a)da
28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
nmax
nnpc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
D2nl1113872 1113873
2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 2053827c4+1 minus 2053827D2middot 71197c4minus(D2)+1
1113872 1113873
middot 1113944
nmax
nnpc+1anec
Frp 1113944
nmax
nnpc+11113946
anl
anpc
fnpMn(a)da
MHD
2minusD1113944
nmax
nnpc+1a
D2nl a
1minus(D2)nl minus 2053827anec( 1113857
1minus(D2)1113960 1113961
(53)
For all frequency exponents the total actual contact areaof the joint interface is
Ar Ar1 + Ar2 + Ar3 + Ar4 (54)
e total contact load of the joint interface is
Fr Fr1 + Fr2 + Fr3 + Fr4 (55)
e total real contact area and the total contact load in anondimensional form can be written as follows
Alowastr
Ar
Aa
Flowastr
Fr
AaE
(56)
where Aa is the nominal contact area and is given byAa L2L 1cnmin
Advances in Materials Science and Engineering 7
4 Results Analysis
In order to further analyze the above calculation results theparameters of equivalent joint interface are taken as shownin Table 1 [16]
Figure 2 shows the relation between all critical contactareas and frequency exponents of single asperity whenD 15 It can be seen from the figure that as for one definiteasperity when frequency exponent n is certain elastic criticalcontact area is minimum followed by the first elastoplasticcritical contact area and the second elastoplastic criticalcontact area is maximum With gradual increase of contactload the contact area increases e single asperity is firstlysubject to elastic deformation followed by the first elasto-plastic deformation the second elastoplastic deformation andfully plastic deformation successively which is consistent withtypical contact mechanics theory As for different asperitieswith increase of frequency exponent all critical contact areasdecrease correspondingly which shows that elastic criticalcontact area the first elastoplastic critical contact area and thesecond elastoplastic critical contact area are all related tofrequency exponent n
Figure 3 shows the relation curve between fractal di-mension D and critical frequency exponent n of asperityWhen fractal dimension is definite elastic critical frequencyexponent nec the first elastoplastic critical frequency ex-ponent nepc and the second elastoplastic critical frequencyexponent npc increase gradually As shown in Figure 3 whenDlt 106 nec nepc and npc are all negative As for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation and fully plasticdeformation will all occur When D 113 nec and nepc arenegative and npc is positive At this time as for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation will occur exceptfully plastic deformation
For D 15 G 25 times 10minus9 m H 55 times 109 Nm2 wecan obtain the elastic critical frequency exponent nec 32the first elastoplastic critical frequency exponent nepc 36and the second elastoplastic critical frequency exponentnpc 43 ese asperities whose frequency exponents rangefrom 20 to 32 are only under elastic deformation Elasticdeformation and the first elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 33 to 36 Elastic deformation the first elastoplasticdeformation and the second elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 37 to 43 When frequency exponents range from 43 to50 all deformations types can occur in these asperities
Figure 4 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the first elastoplastic stage ecomparison diagram is simulation result when n 33 It canbe seen from the figure that with gradual increase of contactarea with contact area of single asperity over 32 times 10minus13 m2contact load of the same asperity with hardness change willbe less than that without hardness change In addition as theamount of deformation increases the difference betweenthem tends to increase
Figure 5 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the second elastoplastic stagee comparison diagram is simulation result when n 37 Itcan be seen from the figure that when the deformation is
Table 1 e parameters of equivalent joint interface
Parameters ValuesEquivalent elastic modulus Eprime 72 times 1010 Nm2
Poissonrsquos ratio υ 017Initial hardness H 55 times 109 Nm2
Profile scale parameter G 25 times 10minus9 mFractal dimension D 1ltDlt 2Frequency exponent n 20sim50
20 25 30 35 40 45 5010ndash1510ndash1410ndash1310ndash1210ndash1110ndash1010ndash910ndash810ndash710ndash610ndash510ndash410ndash3
Criti
cal c
onta
ct ar
eas
of a
singl
e asp
erity
(am
2 )
Asperity levels (n)
Second elastoplastic critical contact areaFirst elastoplastic critical contact areaElastic critical contact area
Figure 2 e relationship between critical contact area and fre-quency exponent of a single asperity
10 11 12 13 14 15 16 17 18 19 20ndash140
ndash120
ndash100
ndash80
ndash60
ndash40
ndash20
0
20
40
Asp
erity
freq
uenc
y ex
pone
nts (n)
e fractal dimension (D)
Elastic critical frequency exponentsFirst elastoplastic critical frequency exponentsSecond elastoplastic critical frequency exponents
Figure 3 e relationship between fractal dimension D andcritical frequency exponent n of a single asperity
8 Advances in Materials Science and Engineering
definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
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ρnmin(x) Rn cminusn D
π2GDminus1(4)
e height before deformation of the asperity is
hn zn(0) GDminus1
c(2minusD)n (5)
In the loading process of asperity the deformation willincrease with the increase of normal contact load Accordinglyasperity will change from elastic deformation to elastoplasticdeformation and then to fully plastic deformation
e elastic critical interference of asperity at initial yieldis [16]
ωnec 3πKH
4Eprime1113874 1113875
2R (6)
where K 0454 + 041υ υ is the Poisson ratio of the softermaterial H is the hardness of the softer material H 28Yand Eprime is the equivalent elastic modulus (1Eprime)
(1minus υ1primeE1) + (1minus υ2primeE2) E1 and E2 are respectively elasticmodulus of two objects in contact with each other υ1prime and υ2primeare respectively the corresponding Poisson ratios
When ωn ltωnec an lt anec the asperity is in a state ofelastic deformation According to Hertz theory the contactarea of the asperity is
an πRωn (7)
Substituting equation (6) in equation (7) the criticalcontact area of the elastic asperity is
anec πRωnec π3πKH
4Eprime1113874 1113875
2R2
1π
3KHcminusn D
4G(Dminus1)Eprime1113888 1113889
2
(8)
According to the Hertz contact theory the normal loadon a single asperity is
fne 43EprimeR12
n ω32n (9)
Substituting equations (4) and (7) in equation (9) we canobtain
fne 4Eprimea32
n π12GDminus1
3cminusDn (10)
According to equations (6) (8) and (9) we can get thecritical contact load of the elastic asperity
fnec K middot H middot anec (11)
22 Elastic-Plastic Deformation of a Single AsperityLiterature [6] through the finite element analysis of a singleasperity it is concluded that when the asperity actual de-formation is greater than the elastic critical interference(ωn gtωnec) the yield phenomenon begins to appear and theelastoplastic deformation of the asperity occurs Accordingto the results of [6] the elastoplastic deformation of asperitycan be divided into two different stages according to theratio ωnωnec namely the first elastoplastic deformationstage when 1ltωnωnec le 6 and the second elastoplasticdeformation stage when 6ltωnωnec le 110 Define ωnepc
6ωnec as the first elastoplastic critical interference where theactual contact area is anepc e actual deformation of as-perity ωnpc 110ωnec is defined as the second elastoplasticcritical interference and the actual contact area is anpc erelationship between contact area-deformation and contactload-deformation in the elastoplastic deformation stage ofasperity is [6]
an
anec 093
ωn
ωnec1113888 1113889
1136
fnep1
fnec 103
ωn
ωnec1113888 1113889
1425
ωnec ltωn le 6ωnec( 1113857
an
anec 094
ωn
ωnec1113888 1113889
1146
fnep2
fnec 140
ωn
ωnec1113888 1113889
1263
6ωnec ltωn le 110ωnec( 1113857
(12)
From the above equations we can get
X
ln
h n
w n
O
Z
Figure 1 Diagram of single asperity loading
Advances in Materials Science and Engineering 3
anepc 71197anec
fnep1 KH times 11282aminus02544nec a
12544n anec lt an lt anepc1113872 1113873
(13)
anpc 2053827anec
fnep2 KH times 14988aminus01021nec a
11021n anepc lt an lt anpc1113872 1113873
(14)
where fnec is contact load for ω ωnec and fnep1 and fnep2are contact loads in the first elastoplastic stage and thesecond elastoplastic stage respectively Both fnep1 and fnep2obtained above are related to the hardness (H) of thematerial However according to the plastic strengtheningprinciple the hardness is not a constant when the materialyields but a function related to the deformation that is itchanges with the deformation erefore it is not accurateto describe elastoplastic deformation by the above formulaIn order to express the characteristics of elastoplastic de-formation more accurately the concept of limit meangeometric hardness is introduced
According to equations (13) and (14) HG(a) is fittedinto the following segmented relations
e first elastoplastic deformation stage is
HG1 an( 1113857 c1Yan
anec1113888 1113889
c2
anec lt an le anepc1113872 1113873 (15)
e second elastoplastic deformation stage is
HG2 an( 1113857 c3Yan
anec1113888 1113889
c4
anepc lt an le anpc1113872 1113873 (16)
where c1 c2 c3 and c4 are the coefficients to be solved
(1) Equation (15) should satisfy two limiting conditions
HG1 anec( 1113857 pea anec( 1113857 (17)
HG1 anepc1113872 1113873 pepa1 anepc1113872 1113873 (18)
where pea(a) is the average contact pressure of theasperity in elastic stage which is given bypea(a) (fnea) pepa1(a) is the average contactpressure of the asperity in the first elastoplastic de-formation stage and is given by pepa1(a) (fnep1a)Substituting equations (11) and (15) in equation (17)we can obtain
c1Y KH (19)
c1 28K (20)
Substituting equations (13) and (15) in equation (18)we can obtain
KH times 11282aminus02544nec times 71197anec( 1113857
02544 28KY times 71197c2
(21)
Derived from equation (21)
c2 ln 11282 times 7119702544( 1113857
ln 71197 (22)
Considering the change of hardness the normal con-tact load of a single asperity in the first elastoplasticstage is
fnep1prime HG1(a) middot an (23)
Substituting equations (15) (20) and (22) in equation(23) new equations are yielded
fnep1prime 28KYaminusc2neca
c2+1n (24)
(2) Equation (16) should satisfy two limiting conditions
HG2 anepc1113872 1113873 pepa1 anepc1113872 1113873 (25)
HG2 anpc1113872 1113873 pepa2 anpc1113872 1113873 (26)
where pepa2(a) (fnep2a) is the average contactpressure of the asperity in the second elastoplastic stageSubstituting equations (13) and (16) in equation (25)we can obtain
c3(71197)c4 K times 28 times 11282 times(71197)
02544 (27)
Substituting equations (14) and (16) in equation (26)we can obtain
c3(2053827)c4 K times 28 times 14988 times(2053827)
01021
(28)
Simultaneous equations (27) and (28) obtained
c4 ln 11282 + 02544 ln 71197minus ln 14988minus 01021 ln 2053827
ln 71197minus ln 2053827
(29)
Substituting equation (29) in equation (27) we canobtain
c3 K times 315896 times(71197)02544minusc4 (30)
Considering the change of hardness the normal con-tact load of a single asperity in the second elastoplasticstage is
fnep2prime HG2(a) middot an K times 315896 times(71197)02544minusc4Y
middot aminusc4nec middot a
c4+1n
(31)
23 Full Plastic Deformation of a Single Asperity As thedeformation continues to increase when ωn gt 110ωnec thecontact area an gt anpc and the asperity enters the stage of fullplastic deformation At this stage the hardness of the ma-terial is no longer affected by the deformation and can beregarded as a constant When the hardness of the material is
4 Advances in Materials Science and Engineering
given according to literature [7] the contact load andcontact area of the asperity at this stage can be expressed as
fnp Han
an 2πRnωn(32)
In conclusion with the increase of load and deformationthe contact area of the same asperity increases graduallyie anec lt anepc lt anpc With the increase of the load andcontact area the asperity underwent elastic deformationfirst elastoplastic deformation second elastoplastic de-formation and full plastic deformation successively Underconstant load and deformation the actual contact area of theasperity is related to the radius of curvature at the vertex ofthe asperity
24 Asperityrsquos Frequency Exponent n When using W-Mfunction to describe the surface profile of an asperity theprofile function is related to the asperityrsquos frequency ex-ponent In other words the radius of curvature at the vertexof the asperity and the height of the asperity vary with thefrequency exponent when the load is constant According tothe equations (5)ndash(7) it was found that the value of hn Rnand ωnec correlated with the frequency exponent When thefrequency exponent is constant the deformation of theasperity is not greater than the height of the asperityunder the action of the load In order to obtain the criticalvalue of the frequency exponent we take hn ωnec ie(GDminus1c(2minusD)nec) (3KH4Eprime)2 middot (cminusnecDGDminus1)
