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International Journal of Civil Engineering and Technology (IJCIET) Volume 9, Issue 8, August 2018, pp. 771–780, Article ID: IJCIET_09_08_078
Available online at http://www.iaeme.com/ijciet/issues.asp?JType=IJCIET&VType=9&IType=8
ISSN Print: 0976-6308 and ISSN Online: 0976-6316
© IAEME Publication Scopus Indexed
EXPERIMENT INVESTIGATION OF FLEXURE
RIGIDITY OF GLUE LAMINATED TIMBER
BEAMS CONSISTING OF COCONUT WOOD
(COCOS NUCIFERA) AND SENGON WOOD
(ALBIZIA FALCATARA) BASED ON FOUR-
POINT BENDING TEST
Kusnindar*
Civil Engineering Department, Brawijaya University,
MT. Haryono street 167 Malang 65145 East Java, Indonesia
Civil Engineering Department, Tadulako University,
Soekarno-Hatta street km.9 Palu, Central of Sulawesi, Indonesia
Sri Murni Dewi
Civil Engineering Department, Brawijaya University,
MT. Haryono street 167 Malang 65145 East Java, Indonesia
Agoes Soehardjono
Civil Engineering Department, Brawijaya University,
MT. Haryono street 167 Malang 65145 East Java, Indonesia
Wisnumurti
Civil Engineering Department, Brawijaya University,
MT. Haryono street 167 Malang 65145 East Java, Indonesia
*Corresponding Author E-mail: [email protected]
ABSTRACT
This paper was intended to describe the performance of mix-glue laminated timber
beams (mix-glulam) compose of coconut wood (Cocos nucifera) and sengon wood
(Albizia falcatara) in the outer zone and core zone, respectively. Mix-glulam system is
an alternative to utilizing a low-grade timber as structural member of building.
Through the analysis of four-point-bending-test results of each of five mix-glulam
beams (BLG) and five sengon-solid beams (SDL) with span (L) = 2750 mm, height (d)
= 155 mm and width (b) = 55 mm was obtained that the mix-glulam system produces
a good performance. The analysis result showed that the flexural rigidity (EI) of BLG
is 1.66 times higher than SDL. Likewise, the maximum bending stress (σmax) of BLG is
Kusnindar, Sri Murni Dewi, Agoes Soehardjono and Wisnumurti
http://www.iaeme.com/IJCIET/index.asp 772 [email protected]
1.6 times higher than the σmax of SDL with tension failure in bending. Generally, the
failure of the beam that occurs is a brittle and sudden tension failure.
Key words: sengon wood (Albizia falcatara), coconut wood (Cocos nucifera), mix-
glulam, flexure rigidity, timber beam.
Cite this Article: Kusnindar, Sri Murni Dewi, Agoes Soehardjono and Wisnumurti,
Experiment Investigation of Flexure Rigidity of Glue Laminated Timber Beams
Consisting of Coconut Wood (Cocos Nucifera) and Sengon Wood (Albizia Falcatara)
Based on Four-Point Bending Test. International Journal of Civil Engineering and
Technology, 9(8), 2018, pp. 771-780.
http://www.iaeme.com/IJCIET/issues.asp?JType=IJCIET&VType=9&IType=8
1. INTRODUCTION
The potential availability of sengon wood (Albizia falcatara) and coconut wood (Cocos
nucifera) in Indonesia is very adequate. In 2013, there are approximately 64 million sengon
trees that can be harvested. This amount is equivalent to 13.9 million m3 of sawn timber [1].
In addition, the potential availability of coconut wood in Indonesia is also quite adequate.
This is a necessity of the extent of the Indonesian coconut plantation which is equivalent to
approximately 26% of the total coconut plantations in the world [2].
Unfortunately, sengon-wood and coconut-wood have not been widely used as structural
elements of building, because in both there are deficiencies in terms of mechanical and
physical properties. Sengon wood has a low-grade modulus of elasticity that is only about
3,881 MPa. While coconut wood has a high variation in the density. The low grade of the
modulus of elasticity causes the carrying capacity of the wood to be low, and the density
variation causes the limitations of sawn timber dimension to be obtained. Approximately only
one-third of the coconut trunk (35 cm diameter) can be utilized to produce good quality sawn
timber with an average elasticity modulus value of 11.414 MPa [2, 3].