e elastic critical frequency exponent can be obtainedas follows
nec intln 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (33)
where int is the integer part of the value in the parenthesisSimilarly the first elastoplastic critical frequency expo-
nent can be obtained
nepc intln 6 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (34)
e second elastoplastic critical frequency exponent canbe obtained
npc intln 110 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (35)
From the above when the asperity frequency exponent isnmin lt nle nec elastic deformation only takes place in theseasperities under contact load When nec lt nle nepc elasticdeformation or the first elastoplastic deformation can takeplace in these asperities When nepc lt nle npc elastic de-formation the first elastoplastic deformation or the secondelastoplastic deformation can take place in these asperities and
full plastic deformation never occur When npc lt nle nmaxelastic deformation elastoplastic deformation or full plasticdeformation can take place in these asperities
3 Actual Contact Area and Normal ContactLoad of Joint Interface
According to reference [10] when the asperity frequencyexponent is n the area distribution density function of theasperity on the joint interface is defined as
nn(a) 12
D middotaD2nl
a(D+2)2 0lt ale anl 1ltDlt 2( 1113857 (36)
where anl represents the largest contact area when theasperityrsquos frequency exponent is n
In order to simplify equation (36) we define the areadistribution function of the asperity of any frequency ex-ponent as nn(a) Mn(a) According to reference [17] theactual contact area of joint interface is
Ar 1113944
nmax
nnmin
1113946anl
0nn(a)a da M 1113944
nmax
nnmin
1113946anl
0n(a)a da (37)
where M (al1113936nmaxnnmin
anl)(nmin le nle nmax al max anl1113864 1113865)
31 When the Frequency Exponent Belongs to nmin lt nle necWhen the frequency exponent belongs to nmin lt nle nec evenif these asperities are completely deformed only elasticdeformation will occur and anl lt anec In this case the actualcontact area of the joint interface is defined as Ar1
Ar1 1113944
nec
nnmin
1113946anl
0Mn(a)ada
MD
2minusD1113944
nec
nnmin
anl (38)
In this case the contact load of the joint interface is asfollows
Fr1 1113944
nec
nnmin
1113946anl
0fneMn(a)da (39)
Substituting equation (11) in equation (39) we canobtain
Fr1 MD
3minusD1113944
nec
nnmin
4Eπ12G(Dminus1)
3cminusDna32nl (40)
32 When the Frequency Exponent Belongs to nec lt nle nepcWhen the frequency exponent belongs to nec lt nle nepc forthe case anec lt anl le anepc elastic deformation or the firstelastoplastic deformation may take place in these asperitiesAt this point the actual contact area of the joint interfaceconsists of two parts the elastic deformation stage and thefirst elastoplastic deformation stage
Advances in Materials Science and Engineering 5
Ar2 Are + Arep1 (41)
Are 1113944
nepc
nnec+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nepc
nnec+1a
(2minusD)2nec a
D2nl
(42)
For the determined frequency exponent the maximumactual contact area of the asperity appears at the maximumdeformation amount ωn where the maximum value of theelastic deformation phase ωn appears at ωnec whereuponformula (42) is simplified to
Are MD
2minusD1113944
nepc
nnec+1anec
MD
(2minusD)π1113944
nepc
nnec+1
3KHcminusDn
4G(Dminus 1)Eprime1113888 1113889
2
Arep1 1113944
nepc
nnec+11113946
anl
anec
Mn(a)ada MD
2minusD
middot 1113944
nepc
nnec+1a
(2minusD)2nl minus a
(2minusD)2nec1113960 1113961a
D2nl
(43)
e contact load is given by
Fr2 Fre + Frep1 (44)
Fre 1113944
nepc
nnec+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572
middot 1113944
nepc
nnec+1cminus2 Dn
(45)
Frep1 1113944
nepc
nnec+11113946
anl
anec
fnep1prime Mn(a)da (46)
Substituting equations (24) and (36) in equation (46) wecan obtain
Frep1 28KYMD
2c2 minusD + 21113944
nepc
nnec+1aminusc2neca
c2+1nl minus a
(2minusD)2nec a
D2nl1113960 1113961 (47)
33 When the Frequency Exponent Belongs to nepc lt nle npcWhen the frequency exponent belongs to nepc lt nle npc forthe case anepc lt anl le anpc elastic deformation the firstelastoplastic deformation or the second elastoplastic de-formation may take place in these asperities At this point
the actual contact area of the joint interface consists ofthree parts the elastic deformation stage the first elas-toplastic deformation stage and the second elastoplasticdeformation stage
Ar3 Are + Arep1 + Arep2
Are 1113944
npc
nnepc+11113946
anec
0Mn(a)ada
MD
(2minusD)π
middot 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep1 1113944
npc
nnepc+11113946
anepc
anec
Mn(a)ada
MD
π(2minusD)71197minus 71197D2
1113872 1113873 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep2 1113944
npc
nnepc+11113946
anl
anepc
Mn(a)ada
MD
(2minusD)1113944
npc
nnepc+1a
(2minusD)2nl minus 71197anec( 1113857
(2minusD)21113960 1113961a
D2nl
(48)
In this case the contact load of the joint interface is asfollows
Fr3 Fre + Frep1 + Frep2
Fre 1113944
npc
nnepc+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572 1113944
npc
nnepc+1cminus2 Dn
Frep1 28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873
middot 1113944
npc
nnepc+1
1π
3KHcminusDn
4GDminus 1Eprime1113888 1113889
2
(49)
When the second elastoplastic deformation occurs thenormal contact load of the joint interface is as follows
6 Advances in Materials Science and Engineering
Frep2 1113944
npc
nnepc+11113946
anl
anepc
fnep2prime Mn(a)da (50)
Substituting equations (31) and (38) in equation (46) wecan obtain
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
npc
nnepc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
(D2)nl1113872 1113873
(51)
34 When the Frequency Exponent Belongs to npc lt nWhen the frequency exponent belongs to npc lt n elasticdeformation elastoplastic deformation or full plastic de-formation may take place in these asperities e actualcontact area of the joint interface can be evaluated as
Ar4 Are + Arep1 + Arep2 + Arp
Are 1113944
nmax
nnpc+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1anec
Arep1 1113944
nmax
nnpc+11113946
anepc
anec
Mn(a)ada
MD
2minusD71197minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Arep2 1113944
nmax
nnpc+11113946
anpc
anepc
Mn(a)ada
MD
2minusD2053827minus 711971minus(D2)
middot 2053827D21113872 1113873 1113944
nmax
nnpc+1anec
Arp 1113944
nmax
nnpc+11113946
anl
anpc
Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1a
(2minusD)2nl minus 2053827anec( 1113857
(2minusD)21113960 1113961a
D2nl
(52)
In this case the contact load of the joint interface is asfollows
Fr4 Fre + Frep1 + Frep2 + Frp
Fre 1113944
nmax
nnpc+11113946
anec
0fneMn(a)da
MDKH
(3minusD)π1113944
nmax
nnpc+1anec
Frep1 1113944
nmax
nnpc+11113946
anepc
anec
fnep1prime Mn(a)da
28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
nmax
nnpc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
D2nl1113872 1113873
2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 2053827c4+1 minus 2053827D2middot 71197c4minus(D2)+1
1113872 1113873
middot 1113944
nmax
nnpc+1anec
Frp 1113944
nmax
nnpc+11113946
anl
anpc
fnpMn(a)da
MHD
2minusD1113944
nmax
nnpc+1a
D2nl a
1minus(D2)nl minus 2053827anec( 1113857
1minus(D2)1113960 1113961
(53)
For all frequency exponents the total actual contact areaof the joint interface is
Ar Ar1 + Ar2 + Ar3 + Ar4 (54)
e total contact load of the joint interface is
Fr Fr1 + Fr2 + Fr3 + Fr4 (55)
e total real contact area and the total contact load in anondimensional form can be written as follows
Alowastr
Ar
Aa
Flowastr
Fr
AaE
(56)
where Aa is the nominal contact area and is given byAa L2L 1cnmin
Advances in Materials Science and Engineering 7
4 Results Analysis
In order to further analyze the above calculation results theparameters of equivalent joint interface are taken as shownin Table 1 [16]
Figure 2 shows the relation between all critical contactareas and frequency exponents of single asperity whenD 15 It can be seen from the figure that as for one definiteasperity when frequency exponent n is certain elastic criticalcontact area is minimum followed by the first elastoplasticcritical contact area and the second elastoplastic criticalcontact area is maximum With gradual increase of contactload the contact area increases e single asperity is firstlysubject to elastic deformation followed by the first elasto-plastic deformation the second elastoplastic deformation andfully plastic deformation successively which is consistent withtypical contact mechanics theory As for different asperitieswith increase of frequency exponent all critical contact areasdecrease correspondingly which shows that elastic criticalcontact area the first elastoplastic critical contact area and thesecond elastoplastic critical contact area are all related tofrequency exponent n
Figure 3 shows the relation curve between fractal di-mension D and critical frequency exponent n of asperityWhen fractal dimension is definite elastic critical frequencyexponent nec the first elastoplastic critical frequency ex-ponent nepc and the second elastoplastic critical frequencyexponent npc increase gradually As shown in Figure 3 whenDlt 106 nec nepc and npc are all negative As for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation and fully plasticdeformation will all occur When D 113 nec and nepc arenegative and npc is positive At this time as for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation will occur exceptfully plastic deformation
For D 15 G 25 times 10minus9 m H 55 times 109 Nm2 wecan obtain the elastic critical frequency exponent nec 32the first elastoplastic critical frequency exponent nepc 36and the second elastoplastic critical frequency exponentnpc 43 ese asperities whose frequency exponents rangefrom 20 to 32 are only under elastic deformation Elasticdeformation and the first elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 33 to 36 Elastic deformation the first elastoplasticdeformation and the second elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 37 to 43 When frequency exponents range from 43 to50 all deformations types can occur in these asperities
Figure 4 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the first elastoplastic stage ecomparison diagram is simulation result when n 33 It canbe seen from the figure that with gradual increase of contactarea with contact area of single asperity over 32 times 10minus13 m2contact load of the same asperity with hardness change willbe less than that without hardness change In addition as theamount of deformation increases the difference betweenthem tends to increase
Figure 5 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the second elastoplastic stagee comparison diagram is simulation result when n 37 Itcan be seen from the figure that when the deformation is
Table 1 e parameters of equivalent joint interface
Parameters ValuesEquivalent elastic modulus Eprime 72 times 1010 Nm2
Poissonrsquos ratio υ 017Initial hardness H 55 times 109 Nm2
Profile scale parameter G 25 times 10minus9 mFractal dimension D 1ltDlt 2Frequency exponent n 20sim50
20 25 30 35 40 45 5010ndash1510ndash1410ndash1310ndash1210ndash1110ndash1010ndash910ndash810ndash710ndash610ndash510ndash410ndash3
Criti
cal c
onta
ct ar
eas
of a
singl
e asp
erity
(am
2 )
Asperity levels (n)
Second elastoplastic critical contact areaFirst elastoplastic critical contact areaElastic critical contact area
Figure 2 e relationship between critical contact area and fre-quency exponent of a single asperity
10 11 12 13 14 15 16 17 18 19 20ndash140
ndash120
ndash100
ndash80
ndash60
ndash40
ndash20
0
20
40
Asp
erity
freq
uenc
y ex
pone
nts (n)
e fractal dimension (D)
Elastic critical frequency exponentsFirst elastoplastic critical frequency exponentsSecond elastoplastic critical frequency exponents
Figure 3 e relationship between fractal dimension D andcritical frequency exponent n of a single asperity
8 Advances in Materials Science and Engineering
definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
CorrosionInternational Journal of
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Hindawiwwwhindawicom Volume 2018
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Journal of
Hindawiwwwhindawicom Volume 2018
High Energy PhysicsAdvances in
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Volume 2018
TribologyAdvances in
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Hindawiwwwhindawicom Volume 2018
ChemistryAdvances in
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Advances inPhysical Chemistry
Hindawiwwwhindawicom Volume 2018
BioMed Research InternationalMaterials
Journal of
Hindawiwwwhindawicom Volume 2018
Na
nom
ate
ria
ls
Hindawiwwwhindawicom Volume 2018
Journal ofNanomaterials
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anepc 71197anec
fnep1 KH times 11282aminus02544nec a
12544n anec lt an lt anepc1113872 1113873
(13)
anpc 2053827anec
fnep2 KH times 14988aminus01021nec a
11021n anepc lt an lt anpc1113872 1113873
(14)
where fnec is contact load for ω ωnec and fnep1 and fnep2are contact loads in the first elastoplastic stage and thesecond elastoplastic stage respectively Both fnep1 and fnep2obtained above are related to the hardness (H) of thematerial However according to the plastic strengtheningprinciple the hardness is not a constant when the materialyields but a function related to the deformation that is itchanges with the deformation erefore it is not accurateto describe elastoplastic deformation by the above formulaIn order to express the characteristics of elastoplastic de-formation more accurately the concept of limit meangeometric hardness is introduced
According to equations (13) and (14) HG(a) is fittedinto the following segmented relations
e first elastoplastic deformation stage is
HG1 an( 1113857 c1Yan
anec1113888 1113889
c2
anec lt an le anepc1113872 1113873 (15)
e second elastoplastic deformation stage is
HG2 an( 1113857 c3Yan
anec1113888 1113889
c4
anepc lt an le anpc1113872 1113873 (16)
where c1 c2 c3 and c4 are the coefficients to be solved
(1) Equation (15) should satisfy two limiting conditions
HG1 anec( 1113857 pea anec( 1113857 (17)
HG1 anepc1113872 1113873 pepa1 anepc1113872 1113873 (18)
where pea(a) is the average contact pressure of theasperity in elastic stage which is given bypea(a) (fnea) pepa1(a) is the average contactpressure of the asperity in the first elastoplastic de-formation stage and is given by pepa1(a) (fnep1a)Substituting equations (11) and (15) in equation (17)we can obtain
c1Y KH (19)
c1 28K (20)
Substituting equations (13) and (15) in equation (18)we can obtain
KH times 11282aminus02544nec times 71197anec( 1113857
02544 28KY times 71197c2
(21)
Derived from equation (21)
c2 ln 11282 times 7119702544( 1113857
ln 71197 (22)
Considering the change of hardness the normal con-tact load of a single asperity in the first elastoplasticstage is
fnep1prime HG1(a) middot an (23)
Substituting equations (15) (20) and (22) in equation(23) new equations are yielded
fnep1prime 28KYaminusc2neca
c2+1n (24)
(2) Equation (16) should satisfy two limiting conditions
HG2 anepc1113872 1113873 pepa1 anepc1113872 1113873 (25)
HG2 anpc1113872 1113873 pepa2 anpc1113872 1113873 (26)
where pepa2(a) (fnep2a) is the average contactpressure of the asperity in the second elastoplastic stageSubstituting equations (13) and (16) in equation (25)we can obtain
c3(71197)c4 K times 28 times 11282 times(71197)
02544 (27)
Substituting equations (14) and (16) in equation (26)we can obtain
c3(2053827)c4 K times 28 times 14988 times(2053827)
01021
(28)
Simultaneous equations (27) and (28) obtained
c4 ln 11282 + 02544 ln 71197minus ln 14988minus 01021 ln 2053827
ln 71197minus ln 2053827
(29)
Substituting equation (29) in equation (27) we canobtain
c3 K times 315896 times(71197)02544minusc4 (30)
Considering the change of hardness the normal con-tact load of a single asperity in the second elastoplasticstage is
fnep2prime HG2(a) middot an K times 315896 times(71197)02544minusc4Y
middot aminusc4nec middot a
c4+1n
(31)
23 Full Plastic Deformation of a Single Asperity As thedeformation continues to increase when ωn gt 110ωnec thecontact area an gt anpc and the asperity enters the stage of fullplastic deformation At this stage the hardness of the ma-terial is no longer affected by the deformation and can beregarded as a constant When the hardness of the material is
4 Advances in Materials Science and Engineering
given according to literature [7] the contact load andcontact area of the asperity at this stage can be expressed as
fnp Han
an 2πRnωn(32)
In conclusion with the increase of load and deformationthe contact area of the same asperity increases graduallyie anec lt anepc lt anpc With the increase of the load andcontact area the asperity underwent elastic deformationfirst elastoplastic deformation second elastoplastic de-formation and full plastic deformation successively Underconstant load and deformation the actual contact area of theasperity is related to the radius of curvature at the vertex ofthe asperity
24 Asperityrsquos Frequency Exponent n When using W-Mfunction to describe the surface profile of an asperity theprofile function is related to the asperityrsquos frequency ex-ponent In other words the radius of curvature at the vertexof the asperity and the height of the asperity vary with thefrequency exponent when the load is constant According tothe equations (5)ndash(7) it was found that the value of hn Rnand ωnec correlated with the frequency exponent When thefrequency exponent is constant the deformation of theasperity is not greater than the height of the asperityunder the action of the load In order to obtain the criticalvalue of the frequency exponent we take hn ωnec ie(GDminus1c(2minusD)nec) (3KH4Eprime)2 middot (cminusnecDGDminus1)
e elastic critical frequency exponent can be obtainedas follows
nec intln 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (33)
where int is the integer part of the value in the parenthesisSimilarly the first elastoplastic critical frequency expo-
nent can be obtained
nepc intln 6 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (34)
e second elastoplastic critical frequency exponent canbe obtained
npc intln 110 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (35)
From the above when the asperity frequency exponent isnmin lt nle nec elastic deformation only takes place in theseasperities under contact load When nec lt nle nepc elasticdeformation or the first elastoplastic deformation can takeplace in these asperities When nepc lt nle npc elastic de-formation the first elastoplastic deformation or the secondelastoplastic deformation can take place in these asperities and
full plastic deformation never occur When npc lt nle nmaxelastic deformation elastoplastic deformation or full plasticdeformation can take place in these asperities
3 Actual Contact Area and Normal ContactLoad of Joint Interface
According to reference [10] when the asperity frequencyexponent is n the area distribution density function of theasperity on the joint interface is defined as
nn(a) 12
D middotaD2nl
a(D+2)2 0lt ale anl 1ltDlt 2( 1113857 (36)
where anl represents the largest contact area when theasperityrsquos frequency exponent is n
In order to simplify equation (36) we define the areadistribution function of the asperity of any frequency ex-ponent as nn(a) Mn(a) According to reference [17] theactual contact area of joint interface is
Ar 1113944
nmax
nnmin
1113946anl
0nn(a)a da M 1113944
nmax
nnmin
1113946anl
0n(a)a da (37)
where M (al1113936nmaxnnmin
anl)(nmin le nle nmax al max anl1113864 1113865)
31 When the Frequency Exponent Belongs to nmin lt nle necWhen the frequency exponent belongs to nmin lt nle nec evenif these asperities are completely deformed only elasticdeformation will occur and anl lt anec In this case the actualcontact area of the joint interface is defined as Ar1
Ar1 1113944
nec
nnmin
1113946anl
0Mn(a)ada
MD
2minusD1113944
nec
nnmin
anl (38)
In this case the contact load of the joint interface is asfollows
Fr1 1113944
nec
nnmin
1113946anl
0fneMn(a)da (39)
Substituting equation (11) in equation (39) we canobtain
Fr1 MD
3minusD1113944
nec
nnmin
4Eπ12G(Dminus1)
3cminusDna32nl (40)
32 When the Frequency Exponent Belongs to nec lt nle nepcWhen the frequency exponent belongs to nec lt nle nepc forthe case anec lt anl le anepc elastic deformation or the firstelastoplastic deformation may take place in these asperitiesAt this point the actual contact area of the joint interfaceconsists of two parts the elastic deformation stage and thefirst elastoplastic deformation stage
Advances in Materials Science and Engineering 5
Ar2 Are + Arep1 (41)
Are 1113944
nepc
nnec+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nepc
nnec+1a
(2minusD)2nec a
D2nl
(42)
For the determined frequency exponent the maximumactual contact area of the asperity appears at the maximumdeformation amount ωn where the maximum value of theelastic deformation phase ωn appears at ωnec whereuponformula (42) is simplified to
Are MD
2minusD1113944
nepc
nnec+1anec
MD
(2minusD)π1113944
nepc
nnec+1
3KHcminusDn
4G(Dminus 1)Eprime1113888 1113889
2
Arep1 1113944
nepc
nnec+11113946
anl
anec
Mn(a)ada MD
2minusD
middot 1113944
nepc
nnec+1a
(2minusD)2nl minus a
(2minusD)2nec1113960 1113961a
D2nl
(43)
e contact load is given by
Fr2 Fre + Frep1 (44)
Fre 1113944
nepc
nnec+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572
middot 1113944
nepc
nnec+1cminus2 Dn
(45)
Frep1 1113944
nepc
nnec+11113946
anl
anec
fnep1prime Mn(a)da (46)
Substituting equations (24) and (36) in equation (46) wecan obtain
Frep1 28KYMD
2c2 minusD + 21113944
nepc
nnec+1aminusc2neca
c2+1nl minus a
(2minusD)2nec a
D2nl1113960 1113961 (47)
33 When the Frequency Exponent Belongs to nepc lt nle npcWhen the frequency exponent belongs to nepc lt nle npc forthe case anepc lt anl le anpc elastic deformation the firstelastoplastic deformation or the second elastoplastic de-formation may take place in these asperities At this point
the actual contact area of the joint interface consists ofthree parts the elastic deformation stage the first elas-toplastic deformation stage and the second elastoplasticdeformation stage
Ar3 Are + Arep1 + Arep2
Are 1113944
npc
nnepc+11113946
anec
0Mn(a)ada
MD
(2minusD)π
middot 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep1 1113944
npc
nnepc+11113946
anepc
anec
Mn(a)ada
MD
π(2minusD)71197minus 71197D2
1113872 1113873 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep2 1113944
npc
nnepc+11113946
anl
anepc
Mn(a)ada
MD
(2minusD)1113944
npc
nnepc+1a
(2minusD)2nl minus 71197anec( 1113857
(2minusD)21113960 1113961a
D2nl
(48)
In this case the contact load of the joint interface is asfollows
Fr3 Fre + Frep1 + Frep2
Fre 1113944
npc
nnepc+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572 1113944
npc
nnepc+1cminus2 Dn
Frep1 28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873
middot 1113944
npc
nnepc+1
1π
3KHcminusDn
4GDminus 1Eprime1113888 1113889
2
(49)
When the second elastoplastic deformation occurs thenormal contact load of the joint interface is as follows
6 Advances in Materials Science and Engineering
Frep2 1113944
npc
nnepc+11113946
anl
anepc
fnep2prime Mn(a)da (50)
Substituting equations (31) and (38) in equation (46) wecan obtain
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
npc
nnepc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
(D2)nl1113872 1113873
(51)
34 When the Frequency Exponent Belongs to npc lt nWhen the frequency exponent belongs to npc lt n elasticdeformation elastoplastic deformation or full plastic de-formation may take place in these asperities e actualcontact area of the joint interface can be evaluated as
Ar4 Are + Arep1 + Arep2 + Arp
Are 1113944
nmax
nnpc+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1anec
Arep1 1113944
nmax
nnpc+11113946
anepc
anec
Mn(a)ada
MD
2minusD71197minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Arep2 1113944
nmax
nnpc+11113946
anpc
anepc
Mn(a)ada
MD
2minusD2053827minus 711971minus(D2)
middot 2053827D21113872 1113873 1113944
nmax
nnpc+1anec
Arp 1113944
nmax
nnpc+11113946
anl
anpc
Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1a
(2minusD)2nl minus 2053827anec( 1113857
(2minusD)21113960 1113961a
D2nl
(52)
In this case the contact load of the joint interface is asfollows
Fr4 Fre + Frep1 + Frep2 + Frp
Fre 1113944
nmax
nnpc+11113946
anec
0fneMn(a)da
MDKH
(3minusD)π1113944
nmax
nnpc+1anec
Frep1 1113944
nmax
nnpc+11113946
anepc
anec
fnep1prime Mn(a)da
28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
nmax
nnpc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
D2nl1113872 1113873
2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 2053827c4+1 minus 2053827D2middot 71197c4minus(D2)+1
1113872 1113873
middot 1113944
nmax
nnpc+1anec
Frp 1113944
nmax
nnpc+11113946
anl
anpc
fnpMn(a)da
MHD
2minusD1113944
nmax
nnpc+1a
D2nl a
1minus(D2)nl minus 2053827anec( 1113857
1minus(D2)1113960 1113961
(53)
For all frequency exponents the total actual contact areaof the joint interface is
Ar Ar1 + Ar2 + Ar3 + Ar4 (54)
e total contact load of the joint interface is
Fr Fr1 + Fr2 + Fr3 + Fr4 (55)
e total real contact area and the total contact load in anondimensional form can be written as follows
Alowastr
Ar
Aa
Flowastr
Fr
AaE
(56)
where Aa is the nominal contact area and is given byAa L2L 1cnmin
Advances in Materials Science and Engineering 7
4 Results Analysis
In order to further analyze the above calculation results theparameters of equivalent joint interface are taken as shownin Table 1 [16]