In order to utilize sengon and coconut wood for structural elements of building, the mix-
glue laminated timber method can be considered. Mix-glue laminated timber beams is one
type of laminated timber structure product. Mix-glue laminated timber beams consists of two
or more species of timber with different mechanical properties. Timbers that have higher
mechanical properties are placed as outer lamination and vice versa as core elements of the
beam.
Glue lamiated timber (glulam) is still very competitive in modern construction material. In
terms of structural efficiency, the laminated wood can produce construction elements with
sufficient strength to density ratios. For example, the mix-glulam beam composed of
Eucalyptus grandis and Poplar laminations has a structural-efficiency value of 120 x 10-3
MPa.m3/ kg [4]. In this case the structural efficiency of timber structures is better than
concrete [5]. The use of a laminated wood system will produce a large construction elements,
regardless of the diameter of the tree. The cross-section depth of glulam beam is in principle
unlimited, but for the accomplished maximum depths are of the order of 2 m. The weakening
of structures caused by natural wood defects can also be reduced by a laminated wood system
[5].
Based on the above description, this research is aimed to determine the flexure rigidity
and strength of mix-glue laminated timber beam was compose of sengon and coconut wood.
In this case, sengon wood lamination is placed in the core zone of the beam and coconut wood
lamination in the outer zone.
Experiment Investigation of Flexure Rigidity of Glue Laminated Timber Beams Consisting of Coconut
Wood (Cocos Nucifera) and Sengon Wood (Albizia Falcatara) Based on Four-Point Bending Test
http://www.iaeme.com/IJCIET/index.asp 773 [email protected]
2. LITERATURE REVIEW
Mix-glue laminated timber beams of hardwood timber were composed of 50% of lower grade
lamination in the core zone and 50% of high-grade lamination in the outer zone can produce a
bending strength and stiffness is 16.5 MPa and 12.4 GPa, respectively. This suggests that the
mix-glue laminated timber beam design with this proportion is technically feasible to
implement [6].
Poplar and spruce combinations as mixed-glulam beams result in a more flexible or
pseudo-ductile behavior than individual poplar beams. Based on the load and deformation
relationships, the mix-glulam beams has a plastic behavior till failure [7]. Similarly, the
combination of poplar-larch and poplar-spruce. Both combinations have higher ductility
compared to solid poplar beams, which are 48% and 64% respectively. So, the performance of
mix-glulam-beams is determined by the mechanical properties of the wood species used,
especially the outer zone lamina [8]. Since the ductility of the structure is very advantageous,
it is appropriate that the structural system is designed to behave in a ductile manner. As stated
by [9] that ductility of timber beams can be improved by application of external fiber
reinforcement. This retrofitting method is easy to implement and at the same time reduces the
risk of failure due to defects.
Furthermore, the mix-glue laminated timber beam which is a combination of poplar and
eucalyptus was produced a higher strength and modulus of elasticity than individual poplar
beams. Modulus of elasticity of the mixed-glulam beams is 51% higher than the individual
poplar beam. Likewise, the flexural strength of the mixed-glulam beams was increased by
35% compared to the solid-poplar beams. In this case, poplar wood is placed in the core
lamination and eucalyptus as the outermost lamination, [4].
3. MATERIAL AND METHOD
3.1. Timber and Adhesive
The initial dimensions, mechanical properties and number of lumber prepared for the beam
manufacture are presented in Table 1. Both lumber materials were obtained from sawmills
industry in Malang, East Java, Indonesia. Before use, both are dried for about three months to
achieve air-dry conditions, ie at ± 12% of moisture content. The physical and mechanical
properties of them are obtained from the clear-specimens test according to [10].
Table 1 Mechanical properties of sengon and coconut wood
Properties in 12% of moisture content Sengon Wood Coconut Wood
Modulus of Elasticity (E12) 3881 MPa 10830 MPa
Modulus of Rupture (MOR12) = 20 MPa 20 MPa 39 MPa
Density (ρ12) 0.29-0.32 gr/cm3 0.6 gr/cm
3
Initial dimension :
width 70 mm;
dept 180 mm; length
3250 mm
width 60 mm;
depth 120 mm; length
3250 mm
Number of the lumber trunks : 15 10
Especially for the manufacture of laminated-timber beams required additional material ie
adhesive. The adhesive used is specifically for wood, ie urea formaldehyde (UF) resin in the
form of ready-made powder. This adhesive specification as issued by the manufacturer is
presented in Table 2.