Figure 2 shows the relation between all critical contactareas and frequency exponents of single asperity whenD 15 It can be seen from the figure that as for one definiteasperity when frequency exponent n is certain elastic criticalcontact area is minimum followed by the first elastoplasticcritical contact area and the second elastoplastic criticalcontact area is maximum With gradual increase of contactload the contact area increases e single asperity is firstlysubject to elastic deformation followed by the first elasto-plastic deformation the second elastoplastic deformation andfully plastic deformation successively which is consistent withtypical contact mechanics theory As for different asperitieswith increase of frequency exponent all critical contact areasdecrease correspondingly which shows that elastic criticalcontact area the first elastoplastic critical contact area and thesecond elastoplastic critical contact area are all related tofrequency exponent n
Figure 3 shows the relation curve between fractal di-mension D and critical frequency exponent n of asperityWhen fractal dimension is definite elastic critical frequencyexponent nec the first elastoplastic critical frequency ex-ponent nepc and the second elastoplastic critical frequencyexponent npc increase gradually As shown in Figure 3 whenDlt 106 nec nepc and npc are all negative As for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation and fully plasticdeformation will all occur When D 113 nec and nepc arenegative and npc is positive At this time as for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation will occur exceptfully plastic deformation
For D 15 G 25 times 10minus9 m H 55 times 109 Nm2 wecan obtain the elastic critical frequency exponent nec 32the first elastoplastic critical frequency exponent nepc 36and the second elastoplastic critical frequency exponentnpc 43 ese asperities whose frequency exponents rangefrom 20 to 32 are only under elastic deformation Elasticdeformation and the first elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 33 to 36 Elastic deformation the first elastoplasticdeformation and the second elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 37 to 43 When frequency exponents range from 43 to50 all deformations types can occur in these asperities
Figure 4 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the first elastoplastic stage ecomparison diagram is simulation result when n 33 It canbe seen from the figure that with gradual increase of contactarea with contact area of single asperity over 32 times 10minus13 m2contact load of the same asperity with hardness change willbe less than that without hardness change In addition as theamount of deformation increases the difference betweenthem tends to increase
Figure 5 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the second elastoplastic stagee comparison diagram is simulation result when n 37 Itcan be seen from the figure that when the deformation is
Table 1 e parameters of equivalent joint interface
Parameters ValuesEquivalent elastic modulus Eprime 72 times 1010 Nm2
Poissonrsquos ratio υ 017Initial hardness H 55 times 109 Nm2
Profile scale parameter G 25 times 10minus9 mFractal dimension D 1ltDlt 2Frequency exponent n 20sim50
20 25 30 35 40 45 5010ndash1510ndash1410ndash1310ndash1210ndash1110ndash1010ndash910ndash810ndash710ndash610ndash510ndash410ndash3
Criti
cal c
onta
ct ar
eas
of a
singl
e asp
erity
(am
2 )
Asperity levels (n)
Second elastoplastic critical contact areaFirst elastoplastic critical contact areaElastic critical contact area
Figure 2 e relationship between critical contact area and fre-quency exponent of a single asperity
10 11 12 13 14 15 16 17 18 19 20ndash140
ndash120
ndash100
ndash80
ndash60
ndash40
ndash20
0
20
40
Asp
erity
freq
uenc
y ex
pone
nts (n)
e fractal dimension (D)
Elastic critical frequency exponentsFirst elastoplastic critical frequency exponentsSecond elastoplastic critical frequency exponents
Figure 3 e relationship between fractal dimension D andcritical frequency exponent n of a single asperity
8 Advances in Materials Science and Engineering
definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
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given according to literature [7] the contact load andcontact area of the asperity at this stage can be expressed as
fnp Han
an 2πRnωn(32)
In conclusion with the increase of load and deformationthe contact area of the same asperity increases graduallyie anec lt anepc lt anpc With the increase of the load andcontact area the asperity underwent elastic deformationfirst elastoplastic deformation second elastoplastic de-formation and full plastic deformation successively Underconstant load and deformation the actual contact area of theasperity is related to the radius of curvature at the vertex ofthe asperity
24 Asperityrsquos Frequency Exponent n When using W-Mfunction to describe the surface profile of an asperity theprofile function is related to the asperityrsquos frequency ex-ponent In other words the radius of curvature at the vertexof the asperity and the height of the asperity vary with thefrequency exponent when the load is constant According tothe equations (5)ndash(7) it was found that the value of hn Rnand ωnec correlated with the frequency exponent When thefrequency exponent is constant the deformation of theasperity is not greater than the height of the asperityunder the action of the load In order to obtain the criticalvalue of the frequency exponent we take hn ωnec ie(GDminus1c(2minusD)nec) (3KH4Eprime)2 middot (cminusnecDGDminus1)
e elastic critical frequency exponent can be obtainedas follows
nec intln 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (33)
where int is the integer part of the value in the parenthesisSimilarly the first elastoplastic critical frequency expo-
nent can be obtained
nepc intln 6 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (34)
e second elastoplastic critical frequency exponent canbe obtained
npc intln 110 3KH4Eprime( 1113857
2middot G2(1minusD)1113960 1113961
2(Dminus 1)ln c
⎧⎨
⎩
⎫⎬
⎭ (35)
From the above when the asperity frequency exponent isnmin lt nle nec elastic deformation only takes place in theseasperities under contact load When nec lt nle nepc elasticdeformation or the first elastoplastic deformation can takeplace in these asperities When nepc lt nle npc elastic de-formation the first elastoplastic deformation or the secondelastoplastic deformation can take place in these asperities and
full plastic deformation never occur When npc lt nle nmaxelastic deformation elastoplastic deformation or full plasticdeformation can take place in these asperities
3 Actual Contact Area and Normal ContactLoad of Joint Interface
According to reference [10] when the asperity frequencyexponent is n the area distribution density function of theasperity on the joint interface is defined as
nn(a) 12
D middotaD2nl
a(D+2)2 0lt ale anl 1ltDlt 2( 1113857 (36)
where anl represents the largest contact area when theasperityrsquos frequency exponent is n
In order to simplify equation (36) we define the areadistribution function of the asperity of any frequency ex-ponent as nn(a) Mn(a) According to reference [17] theactual contact area of joint interface is
Ar 1113944
nmax
nnmin
1113946anl
0nn(a)a da M 1113944
nmax
nnmin
1113946anl
0n(a)a da (37)
where M (al1113936nmaxnnmin
anl)(nmin le nle nmax al max anl1113864 1113865)
31 When the Frequency Exponent Belongs to nmin lt nle necWhen the frequency exponent belongs to nmin lt nle nec evenif these asperities are completely deformed only elasticdeformation will occur and anl lt anec In this case the actualcontact area of the joint interface is defined as Ar1
Ar1 1113944
nec
nnmin
1113946anl
0Mn(a)ada
MD
2minusD1113944
nec
nnmin
anl (38)
In this case the contact load of the joint interface is asfollows
Fr1 1113944
nec
nnmin
1113946anl
0fneMn(a)da (39)
Substituting equation (11) in equation (39) we canobtain
Fr1 MD
3minusD1113944
nec
nnmin
4Eπ12G(Dminus1)
3cminusDna32nl (40)
32 When the Frequency Exponent Belongs to nec lt nle nepcWhen the frequency exponent belongs to nec lt nle nepc forthe case anec lt anl le anepc elastic deformation or the firstelastoplastic deformation may take place in these asperitiesAt this point the actual contact area of the joint interfaceconsists of two parts the elastic deformation stage and thefirst elastoplastic deformation stage
Advances in Materials Science and Engineering 5
Ar2 Are + Arep1 (41)
Are 1113944
nepc
nnec+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nepc
nnec+1a
(2minusD)2nec a
D2nl
(42)
For the determined frequency exponent the maximumactual contact area of the asperity appears at the maximumdeformation amount ωn where the maximum value of theelastic deformation phase ωn appears at ωnec whereuponformula (42) is simplified to
Are MD
2minusD1113944
nepc
nnec+1anec
MD
(2minusD)π1113944
nepc
nnec+1
3KHcminusDn
4G(Dminus 1)Eprime1113888 1113889
2
Arep1 1113944
nepc
nnec+11113946
anl
anec
Mn(a)ada MD
2minusD
middot 1113944
nepc
nnec+1a
(2minusD)2nl minus a
(2minusD)2nec1113960 1113961a
D2nl
(43)
e contact load is given by
Fr2 Fre + Frep1 (44)
Fre 1113944
nepc
nnec+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572
middot 1113944
nepc
nnec+1cminus2 Dn
(45)
Frep1 1113944
nepc
nnec+11113946
anl
anec
fnep1prime Mn(a)da (46)
Substituting equations (24) and (36) in equation (46) wecan obtain
Frep1 28KYMD
2c2 minusD + 21113944
nepc
nnec+1aminusc2neca
c2+1nl minus a
(2minusD)2nec a
D2nl1113960 1113961 (47)
33 When the Frequency Exponent Belongs to nepc lt nle npcWhen the frequency exponent belongs to nepc lt nle npc forthe case anepc lt anl le anpc elastic deformation the firstelastoplastic deformation or the second elastoplastic de-formation may take place in these asperities At this point
the actual contact area of the joint interface consists ofthree parts the elastic deformation stage the first elas-toplastic deformation stage and the second elastoplasticdeformation stage
Ar3 Are + Arep1 + Arep2
Are 1113944
npc
nnepc+11113946
anec
0Mn(a)ada
MD
(2minusD)π
middot 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep1 1113944
npc
nnepc+11113946
anepc
anec
Mn(a)ada
MD
π(2minusD)71197minus 71197D2
1113872 1113873 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep2 1113944
npc
nnepc+11113946
anl
anepc
Mn(a)ada
MD
(2minusD)1113944
npc
nnepc+1a
(2minusD)2nl minus 71197anec( 1113857
(2minusD)21113960 1113961a
D2nl
(48)
In this case the contact load of the joint interface is asfollows
Fr3 Fre + Frep1 + Frep2
Fre 1113944
npc
nnepc+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572 1113944
npc
nnepc+1cminus2 Dn
Frep1 28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873
middot 1113944
npc
nnepc+1
1π
3KHcminusDn
4GDminus 1Eprime1113888 1113889
2
(49)
When the second elastoplastic deformation occurs thenormal contact load of the joint interface is as follows
6 Advances in Materials Science and Engineering
Frep2 1113944
npc
nnepc+11113946
anl
anepc
fnep2prime Mn(a)da (50)
Substituting equations (31) and (38) in equation (46) wecan obtain
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
npc
nnepc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
(D2)nl1113872 1113873
(51)
34 When the Frequency Exponent Belongs to npc lt nWhen the frequency exponent belongs to npc lt n elasticdeformation elastoplastic deformation or full plastic de-formation may take place in these asperities e actualcontact area of the joint interface can be evaluated as
Ar4 Are + Arep1 + Arep2 + Arp
Are 1113944
nmax
nnpc+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1anec
Arep1 1113944
nmax
nnpc+11113946
anepc
anec
Mn(a)ada
MD
2minusD71197minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Arep2 1113944
nmax
nnpc+11113946
anpc
anepc
Mn(a)ada
MD
2minusD2053827minus 711971minus(D2)
middot 2053827D21113872 1113873 1113944
nmax
nnpc+1anec
Arp 1113944
nmax
nnpc+11113946
anl
anpc
Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1a
(2minusD)2nl minus 2053827anec( 1113857
(2minusD)21113960 1113961a
D2nl
(52)
In this case the contact load of the joint interface is asfollows
Fr4 Fre + Frep1 + Frep2 + Frp
Fre 1113944
nmax
nnpc+11113946
anec
0fneMn(a)da
MDKH
(3minusD)π1113944
nmax
nnpc+1anec
Frep1 1113944
nmax
nnpc+11113946
anepc
anec
fnep1prime Mn(a)da
28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
nmax
nnpc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
D2nl1113872 1113873
2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 2053827c4+1 minus 2053827D2middot 71197c4minus(D2)+1
1113872 1113873
middot 1113944
nmax
nnpc+1anec
Frp 1113944
nmax
nnpc+11113946
anl
anpc
fnpMn(a)da
MHD
2minusD1113944
nmax
nnpc+1a
D2nl a
1minus(D2)nl minus 2053827anec( 1113857
1minus(D2)1113960 1113961
(53)
For all frequency exponents the total actual contact areaof the joint interface is
Ar Ar1 + Ar2 + Ar3 + Ar4 (54)
e total contact load of the joint interface is
Fr Fr1 + Fr2 + Fr3 + Fr4 (55)
e total real contact area and the total contact load in anondimensional form can be written as follows
Alowastr
Ar
Aa
Flowastr
Fr
AaE
(56)
where Aa is the nominal contact area and is given byAa L2L 1cnmin
Advances in Materials Science and Engineering 7
4 Results Analysis
In order to further analyze the above calculation results theparameters of equivalent joint interface are taken as shownin Table 1 [16]
Figure 2 shows the relation between all critical contactareas and frequency exponents of single asperity whenD 15 It can be seen from the figure that as for one definiteasperity when frequency exponent n is certain elastic criticalcontact area is minimum followed by the first elastoplasticcritical contact area and the second elastoplastic criticalcontact area is maximum With gradual increase of contactload the contact area increases e single asperity is firstlysubject to elastic deformation followed by the first elasto-plastic deformation the second elastoplastic deformation andfully plastic deformation successively which is consistent withtypical contact mechanics theory As for different asperitieswith increase of frequency exponent all critical contact areasdecrease correspondingly which shows that elastic criticalcontact area the first elastoplastic critical contact area and thesecond elastoplastic critical contact area are all related tofrequency exponent n
Figure 3 shows the relation curve between fractal di-mension D and critical frequency exponent n of asperityWhen fractal dimension is definite elastic critical frequencyexponent nec the first elastoplastic critical frequency ex-ponent nepc and the second elastoplastic critical frequencyexponent npc increase gradually As shown in Figure 3 whenDlt 106 nec nepc and npc are all negative As for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation and fully plasticdeformation will all occur When D 113 nec and nepc arenegative and npc is positive At this time as for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation will occur exceptfully plastic deformation
For D 15 G 25 times 10minus9 m H 55 times 109 Nm2 wecan obtain the elastic critical frequency exponent nec 32the first elastoplastic critical frequency exponent nepc 36and the second elastoplastic critical frequency exponentnpc 43 ese asperities whose frequency exponents rangefrom 20 to 32 are only under elastic deformation Elasticdeformation and the first elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 33 to 36 Elastic deformation the first elastoplasticdeformation and the second elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 37 to 43 When frequency exponents range from 43 to50 all deformations types can occur in these asperities
Figure 4 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the first elastoplastic stage ecomparison diagram is simulation result when n 33 It canbe seen from the figure that with gradual increase of contactarea with contact area of single asperity over 32 times 10minus13 m2contact load of the same asperity with hardness change willbe less than that without hardness change In addition as theamount of deformation increases the difference betweenthem tends to increase
Figure 5 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the second elastoplastic stagee comparison diagram is simulation result when n 37 Itcan be seen from the figure that when the deformation is
Table 1 e parameters of equivalent joint interface
Parameters ValuesEquivalent elastic modulus Eprime 72 times 1010 Nm2
Poissonrsquos ratio υ 017Initial hardness H 55 times 109 Nm2
Profile scale parameter G 25 times 10minus9 mFractal dimension D 1ltDlt 2Frequency exponent n 20sim50
20 25 30 35 40 45 5010ndash1510ndash1410ndash1310ndash1210ndash1110ndash1010ndash910ndash810ndash710ndash610ndash510ndash410ndash3
Criti
cal c
onta
ct ar
eas
of a
singl
e asp
erity
(am
2 )
Asperity levels (n)
Second elastoplastic critical contact areaFirst elastoplastic critical contact areaElastic critical contact area
Figure 2 e relationship between critical contact area and fre-quency exponent of a single asperity
10 11 12 13 14 15 16 17 18 19 20ndash140
ndash120
ndash100
ndash80
ndash60
ndash40
ndash20
0
20
40
Asp
erity
freq
uenc
y ex
pone
nts (n)
e fractal dimension (D)
Elastic critical frequency exponentsFirst elastoplastic critical frequency exponentsSecond elastoplastic critical frequency exponents
Figure 3 e relationship between fractal dimension D andcritical frequency exponent n of a single asperity
8 Advances in Materials Science and Engineering
definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
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Ar2 Are + Arep1 (41)
Are 1113944
nepc
nnec+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nepc
nnec+1a
(2minusD)2nec a
D2nl
(42)
For the determined frequency exponent the maximumactual contact area of the asperity appears at the maximumdeformation amount ωn where the maximum value of theelastic deformation phase ωn appears at ωnec whereuponformula (42) is simplified to
Are MD
2minusD1113944
nepc
nnec+1anec
MD
(2minusD)π1113944
nepc
nnec+1
3KHcminusDn
4G(Dminus 1)Eprime1113888 1113889
2
Arep1 1113944
nepc
nnec+11113946
anl
anec
Mn(a)ada MD
2minusD
middot 1113944
nepc
nnec+1a
(2minusD)2nl minus a
(2minusD)2nec1113960 1113961a
D2nl
(43)
e contact load is given by
Fr2 Fre + Frep1 (44)
Fre 1113944
nepc
nnec+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572
middot 1113944
nepc
nnec+1cminus2 Dn
(45)
Frep1 1113944
nepc
nnec+11113946
anl
anec
fnep1prime Mn(a)da (46)
Substituting equations (24) and (36) in equation (46) wecan obtain
Frep1 28KYMD
2c2 minusD + 21113944
nepc
nnec+1aminusc2neca
c2+1nl minus a
(2minusD)2nec a
D2nl1113960 1113961 (47)
33 When the Frequency Exponent Belongs to nepc lt nle npcWhen the frequency exponent belongs to nepc lt nle npc forthe case anepc lt anl le anpc elastic deformation the firstelastoplastic deformation or the second elastoplastic de-formation may take place in these asperities At this point
the actual contact area of the joint interface consists ofthree parts the elastic deformation stage the first elas-toplastic deformation stage and the second elastoplasticdeformation stage
Ar3 Are + Arep1 + Arep2
Are 1113944
npc
nnepc+11113946
anec
0Mn(a)ada
MD
(2minusD)π
middot 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep1 1113944
npc
nnepc+11113946
anepc
anec
Mn(a)ada
MD
π(2minusD)71197minus 71197D2
1113872 1113873 1113944
npc
nnepc+1
3KHcminusDn
4GDminus1Eprime1113888 1113889
2
Arep2 1113944
npc
nnepc+11113946
anl
anepc
Mn(a)ada
MD
(2minusD)1113944
npc
nnepc+1a
(2minusD)2nl minus 71197anec( 1113857
(2minusD)21113960 1113961a
D2nl
(48)
In this case the contact load of the joint interface is asfollows
Fr3 Fre + Frep1 + Frep2
Fre 1113944
npc
nnepc+11113946
anec
0fneMn(a)da
9MD(KH)3
16(3minusD) EprimeπGDminus1( 11138572 1113944
npc
nnepc+1cminus2 Dn
Frep1 28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873
middot 1113944
npc
nnepc+1
1π
3KHcminusDn
4GDminus 1Eprime1113888 1113889
2
(49)
When the second elastoplastic deformation occurs thenormal contact load of the joint interface is as follows
6 Advances in Materials Science and Engineering
Frep2 1113944
npc
nnepc+11113946
anl
anepc
fnep2prime Mn(a)da (50)
Substituting equations (31) and (38) in equation (46) wecan obtain
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
npc
nnepc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
(D2)nl1113872 1113873
(51)
34 When the Frequency Exponent Belongs to npc lt nWhen the frequency exponent belongs to npc lt n elasticdeformation elastoplastic deformation or full plastic de-formation may take place in these asperities e actualcontact area of the joint interface can be evaluated as
Ar4 Are + Arep1 + Arep2 + Arp
Are 1113944
nmax
nnpc+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1anec
Arep1 1113944
nmax
nnpc+11113946
anepc
anec
Mn(a)ada
MD
2minusD71197minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Arep2 1113944
nmax
nnpc+11113946
anpc
anepc
Mn(a)ada
MD
2minusD2053827minus 711971minus(D2)
middot 2053827D21113872 1113873 1113944
nmax
nnpc+1anec
Arp 1113944
nmax
nnpc+11113946
anl
anpc
Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1a
(2minusD)2nl minus 2053827anec( 1113857
(2minusD)21113960 1113961a
D2nl
(52)
In this case the contact load of the joint interface is asfollows
Fr4 Fre + Frep1 + Frep2 + Frp
Fre 1113944
nmax
nnpc+11113946
anec
0fneMn(a)da
MDKH
(3minusD)π1113944
nmax
nnpc+1anec
Frep1 1113944
nmax
nnpc+11113946
anepc
anec
fnep1prime Mn(a)da
28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
nmax
nnpc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
D2nl1113872 1113873
2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 2053827c4+1 minus 2053827D2middot 71197c4minus(D2)+1
1113872 1113873
middot 1113944
nmax
nnpc+1anec
Frp 1113944
nmax
nnpc+11113946
anl
anpc
fnpMn(a)da
MHD
2minusD1113944
nmax
nnpc+1a
D2nl a
1minus(D2)nl minus 2053827anec( 1113857
1minus(D2)1113960 1113961
(53)
For all frequency exponents the total actual contact areaof the joint interface is
Ar Ar1 + Ar2 + Ar3 + Ar4 (54)
e total contact load of the joint interface is
Fr Fr1 + Fr2 + Fr3 + Fr4 (55)
e total real contact area and the total contact load in anondimensional form can be written as follows
Alowastr
Ar
Aa
Flowastr
Fr
AaE
(56)
where Aa is the nominal contact area and is given byAa L2L 1cnmin
Advances in Materials Science and Engineering 7
4 Results Analysis
In order to further analyze the above calculation results theparameters of equivalent joint interface are taken as shownin Table 1 [16]
Figure 2 shows the relation between all critical contactareas and frequency exponents of single asperity whenD 15 It can be seen from the figure that as for one definiteasperity when frequency exponent n is certain elastic criticalcontact area is minimum followed by the first elastoplasticcritical contact area and the second elastoplastic criticalcontact area is maximum With gradual increase of contactload the contact area increases e single asperity is firstlysubject to elastic deformation followed by the first elasto-plastic deformation the second elastoplastic deformation andfully plastic deformation successively which is consistent withtypical contact mechanics theory As for different asperitieswith increase of frequency exponent all critical contact areasdecrease correspondingly which shows that elastic criticalcontact area the first elastoplastic critical contact area and thesecond elastoplastic critical contact area are all related tofrequency exponent n
Figure 3 shows the relation curve between fractal di-mension D and critical frequency exponent n of asperityWhen fractal dimension is definite elastic critical frequencyexponent nec the first elastoplastic critical frequency ex-ponent nepc and the second elastoplastic critical frequencyexponent npc increase gradually As shown in Figure 3 whenDlt 106 nec nepc and npc are all negative As for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation and fully plasticdeformation will all occur When D 113 nec and nepc arenegative and npc is positive At this time as for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation will occur exceptfully plastic deformation
For D 15 G 25 times 10minus9 m H 55 times 109 Nm2 wecan obtain the elastic critical frequency exponent nec 32the first elastoplastic critical frequency exponent nepc 36and the second elastoplastic critical frequency exponentnpc 43 ese asperities whose frequency exponents rangefrom 20 to 32 are only under elastic deformation Elasticdeformation and the first elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 33 to 36 Elastic deformation the first elastoplasticdeformation and the second elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 37 to 43 When frequency exponents range from 43 to50 all deformations types can occur in these asperities
Figure 4 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the first elastoplastic stage ecomparison diagram is simulation result when n 33 It canbe seen from the figure that with gradual increase of contactarea with contact area of single asperity over 32 times 10minus13 m2contact load of the same asperity with hardness change willbe less than that without hardness change In addition as theamount of deformation increases the difference betweenthem tends to increase
Figure 5 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the second elastoplastic stagee comparison diagram is simulation result when n 37 Itcan be seen from the figure that when the deformation is
Table 1 e parameters of equivalent joint interface
Parameters ValuesEquivalent elastic modulus Eprime 72 times 1010 Nm2
Poissonrsquos ratio υ 017Initial hardness H 55 times 109 Nm2
Profile scale parameter G 25 times 10minus9 mFractal dimension D 1ltDlt 2Frequency exponent n 20sim50