Kusnindar, Sri Murni Dewi, Agoes Soehardjono and Wisnumurti
http://www.iaeme.com/IJCIET/index.asp 774 [email protected]
Table 2 Properties of adhesive
Material Material Properties
Urea Formaldehyde Adhesive (UF)
shear strength of glue line = 45 kg/in2
Gelatin time = 5 hours
spreading ability = 2 m2/ kg
3.2. Geometry and the Beams Dimensions
The specimen consists of two series, namely sengon-wood solid beams (SDL) and glulam-
mixed beams (BLG). The dimensions and geometry of the cross-section of each beam are
presented in Table 3 and Figure 1. To ensure flexural failure without lateral buckling during
testing, it was determined that the high to span ratio of more than 14.0 [11] and the height to
width ratio less than 3.0 [12].
Tabel 3 The beams dimension.
Beams
Series
Number
of specimen
b
(mm)
d
(mm)
L
(mm) L/d d/b
SDL 5 55 155 2750 18 2.8
BLG 5 55 155 2750 18 2.8
Figure 1 Cross section of the beams
3.3. Beams Fabrication
The SDL series manufactured starts from the selection of five previously prepared sengon-
wood trunk as shown in Table 1. To ensure uniformity of density, a relatively similar weight
of sengon-wood trunk is selected. The sengon-wood trunk is then cut and finishing with a
planer machine until the net dimensions are reached as Table 3. Then each beam is labeled
SDL-1, SDL-2, SDL-3, SDL-4, and SDL-5. The total length of all the beams is made equal to
the length of the span (L) plus 0.5d to provide the placement area at the support during the test
[13].
Furthermore, the BLG manufactured starts from the preparation of lamination from the
source material as in the Table 1. The coconut-wood lamination will be made from six sawn
lumber. The six sawn lumber were subsequently cut into 24 sheets of board. Each of the board
has a thickness of 30 mm, width 60 mm and length 3250 mm. Each board was then leveling
with a planer machine so as to achieve a net of thickness is 26 mm. It also produces a cleaned
surface from dirt that can inhibit the gluing process. After obtaining 24 pieces of coconut-
wood lamination ready for use then selected 10 sheets of laminations that has a uniform
density of approximately 0.6 gr/cm3 (Figure 2).
For the preparation of sengon-wood laminations, the process is the same as the coconut-
wood lamination, only different amount. Seven sengon-wood sawn timber were used and
b
d
a. SDL
1
b
d
b. BLG
2
3
3
2
1
Legend:
a) Solid sengon wood beams (SDL)
b) Mix-glulam beams (BLG)
1 = coconut wood lamination (ρ12 = 0.6 gr/cm3)
2 = sengon wood lamination (ρ12 = 0.32 gr/cm3)
3 = sengon wood lamination (ρ12 = 0.29 gr/cm3)
∆d = lamnation tickness (26 mm)
∆d
Experiment Investigation of Flexure Rigidity of Glue Laminated Timber Beams Consisting of Coconut
Wood (Cocos Nucifera) and Sengon Wood (Albizia Falcatara) Based on Four-Point Bending Test
http://www.iaeme.com/IJCIET/index.asp 775 [email protected]
produce 10 laminations having density ± 0.29 gr / cm3 and 10 laminations having density ±
0.32 gr/cm3 as Figure 2. The sengon and coconut wood laminations are then grouped
according to the beam formation to be made. The density uniformity control is necessary
because it determines the mechanical properties of wood in general, although there is a natural
wood factor that also determines [14].
Figure 2 Laminations are ready to be glued, pressure and clamping of the beams
The adhesive application was carried out using a manual brush spreader and the average
amount of 350 g/m2 [4]. The adhesive composition according to the manufacturer's
specifications is 0.5 kg water: 1kg UF-powder. Furthermore, the lamination arrangement is
given 2MPa pressure. This pressure is applied at 25 cm intervals along the beam as in Figure
2. After pressing at each point, immediately vertical steel clamps are fixed at that point and
attached for approximately 18 hours. The final process of mix-glulam beams fabrication is the
leveling of two sides of the beams to obtain a net width of 55 mm. These processes are not
applied on the top and bottom side of the beam, as it has been obtained 155 mm hight.