20 25 30 35 40 45 5010ndash1510ndash1410ndash1310ndash1210ndash1110ndash1010ndash910ndash810ndash710ndash610ndash510ndash410ndash3
Criti
cal c
onta
ct ar
eas
of a
singl
e asp
erity
(am
2 )
Asperity levels (n)
Second elastoplastic critical contact areaFirst elastoplastic critical contact areaElastic critical contact area
Figure 2 e relationship between critical contact area and fre-quency exponent of a single asperity
10 11 12 13 14 15 16 17 18 19 20ndash140
ndash120
ndash100
ndash80
ndash60
ndash40
ndash20
0
20
40
Asp
erity
freq
uenc
y ex
pone
nts (n)
e fractal dimension (D)
Elastic critical frequency exponentsFirst elastoplastic critical frequency exponentsSecond elastoplastic critical frequency exponents
Figure 3 e relationship between fractal dimension D andcritical frequency exponent n of a single asperity
8 Advances in Materials Science and Engineering
definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
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Frep2 1113944
npc
nnepc+11113946
anl
anepc
fnep2prime Mn(a)da (50)
Substituting equations (31) and (38) in equation (46) wecan obtain
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
npc
nnepc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
(D2)nl1113872 1113873
(51)
34 When the Frequency Exponent Belongs to npc lt nWhen the frequency exponent belongs to npc lt n elasticdeformation elastoplastic deformation or full plastic de-formation may take place in these asperities e actualcontact area of the joint interface can be evaluated as
Ar4 Are + Arep1 + Arep2 + Arp
Are 1113944
nmax
nnpc+11113946
anec
0Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1anec
Arep1 1113944
nmax
nnpc+11113946
anepc
anec
Mn(a)ada
MD
2minusD71197minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Arep2 1113944
nmax
nnpc+11113946
anpc
anepc
Mn(a)ada
MD
2minusD2053827minus 711971minus(D2)
middot 2053827D21113872 1113873 1113944
nmax
nnpc+1anec
Arp 1113944
nmax
nnpc+11113946
anl
anpc
Mn(a)ada
MD
2minusD1113944
nmax
nnpc+1a
(2minusD)2nl minus 2053827anec( 1113857
(2minusD)21113960 1113961a
D2nl
(52)
In this case the contact load of the joint interface is asfollows
Fr4 Fre + Frep1 + Frep2 + Frp
Fre 1113944
nmax
nnpc+11113946
anec
0fneMn(a)da
MDKH
(3minusD)π1113944
nmax
nnpc+1anec
Frep1 1113944
nmax
nnpc+11113946
anepc
anec
fnep1prime Mn(a)da
28KYMD
2c2 minusD + 271197c2+1 minus 71197D2
1113872 1113873 1113944
nmax
nnpc+1anec
Frep2 2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 1113944
nmax
nnpc+1aminusc4neca
c4+1nl minus 71197c4minus(D2)+1
a1minus(D2)nec a
D2nl1113872 1113873
2106 times 7119702544minusc4KYMD
2c4 minusD + 2
middot 2053827c4+1 minus 2053827D2middot 71197c4minus(D2)+1
1113872 1113873
middot 1113944
nmax
nnpc+1anec
Frp 1113944
nmax
nnpc+11113946
anl
anpc
fnpMn(a)da
MHD
2minusD1113944
nmax
nnpc+1a
D2nl a
1minus(D2)nl minus 2053827anec( 1113857
1minus(D2)1113960 1113961
(53)
For all frequency exponents the total actual contact areaof the joint interface is
Ar Ar1 + Ar2 + Ar3 + Ar4 (54)
e total contact load of the joint interface is
Fr Fr1 + Fr2 + Fr3 + Fr4 (55)
e total real contact area and the total contact load in anondimensional form can be written as follows
Alowastr
Ar
Aa
Flowastr
Fr
AaE
(56)
where Aa is the nominal contact area and is given byAa L2L 1cnmin
Advances in Materials Science and Engineering 7
4 Results Analysis
In order to further analyze the above calculation results theparameters of equivalent joint interface are taken as shownin Table 1 [16]
Figure 2 shows the relation between all critical contactareas and frequency exponents of single asperity whenD 15 It can be seen from the figure that as for one definiteasperity when frequency exponent n is certain elastic criticalcontact area is minimum followed by the first elastoplasticcritical contact area and the second elastoplastic criticalcontact area is maximum With gradual increase of contactload the contact area increases e single asperity is firstlysubject to elastic deformation followed by the first elasto-plastic deformation the second elastoplastic deformation andfully plastic deformation successively which is consistent withtypical contact mechanics theory As for different asperitieswith increase of frequency exponent all critical contact areasdecrease correspondingly which shows that elastic criticalcontact area the first elastoplastic critical contact area and thesecond elastoplastic critical contact area are all related tofrequency exponent n
Figure 3 shows the relation curve between fractal di-mension D and critical frequency exponent n of asperityWhen fractal dimension is definite elastic critical frequencyexponent nec the first elastoplastic critical frequency ex-ponent nepc and the second elastoplastic critical frequencyexponent npc increase gradually As shown in Figure 3 whenDlt 106 nec nepc and npc are all negative As for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation and fully plasticdeformation will all occur When D 113 nec and nepc arenegative and npc is positive At this time as for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation will occur exceptfully plastic deformation
For D 15 G 25 times 10minus9 m H 55 times 109 Nm2 wecan obtain the elastic critical frequency exponent nec 32the first elastoplastic critical frequency exponent nepc 36and the second elastoplastic critical frequency exponentnpc 43 ese asperities whose frequency exponents rangefrom 20 to 32 are only under elastic deformation Elasticdeformation and the first elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 33 to 36 Elastic deformation the first elastoplasticdeformation and the second elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 37 to 43 When frequency exponents range from 43 to50 all deformations types can occur in these asperities
Figure 4 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the first elastoplastic stage ecomparison diagram is simulation result when n 33 It canbe seen from the figure that with gradual increase of contactarea with contact area of single asperity over 32 times 10minus13 m2contact load of the same asperity with hardness change willbe less than that without hardness change In addition as theamount of deformation increases the difference betweenthem tends to increase
Figure 5 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the second elastoplastic stagee comparison diagram is simulation result when n 37 Itcan be seen from the figure that when the deformation is
Table 1 e parameters of equivalent joint interface
Parameters ValuesEquivalent elastic modulus Eprime 72 times 1010 Nm2
Poissonrsquos ratio υ 017Initial hardness H 55 times 109 Nm2
Profile scale parameter G 25 times 10minus9 mFractal dimension D 1ltDlt 2Frequency exponent n 20sim50
20 25 30 35 40 45 5010ndash1510ndash1410ndash1310ndash1210ndash1110ndash1010ndash910ndash810ndash710ndash610ndash510ndash410ndash3
Criti
cal c
onta
ct ar
eas
of a
singl
e asp
erity
(am
2 )
Asperity levels (n)
Second elastoplastic critical contact areaFirst elastoplastic critical contact areaElastic critical contact area
Figure 2 e relationship between critical contact area and fre-quency exponent of a single asperity
10 11 12 13 14 15 16 17 18 19 20ndash140
ndash120
ndash100
ndash80
ndash60
ndash40
ndash20
0
20
40
Asp
erity
freq
uenc
y ex
pone
nts (n)
e fractal dimension (D)
Elastic critical frequency exponentsFirst elastoplastic critical frequency exponentsSecond elastoplastic critical frequency exponents
Figure 3 e relationship between fractal dimension D andcritical frequency exponent n of a single asperity
8 Advances in Materials Science and Engineering
definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
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Submit your manuscripts atwwwhindawicom
4 Results Analysis
In order to further analyze the above calculation results theparameters of equivalent joint interface are taken as shownin Table 1 [16]
Figure 2 shows the relation between all critical contactareas and frequency exponents of single asperity whenD 15 It can be seen from the figure that as for one definiteasperity when frequency exponent n is certain elastic criticalcontact area is minimum followed by the first elastoplasticcritical contact area and the second elastoplastic criticalcontact area is maximum With gradual increase of contactload the contact area increases e single asperity is firstlysubject to elastic deformation followed by the first elasto-plastic deformation the second elastoplastic deformation andfully plastic deformation successively which is consistent withtypical contact mechanics theory As for different asperitieswith increase of frequency exponent all critical contact areasdecrease correspondingly which shows that elastic criticalcontact area the first elastoplastic critical contact area and thesecond elastoplastic critical contact area are all related tofrequency exponent n
Figure 3 shows the relation curve between fractal di-mension D and critical frequency exponent n of asperityWhen fractal dimension is definite elastic critical frequencyexponent nec the first elastoplastic critical frequency ex-ponent nepc and the second elastoplastic critical frequencyexponent npc increase gradually As shown in Figure 3 whenDlt 106 nec nepc and npc are all negative As for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation and fully plasticdeformation will all occur When D 113 nec and nepc arenegative and npc is positive At this time as for asperitieswith minimum value of frequency exponent being 0 elasticdeformation elastoplastic deformation will occur exceptfully plastic deformation
For D 15 G 25 times 10minus9 m H 55 times 109 Nm2 wecan obtain the elastic critical frequency exponent nec 32the first elastoplastic critical frequency exponent nepc 36and the second elastoplastic critical frequency exponentnpc 43 ese asperities whose frequency exponents rangefrom 20 to 32 are only under elastic deformation Elasticdeformation and the first elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 33 to 36 Elastic deformation the first elastoplasticdeformation and the second elastoplastic deformation canoccur in these asperities whose frequency exponents rangefrom 37 to 43 When frequency exponents range from 43 to50 all deformations types can occur in these asperities
Figure 4 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the first elastoplastic stage ecomparison diagram is simulation result when n 33 It canbe seen from the figure that with gradual increase of contactarea with contact area of single asperity over 32 times 10minus13 m2contact load of the same asperity with hardness change willbe less than that without hardness change In addition as theamount of deformation increases the difference betweenthem tends to increase
Figure 5 shows relation comparison diagram betweencontact load and contact area of single asperity with andwithout hardness change at the second elastoplastic stagee comparison diagram is simulation result when n 37 Itcan be seen from the figure that when the deformation is
Table 1 e parameters of equivalent joint interface
Parameters ValuesEquivalent elastic modulus Eprime 72 times 1010 Nm2
Poissonrsquos ratio υ 017Initial hardness H 55 times 109 Nm2
Profile scale parameter G 25 times 10minus9 mFractal dimension D 1ltDlt 2Frequency exponent n 20sim50
20 25 30 35 40 45 5010ndash1510ndash1410ndash1310ndash1210ndash1110ndash1010ndash910ndash810ndash710ndash610ndash510ndash410ndash3
Criti
cal c
onta
ct ar
eas
of a
singl
e asp
erity
(am
2 )
Asperity levels (n)
Second elastoplastic critical contact areaFirst elastoplastic critical contact areaElastic critical contact area
Figure 2 e relationship between critical contact area and fre-quency exponent of a single asperity
10 11 12 13 14 15 16 17 18 19 20ndash140
ndash120
ndash100
ndash80
ndash60
ndash40
ndash20
0
20
40
Asp
erity
freq
uenc
y ex
pone
nts (n)
e fractal dimension (D)
Elastic critical frequency exponentsFirst elastoplastic critical frequency exponentsSecond elastoplastic critical frequency exponents
Figure 3 e relationship between fractal dimension D andcritical frequency exponent n of a single asperity
8 Advances in Materials Science and Engineering
definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
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definite contact load of the same asperity with hardnesschange will be less than that without hardness change Inaddition with increase of deformation amount the differ-ence between them tends to increase which is consistentwith the change trend at the first elastoplastic stage
Figure 6 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the first elastoplastic deformation stage Figure 6(a)shows relation curve that D 11 13 15 17 when n 34Figure 6(b) shows relation curve that n 32 33 34 35 whenD 15 It can be seen from Figure 6 that the limit meangeometric hardness of single asperity is related to contactarea fractal dimension and frequency exponent in the firstelastoplastic deformation stage e limit mean geometrichardness increases with increase of contact area When n is
definite the relation between limit mean geometric hardnessand contact area of asperity is related to fractal dimension De larger the D is the more obvious the relation curvebetween them changes when D is definite the relationbetween limit mean geometric hardness and contact area ofasperity is related to frequency exponent n e smaller n isthe more obvious the relation curve between them changes
Figure 7 shows the relation between limit mean geo-metric hardness and contact area (logarithm) of single as-perity at the second elastoplastic deformation stageFigure 7(a) shows the relation curve n 40 that D 11 1315 17 when n 40 Figure 7(b) shows the relation curvethat n 36 38 40 42 when D 15
During loading the contact area increases with the in-crease of deformation of a single asperity e ratio of de-formation to the natural height of the asperity is defined asthe pushing coefficient namely the pushing coefficientk ωnhn 0le kle 09 When fractal dimension is 15 we willresearch the relation between contact load and contact areaof single asperity with frequency exponent n being 30 35and 40 respectively during loading
When n 30 the asperity will only be subject to elasticdeformation During loading even the pushing coefficient k
is maximum no plastic deformation will occur e relationbetween contact area and contact load is fsima15 approxi-mately as shown in Figure 8(a)
As is shown in Figure 8(b) when n 35 elastic de-formation and the first elastoplastic deformation may takeplace in the asperity during loading When the pushingcoefficient k is less than 0247 the asperity will under elasticdeformation At this time the relation between contact areaand contact load is fsima15 approximately when the pushingcoefficient is over 0247 the first elastoplastic deformationoccurs At this time the relation between contact area andcontact load is fsima11093 approximately As is shown inFigure 8(c) when n 40 elastic deformation the firstelastoplastic deformation and the second elastoplastic
0000 0001 0002 0003 0004 0005Contact load of a single asperity in the
first elastoplastic deformation regime (fN)
00
12 times 10ndash12
10 times 10ndash12
80 times 10ndash13
60 times 10ndash13
40 times 10ndash13
20 times 10ndash13
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Change of hardness is consideredChange of hardness is not considered
Figure 4 e relationship between contact load and contact area of single asperity in the first elastoplastic deformation stage
0000 0001 0002 0003 0004 00050
2 times 10ndash13
4 times 10ndash13
6 times 10ndash13
8 times 10ndash13
1 times 10ndash12
1 times 10ndash12
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
Contact load of a single asperity in the second elastoplastic deformation regime (f2N)
Change of hardness is not consideredChange of hardness is considered
Figure 5e relationship between contact load and contact area ofsingle asperity in the second elastoplastic deformation stage
Advances in Materials Science and Engineering 9
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
CorrosionInternational Journal of
Hindawiwwwhindawicom Volume 2018
Advances in
Materials Science and EngineeringHindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Journal of
Chemistry
Analytical ChemistryInternational Journal of
Hindawiwwwhindawicom Volume 2018
ScienticaHindawiwwwhindawicom Volume 2018
Polymer ScienceInternational Journal of
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Advances in Condensed Matter Physics
Hindawiwwwhindawicom Volume 2018
International Journal of
BiomaterialsHindawiwwwhindawicom
Journal ofEngineeringVolume 2018
Applied ChemistryJournal of
Hindawiwwwhindawicom Volume 2018
NanotechnologyHindawiwwwhindawicom Volume 2018
Journal of
Hindawiwwwhindawicom Volume 2018
High Energy PhysicsAdvances in
Hindawi Publishing Corporation httpwwwhindawicom Volume 2013Hindawiwwwhindawicom
The Scientific World Journal
Volume 2018
TribologyAdvances in
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
ChemistryAdvances in
Hindawiwwwhindawicom Volume 2018
Advances inPhysical Chemistry
Hindawiwwwhindawicom Volume 2018
BioMed Research InternationalMaterials
Journal of
Hindawiwwwhindawicom Volume 2018
Na
nom
ate
ria
ls
Hindawiwwwhindawicom Volume 2018
Journal ofNanomaterials
Submit your manuscripts atwwwhindawicom
deformation may take place in the asperity during loadingWhen the pushing coefficient is greater than 01954 theasperity begins to enter the second elastoplastic de-formation the relation between contact area and contactload is fsima10977 approximately When n 45 and thepushing coefficient is greater than 0472 the asperity beginsto enter fully plastic deformation the relation betweencontact area and contact load is fsima approximately
Figure 9 shows that when the minimum frequency ex-ponent is 20 and the maximum value is 32 the actual contactarea of the joint interface increases with the increase of thetotal contact load and the relation between them isFlowastr simAlowast15
r approximately During the whole deformationprocess the joint interface appears to be of elastic property
Figure 10 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loading
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash9
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
10ndash10
D = 11 n = 34D = 13 n = 34
D = 15 n = 34D = 17 n = 34
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(a)C
onta
ct ar
eas o
f a si
ngle
aspe
rity
(am
2 )
10ndash10
10ndash15
10ndash14
10ndash13
10ndash12
10ndash11
n = 32 D = 15n = 33 D = 15
n = 34 D = 15n = 35 D = 15
25 times 109 30 times 109 35 times 109 40 times 109 45 times 109 50 times 109 55 times 109
Limit mean geometric hardness in the firstelastoplastic deformation regime HG1(Nm2)
(b)
Figure 6 e relationship between limit mean geometric hardness and contact for single asperity during the first elastoplastic deformationstage (a) n 34 11leDle 17 (b) D 15 32le nle 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash12
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
10ndash13
D = 11 n = 40D = 13 n = 40
D = 15 n = 40D = 17 n = 40
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(a)
50 times 109 55 times 109 60 times 109 65 times 109 70 times 109 75 times 109
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
10ndash10
10ndash11
10ndash12
10ndash13
10ndash18
10ndash17
10ndash16
10ndash15
10ndash14
n = 36 D = 15n = 38 D = 15
n = 40 D = 15n = 42 D = 15
Limit mean geometric hardness in the secondelastoplastic deformation regime HG2(Nm2)
(b)
Figure 7 e relationship between limit mean geometric hardness and contact for single asperity during the second elastoplastic de-formation stage (a) n 40 11leDle 17 (b) D 15 36le nle 42
10 Advances in Materials Science and Engineering
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
CorrosionInternational Journal of
Hindawiwwwhindawicom Volume 2018
Advances in
Materials Science and EngineeringHindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Journal of
Chemistry
Analytical ChemistryInternational Journal of
Hindawiwwwhindawicom Volume 2018
ScienticaHindawiwwwhindawicom Volume 2018
Polymer ScienceInternational Journal of
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Advances in Condensed Matter Physics
Hindawiwwwhindawicom Volume 2018
International Journal of
BiomaterialsHindawiwwwhindawicom
Journal ofEngineeringVolume 2018
Applied ChemistryJournal of
Hindawiwwwhindawicom Volume 2018
NanotechnologyHindawiwwwhindawicom Volume 2018
Journal of
Hindawiwwwhindawicom Volume 2018
High Energy PhysicsAdvances in
Hindawi Publishing Corporation httpwwwhindawicom Volume 2013Hindawiwwwhindawicom
The Scientific World Journal
Volume 2018
TribologyAdvances in
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
ChemistryAdvances in
Hindawiwwwhindawicom Volume 2018
Advances inPhysical Chemistry
Hindawiwwwhindawicom Volume 2018
BioMed Research InternationalMaterials
Journal of
Hindawiwwwhindawicom Volume 2018
Na
nom
ate
ria
ls
Hindawiwwwhindawicom Volume 2018
Journal ofNanomaterials
Submit your manuscripts atwwwhindawicom
of the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 20and 36When the pushing coefficient k is 01648 the asperitybegins to be subject to the first elastoplastic deformation andthe relation between dimensionless total real contact areaand the dimensionless total contact loading is FlowastrsimAlowast15
r
approximately e joint interface appears to be of elasticproperty As the load continues increasing when thepushing coefficient k is 05564 at this pointFlowastr gt 69023 times 10minus3 the relation between above load and areais approximately FlowastrsimAlowast11093
r e joint interface presentselastoplastic properties At this time the first elastoplasticdeformation takes place in these asperities whose frequencyexponents range 33sim36
Figure 11 shows the relation between dimensionless totalreal contact area and the dimensionless total contact loadingof the joint interface when minimum value and maximumvalue of frequency exponent of asperities are respectively 44and 50When the pushing coefficient k is 00621 the asperity
begins to be subject to the second elastoplastic deformationat this point 00016ltFlowastr lt 0023 and the relation betweendimensionless total real contact area and the dimensionlesstotal contact loading is FlowastrsimAlowast10977
r approximately Whenthe pushing coefficient k is 07076 the asperity begins to besubject to the fully plastic deformation at this pointFlowastr gt 0023 and the relation between dimensionless total realcontact area and the dimensionless total contact loading isapproximately FlowastrsimAlowastr
5 Conclusions
(1) e contact mechanical properties of a single as-perity on a joint interface are related to the frequencyexponent of the asperity while the frequency ex-ponent of an asperity is related to the fractal di-mension and the profile scale parameter In thispaper the critical frequency exponents of each de-formation stage of a single asperity are obtained and
000 005 010 015 020 025 030 03500
10 times 10ndash11
20 times 10ndash11
30 times 10ndash11
40 times 10ndash11
50 times 10ndash11
60 times 10ndash11
Contact load of a single asperity (fN)
n = 30
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
(a)
Contact load of a single asperity (fN)
n = 35
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
50
times10
ndash5
10
times10
ndash4
104 times 10ndash4
10 times 10ndash13
80 times 10ndash14
60 times 10ndash14
40 times 10ndash14
20 times 10ndash14
363 times 10ndash14
15
times10
ndash4
20
times10
ndash4
25
times10
ndash4
30
times10
ndash4
35
times10
ndash400
00
(b)
Contact load of a single asperity (fN)
n = 40
Con
tact
area
s of a
sing
le as
perit
y (a
m2 )
4 times 10ndash17
3 times 10ndash17
2 times 10ndash17
1 times 10ndash17
0
20
times10
ndash8
40
times10
ndash8
60
times10
ndash8
80
times10
ndash8
10
times10
ndash700
(c)
Figure 8 e relationship between contact load and contact area of a single asperity during loading
Advances in Materials Science and Engineering 11
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
CorrosionInternational Journal of
Hindawiwwwhindawicom Volume 2018
Advances in
Materials Science and EngineeringHindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Journal of
Chemistry
Analytical ChemistryInternational Journal of
Hindawiwwwhindawicom Volume 2018
ScienticaHindawiwwwhindawicom Volume 2018
Polymer ScienceInternational Journal of
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Advances in Condensed Matter Physics
Hindawiwwwhindawicom Volume 2018
International Journal of
BiomaterialsHindawiwwwhindawicom
Journal ofEngineeringVolume 2018
Applied ChemistryJournal of
Hindawiwwwhindawicom Volume 2018
NanotechnologyHindawiwwwhindawicom Volume 2018
Journal of
Hindawiwwwhindawicom Volume 2018
High Energy PhysicsAdvances in
Hindawi Publishing Corporation httpwwwhindawicom Volume 2013Hindawiwwwhindawicom
The Scientific World Journal
Volume 2018
TribologyAdvances in
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
ChemistryAdvances in
Hindawiwwwhindawicom Volume 2018
Advances inPhysical Chemistry
Hindawiwwwhindawicom Volume 2018
BioMed Research InternationalMaterials
Journal of
Hindawiwwwhindawicom Volume 2018
Na
nom
ate
ria
ls
Hindawiwwwhindawicom Volume 2018
Journal ofNanomaterials
Submit your manuscripts atwwwhindawicom
the deformation characteristics of the asperity underdifferent frequency exponents are obtained
(2) e normal contact load of a single asperity in theelastoplastic stage is related to the hardness of thematerial When the material yields the hardness H isnot a constant but a function related to the amountof deformation In this paper the limit mean geo-metric hardness is introduced to express the normalcontact load of a single asperity in the first andsecond elastoplastic deformation stages consideringthe change of hardness