3.4. Method of Testing and Data Analysis
3.4.1. Test Methods
To evaluate the flexural rigidity and bending strength of the timber beams, four-point bending
tests were used as shown in Figure 4. In this test was recorded the load and deflection data of
each beam at three locations in the pure bending area [13]
Figure 4 Apparatus configuration of four-point bending test
3.4.2. Analisis of Moment-curvature Diagram
The load-deformation diagram of each beam is obtained by plotting of moment and curvature.
The curvature value is determined based on the experimental deflection data. The calculation
can use Equation 1 was refers to the beam theory.
κ � 2. ��2 � ��1��32� . s�2 (1)
Where:
κ = mid-span curvature of beam (mm-1
)
Kusnindar, Sri Murni Dewi, Agoes Soehardjono and Wisnumurti
http://www.iaeme.com/IJCIET/index.asp 776 [email protected]
δ1 = deflection of LVDT-1 (mm)
δ2 = deflection of LVDT-2 (mm)
δ3 = deflection of LVDT-3 (mm)
s = distance between points of loading (mm)
Based on the moment-curvature diagram, then determined the value of elastic moment
(Me), elastic curvature (κe), maximum moment (Mmax) and maximum curvature (κmax). The
procedure of determining these magnitude value involves the initial deformation, elastic
deformation contribution, and permanent deformations [15]. On the other hand, the
determination of flexure rigidity (EI) and the bending strength (σmax) of each beam is based
on the beam theory using Equation 2 and 3 [16]. Furthermore, the ductility of beams is
determined using Equation 4 [3].
EI � P'.a
24.� �3L2-4a2� (2)
�max � 3Pmax . a
b . d2 (3)
μκ� κmaxκe
(4)
Where:
EI = flexure rigidity of beams (N.mm2)
P’ = linier stage load (0.4Pmax – 0.1Pmax) [15]
δ' = linier stage deflection at mid span (0.4δmax – 0.1δmax) [15]
a = distance between loading point to support (mm)
σmax = bending stresses of beam (MPa)
Pmax = maksimum load ( N )
L, b, d = span, width and depth of beams (mm)
µκ = curvature ductility
κmax = maximum curvature (mm-1
)
κe = limit of linear curvature (mm-1
)
4. RESULT AND DISCUSSION
4.1. Mechanical Parameters of Beams
The mechanical parameters of beams are determined based on the moment-curvature diagram
as Figure 5, Table 4 and Table 5. The moment-curvature diagram of each beam always begins
with a linear stage up to the elastic limit. This elastic load limit is further expressed by Me.
The experimental results show that the mean of elastic moments of mix-glulam beams (BLG)
and sengon solid beams (SDL) are 5.977 kN.m and 2.848 kN.m, respectively. This shows that
the elastic moment of mix-glulam beams is 2.25 times higher than the solid sengon beams.
Experiment Investigation of Flexure Rigidity of Glue Laminated Timber Beams Consisting of Coconut
Wood (Cocos Nucifera) and Sengon Wood (Albizia Falcatara) Based on Four-Point Bending Test
http://www.iaeme.com/IJCIET/index.asp 777 [email protected]
Figure 5 The moment-curvature diagram at mid-span of beams
Similar to bending moment, the experimental results also show that the flexure rigidity of
mix-glulam beams is also higher than the solid sengon beam. Flexure rigidity of each beam is
represented by the tangent of the moment-curvature diagram in the linear stage as Figure 5. In
this case, the average flexure rigidity of mix glulam beams is 1.66 times higher than the solid
sengon beam.
Table 4 Bending test result of solid sengon-wood beams.