(3) e relationship between the contact load andcontact area of a single asperity in the first andsecond elastoplastic deformation stages considering
the change of material hardness and not consideringthe change of hardness is compared respectivelyWhen the contact area of the asperity is the same thecontact load with the change of hardness is smallerthan that without the change of hardness and thedifference between them increases with the increaseof deformation
(4) e limit mean geometric hardness of a single as-perity is related to the contact area fractal di-mension and frequency exponent during theelastoplastic deformation stage and the limit meangeometric hardness increases with the increase of thecontact area When the frequency exponent isconstant the relationship between the limit meangeometric hardness and the contact area of the as-perity is related to the fractal dimension e largerthe fractal dimension is the more obvious the re-lationship curve between them is When the fractaldimension is constant the relationship between thelimit mean geometric hardness of the asperity andthe contact area is related to the frequency exponente smaller the frequency exponent is the moreobvious the change of the curve is
(5) e relationship between dimensionless total realcontact area and the dimensionless total contactloading of joint interface at each deformation stageis obtained by introducing the pushing coefficientand the critical pushing coefficient exists Whenthe pushing coefficient exceeds this value someasperities begin to deform in the next stage andthe inflection point appears on the relationshipcurve
(6) e current model still has some limitations on theapplicable scope of materials and further researchand improvement are needed to make it more ap-plicable in the future
09
08
07
06
05
04
03
02
01
000000 0002 0004 0006 0008 0010 0012 0014
Nondimensional total contact load (Flowastr)
Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
nmin = 20 nmax = 36
Figure 10 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for20le nle 36
10
09
08
07
06
05
04
03
02
01Non
dim
ensio
nal t
otal
cont
act a
rea (
Alowastr)
000000 0005 0010 0015 0020 0025 0030 0035
Nondimensional total contact load (Flowastr)
nmin = 44 nmax = 50
Figure 11 e relationship between dimensionless total realcontact area and the dimensionless total contact loading for44le nle 50
10
09
08
07
06
05
04
03
02
01
Nondimensional total contact load (Flowastr1)
Non
dim
ensio
nal t
otal
real
cont
act a
rea (
Alowastr1
)
0000 10 times 10ndash3 20 times 10ndash3 30 times 10ndash3 40 times 10ndash3 50 times 10ndash3
nmin = 20 nmax = 32
Figure 9e relationship between dimensionless total real contactarea and the dimensionless total contact loading for 20le nle 32
12 Advances in Materials Science and Engineering
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
CorrosionInternational Journal of
Hindawiwwwhindawicom Volume 2018
Advances in
Materials Science and EngineeringHindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Journal of
Chemistry
Analytical ChemistryInternational Journal of
Hindawiwwwhindawicom Volume 2018
ScienticaHindawiwwwhindawicom Volume 2018
Polymer ScienceInternational Journal of
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Advances in Condensed Matter Physics
Hindawiwwwhindawicom Volume 2018
International Journal of
BiomaterialsHindawiwwwhindawicom
Journal ofEngineeringVolume 2018
Applied ChemistryJournal of
Hindawiwwwhindawicom Volume 2018
NanotechnologyHindawiwwwhindawicom Volume 2018
Journal of
Hindawiwwwhindawicom Volume 2018
High Energy PhysicsAdvances in
Hindawi Publishing Corporation httpwwwhindawicom Volume 2013Hindawiwwwhindawicom
The Scientific World Journal
Volume 2018
TribologyAdvances in
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
ChemistryAdvances in
Hindawiwwwhindawicom Volume 2018
Advances inPhysical Chemistry
Hindawiwwwhindawicom Volume 2018
BioMed Research InternationalMaterials
Journal of
Hindawiwwwhindawicom Volume 2018
Na
nom
ate
ria
ls
Hindawiwwwhindawicom Volume 2018
Journal ofNanomaterials
Submit your manuscripts atwwwhindawicom
Nomenclature
ωn Interference of the asperityωnec Elastic critical interference of the asperityωnepc First elastoplastic critical interference of the
asperityωnpc Second elastoplastic critical interference of the
asperityan Contact area of the asperityanec Elastic critical contact area of the asperityanepc First elastoplastic critical contact area of the
asperityanpc Second elastoplastic critical contact area of the
asperityfne Normal load in the elastic deformation of a single
asperityfnec Normal contact load for ω ωnecfnep1 Normal contact load of a single asperity in the
first elastoplastic stagefnep2 Normal contact load of a single asperity in the
second elastoplastic stagefnp Normal contact load of a single asperity in the full
plastic deformation stagefnep1prime Normal contact load of a single asperity in the
first elastoplastic stage considering the change ofhardness
fnep2prime Normal contact load of a single asperity in thesecond elastoplastic stage considering the changeof hardness
HG1(an) Limit mean geometric hardness in the firstelastoplastic deformation stage
HG2(an) Limit mean geometric hardness in the secondelastoplastic deformation stage
nec Elastic critical frequency exponentnepc First elastoplastic critical frequency exponentnpc Second elastoplastic critical frequency exponentAr Actual contact area of the joint interfaceAr1 Actual contact area of the joint interface for
nmin lt nle necAr2 Actual contact area of the joint interface for
nec lt nle nepcAr3 Actual contact area of the joint interface for
nepc lt nle npcAr4 Actual contact area of the joint interface for
npc lt n
Fr1 Actual contact load of the joint interface fornmin lt nle nec
Fr2 Actual contact load of the joint interface fornec lt nle nepc
Fr3 Actual contact load of the joint interface fornepc lt nle npc
Fr4 Actual contact load of the joint interface fornpc lt n
pea(a) Average contact pressure of the asperity in elasticstage
pepa1(a) Average contact pressure of the asperity in thefirst elastoplastic deformation stage
pepa2(a) Average contact pressure of the asperity in thesecond elastoplastic stage
Data Availability
e data used to support the findings of this study areavailable from the corresponding author upon request
Conflicts of Interest
e authors declare that they have no conflicts of interest
Acknowledgments
is work was supported by the National Natural ScienceFoundation of China (grant no 51275328) and the NaturalScience Foundation Project of Shanxi Province (grant no201601D011062)
References
[1] B Zhao S Zhang P Wang and Y Hai ldquoLoading-unloadingnormal stiffness model for power-law hardening surfacesconsidering actual surface topographyrdquo Tribology In-ternational vol 90 pp 332ndash342 2015
[2] J Greenwood and J Williamson ldquoContact of nominally flatsurfacesrdquo Mathematical Physical and Engineering Sciencesvol 295 no 1442 pp 299ndash319 1966
[3] J A Greenwood and J H Tripp ldquoe contact of twonominally flat rough surfacesrdquo Proceedings of the Institution ofMechanical Engineers vol 185 no 1 pp 625ndash633 1970
[4] W R Chang I Etsion and D B Bogy ldquoAn elastic-plasticmodel for the contact of rough surfacesrdquo Journal of Tribologyvol 109 no 2 pp 257ndash263 1987
[5] Y Zhao D M Maietta and L Chang ldquoAn asperity micro-contact model incorporating the transition from elastic de-formation to fully plastic flowrdquo Journal of Tribology vol 122no 1 pp 86ndash93 2000
[6] L Kogut and I Etsion ldquoElastic-plastic contact analysis ofasphere and a rigid flatrdquo Journal of Applied Mechanics vol 69no 5 pp 657ndash662 2002
[7] I Etsion Y Kligerman and Y Kadin ldquoUnloading of anelastic-plastic loaded spherical contactrdquo International Journalof Solids and Structures vol 42 no 13 pp 3716ndash3729 2005
[8] Y Kadin Y Kligerman and I Etsion ldquoUnloading an elastic-plastic contact of rough surfacesrdquo Journal of the Mechanicsand Physics of Solids vol 54 no 12 pp 2652ndash2674 2006
[9] Y Kadin Y Kligerman and I Etsion ldquoMultiple loading-unloading of an elastic-plastic spherical contactrdquo In-ternational Journal of Solids and Structures vol 43 no 22-23pp 7119ndash7127 2006
[10] A Majumdar and B Bhushan ldquoRole of fractal geometry inroughness characterization and contact mechanics of sur-facesrdquo Journal of Tribology vol 112 no 2 pp 205ndash216 1990
[11] A Majumdar and C L Tien ldquoFractal characterization andsimulation of rough surfacesrdquo Wear vol 136 no 2pp 313ndash327 1990
[12] AMajumdar and B Bhushan ldquoFractal model of elastic-plasticcontact between rough surfacesrdquo Journal of Tribology vol 113no 1 pp 1ndash11 1991
[13] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regimePart I-elastic contact and heat transfer analysisrdquo Journal ofTribology vol 116 no 4 pp 812ndash822 1994
[14] S Wang and K Komvopoulos ldquoA fractal theory of the in-terfacial temperature distribution in the slow sliding regime
Advances in Materials Science and Engineering 13
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
CorrosionInternational Journal of
Hindawiwwwhindawicom Volume 2018
Advances in
Materials Science and EngineeringHindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Journal of
Chemistry
Analytical ChemistryInternational Journal of
Hindawiwwwhindawicom Volume 2018
ScienticaHindawiwwwhindawicom Volume 2018
Polymer ScienceInternational Journal of
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Advances in Condensed Matter Physics
Hindawiwwwhindawicom Volume 2018
International Journal of
BiomaterialsHindawiwwwhindawicom
Journal ofEngineeringVolume 2018
Applied ChemistryJournal of
Hindawiwwwhindawicom Volume 2018
NanotechnologyHindawiwwwhindawicom Volume 2018
Journal of
Hindawiwwwhindawicom Volume 2018
High Energy PhysicsAdvances in
Hindawi Publishing Corporation httpwwwhindawicom Volume 2013Hindawiwwwhindawicom
The Scientific World Journal
Volume 2018
TribologyAdvances in
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
ChemistryAdvances in
Hindawiwwwhindawicom Volume 2018
Advances inPhysical Chemistry
Hindawiwwwhindawicom Volume 2018
BioMed Research InternationalMaterials
Journal of
Hindawiwwwhindawicom Volume 2018
Na
nom
ate
ria
ls
Hindawiwwwhindawicom Volume 2018
Journal ofNanomaterials
Submit your manuscripts atwwwhindawicom
Part II-multiple domains elastoplastic contacts and appli-cationsrdquo Journal of Tribology vol 116 no 4 pp 824ndash8321994
[15] Y Morag and I Etsion ldquoResolving the contradiction of as-perities plastic to elastic mode transition in current contactmodels of fractal rough surfacesrdquo Wear vol 262 no 5-6pp 624ndash629 2007
[16] H Tian X Zhong and C Zhao ldquoOne loading model of jointinterface considering elastoplastic and variation of hardnesswith surface depthrdquo Journal of Mechanical Engineeringvol 51 no 5 pp 90ndash104 2015
[17] Y Yuan Y Cheng K Liu et al ldquoA revised Majumdar andBushan model of elastoplastic contact between rough sur-facesrdquo Applied Surface Science vol 425 pp 1138ndash1157 2017
[18] R S Sayles and T R omas ldquoSurface topography as anonstationary random processrdquo Nature vol 271 no 5644pp 431ndash434 1978
14 Advances in Materials Science and Engineering
CorrosionInternational Journal of
Hindawiwwwhindawicom Volume 2018
Advances in
Materials Science and EngineeringHindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Journal of
Chemistry
Analytical ChemistryInternational Journal of
Hindawiwwwhindawicom Volume 2018
ScienticaHindawiwwwhindawicom Volume 2018
Polymer ScienceInternational Journal of
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
Advances in Condensed Matter Physics
Hindawiwwwhindawicom Volume 2018
International Journal of
BiomaterialsHindawiwwwhindawicom
Journal ofEngineeringVolume 2018
Applied ChemistryJournal of
Hindawiwwwhindawicom Volume 2018
NanotechnologyHindawiwwwhindawicom Volume 2018
Journal of
Hindawiwwwhindawicom Volume 2018
High Energy PhysicsAdvances in
Hindawi Publishing Corporation httpwwwhindawicom Volume 2013Hindawiwwwhindawicom
The Scientific World Journal
Volume 2018
TribologyAdvances in
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Volume 2018
TribologyAdvances in
Hindawiwwwhindawicom Volume 2018
Hindawiwwwhindawicom Volume 2018
ChemistryAdvances in
Hindawiwwwhindawicom Volume 2018
Advances inPhysical Chemistry
Hindawiwwwhindawicom Volume 2018
BioMed Research InternationalMaterials
Journal of
Hindawiwwwhindawicom Volume 2018
Na
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Hindawiwwwhindawicom Volume 2018
Journal ofNanomaterials
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