Name of
Beams
EI Mmax σσσσmax κκκκmax/κκκκe Failure Mode x10
11 N.mm
2 kN.m MPa
SDL-1 1.466 4.145 21 4.270 Tension
SDL-2 1.536 5.317 23 2.773 Tension
SDL-3 1.029 4.804 25 2.951 Tension
SDL-4 1.107 2.425 12 1.419 Premature tension
SDL-5 0.525 4.913 24 2.211 Tension
Average 1.133 4.321 23.19 2.7 -
Table 5 Bending test result of mix-glulam beams
Name of
Beams
EI Mmax σσσσmax κκκκmax/κκκκe Failure Mode x10
11 N.mm
2 kN.m Mpa
BLG-1 1.264 8.018 35 2.431 Tension
BLG-2 1.432 7.073 30 1.810 Tension
BLG-3 2.668 7.912 40 1.048 Compression at load point
BLG-4 2.262 6.846 43 1.298 Tension
BLG-5 1.772 8.027 36 1.827 Tension
Average 1.879 7.575 36.8 1.7 -
After the limit of linear deformation is reached, the next deformation switches to a
nonlinear stage. This nonlinear deformation continues until the failure of the beam. This
becomes an indication that there has been a nonlinear stress in the compression zone [17] as
well as describing the ductility of the beam (κmax/κe) [3]. Ductility of sengon wood solid
beams is 1.6 times higher than mix-glulam beams. But in terms of a bending moment
achievement, it appears that the performance of mix-glulam beams is much better than sengon
solid beams. The average of the maximum value of bending moment of mix glulam beams is
1.75 times higher than the sengon solid beams.
Me
0
2
4
6
8
10
0 20 40 60 80 100
M (
kN
-m)
κ (x 10-6 mm-1)
SDL-1
SDL-2
SDL-3
SDL-4
SDL-5
Me
0
2
4
6
8
10
0 20 40 60 80 100
M (
kN
-m)
κ (x 10-6 mm-1)
BLG-1
BLG-2
BLG-3
BLG-4
BLG-5
Kusnindar, Sri Murni Dewi, Agoes Soehardjono and Wisnumurti
http://www.iaeme.com/IJCIET/index.asp 778 [email protected]
Regarding the bending strength of the beam expressed by the maximum bending stress
(σmax), the mix-glulam beam has a better performance than the solid sengon beams. The
average of bending strength of mix-glulam beams and sengon solid beams are 36.8 MPa and
23.19 MPa, respectively, or it can be stated that the bending strength of the mix-glulam beams
is 1.6 times higher than the solid sengon beams.
4.2. Failure Mechanism of Beams
The SDL beams failure is characterized by a rupture on the tension side as shown in Figure 6.
This tensile failure is brittle and occurs suddenly. This corresponds to the nature of wood in
response to tensile stress. Cracks in the tensile side will then propagate toward the neutral axis
of the beam. This failure is identified at a time when the moment-curvature diagram begins to
switch to a non-linear stage. This means that the compression stress of the beam begins to be
a plastic stage, but the maximum compressive stress has not been reached. Such failure is
categorized as a second mode of failure [17].
Figure 6 Typical failure of SDL beams
In SDL-4 beams premature tensile failure occurred. The tensile failure is achieved at a low
magnitude of bending moment, and the value is less than the average of linear bending
moment limit of the SDL group. Premature failure is caused by defects in the wood caused by
insects attack (Figure 6). This defect is not detected when sorting from the material because it
is located inside the beam. This is one of the disadvantages of using wood for construction in
solid timber.
The BLG beams failure is characterized by a rupture on the tension side in the coconut
wood lamination. Furthermore, the crack propagation occurs horizontally following the fiber
orientation after it reaches the sengon wood lamination. At this time the total failure has
occurred. This total failure is suddenly with high damage intensity as shown in Figure 8.
However, different modes of failure occur on BLG-3. This beam failed at the contact-point
with the load spread. This failure mode is reached before the compression stress switches to a
nonlinear stage like Figure 9.
Figure 8 Typical failure of BLG beams
Experiment Investigation of Flexure Rigidity of Glue Laminated Timber Beams Consisting of Coconut
Wood (Cocos Nucifera) and Sengon Wood (Albizia Falcatara) Based on Four-Point Bending Test
http://www.iaeme.com/IJCIET/index.asp 779 [email protected]
Figure 9 Local failure in the loading point contact of BLG-3
5. CONCLUSIONS
Mix-glulam beams consisting of one-third of the cross-sectional are coconut wood
laminations and the other two-thirds are wood-sengon laminations can produce a flexure
rigidity (EI) by 1.66 times higher than solid sengon wood beams. The placement of the
coconut wood laminations in the outermost of the glulam beams produces the bending
strength 1.6 times higher than the bending strength of the individual sengon beams. Although
there are consequences of decreasing the ductility index up to 40%. The failure mode that
occurs is similar for both types of beams. The failure mode that occurs in the form of sudden
tensile failure with crack propagation tends to adjust the fiber orientation.
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