problem 6-010
TRANSCRIPT
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EXAMPLE 6-010 - 1
EXAMPLE 6-010
LINK SUNY BUFFALO EIGHT-STORY BUILDING WITH RUBBER ISOLATORS
PROBLEM DESCRIPTION
This example is presented in Section 2, pages 5 through 23, of Scheller and
Constantinou 1999 (the SUNY Buffalo report). It is an eight-story building that
is seismically isolated using rubber bearings. The model is subjected to arecorded pair of scaled horizontal ground acceleration histories from the 1971San Fernando earthquake. SAP2000 results for superstructure displacements
relative to the isolation system, superstructure accelerations, and isolator forcesand deformations are compared with results obtained using the computerprogram 3D-BASIS-ME (see Tsopelas, Constantinou and Reinhorn 1994).
The SAP2000 model is shown in the figures on the following three pages. Thesuperstructure is modeled as a stick using linear link elements. The
superstructure stick connects joints 23 and 55 through 62. The floor masses are
concentrated at the eccentric joints, joints 46 through 54. Diaphragm constraintsare used at each floor level above the isolation system to connect the mass to the
superstructure. Only the Ux, Uy and Rz degrees of freedom are active for the
analysis. The superstructure is assumed to have 3% modal damping and theisolation system to have 0% modal damping.
Joints 1 through 45 define the location of the 45 rubber isolators in the model.Those joints are constrained to joint 46 using a body constraint. Joints 101 to 145
are in the same location as joints 1 through 45, respectively, and are fully
restrained (fixed to the ground). Zero-length link elements with rubber isolatorproperties connect joints 1 through 45 to joints 101 through 145. The properties
for all of the link elements in the model are presented in the section titled Link
Element Properties later in this example.
The SAP2000 model used in this verification example differs from that used in
the Scheller and Constantinou 1999 report as follows. First, this verification
example uses a linear link element for the stick superstructure rather than thedamper element used in the report. The linear link is a simpler and more
appropriate element to use, but it was not available when the report was written.
Second, this verification example uses the actual linear effective stiffness for theisolators, 6.55 kip/in, rather than the artificially small effective stiffness used in
the report. This item is explained in more detail in the section titled Linear
Effective Stiffness of Rubber Isolator Elements later in this example.
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EXAMPLE 6-010 - 2
GEOMETRY AND PROPERTIES
1, 101
Y
X
5, 1052 3 4
6 7 8 9 10
11 12 13 14 15
16 17 18 19 20
21 22 23, 123 24 25, 125
26 27 28 29 30
31 32 33 34 35
36 37 38 39 40
41, 141 42 43 44 45, 145
4 @ 20' = 80'
8@
20'=
160'
CG8'
46
Two joints at the same
location with a rubberisolator link element
connecting them, typical
for joints 1 through 45 and
101 through 145
Note: Joints 1
through 46 are
constrained using a
body constraint
Plan View at Isolator Level
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EXAMPLE 6-010 - 3
43,143 38,138 33,133 28,128 23,123 18,118 13,113 8,108 3,10346
47 55
48 56
49 57
50 58
51 59
52 60
53 61
54 62
Isolator Level
Level 1
Level 2
Level 3
Level 4
Level 5
Level 6
Level 7
Level 8
Y
Z
8'
8@
12'=9
6'
8 @ 20' = 160'
Longitudinal Section
Joints constrained asdiaphragm, typical atlevels 1 through 8
Linear link element typicalat each level for the stickrepresenting the buildingsuperstructure
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EXAMPLE 6-010 - 4
1, 101
23, 123
XY
Z
46
54
5, 105
41, 141
45, 145
62
2, 102
21, 121
25, 125
Active degrees of
freedom are Ux, Uyand Rz
Linear link element typical
at each level for the stick
representing the building
superstructure
Two joints at the same
location with a rubber
isolator link element
connecting them, typicalfor joints 1 through 45 and
101 through 145.
3, 103
43, 143
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EXAMPLE 6-010 - 5
ANALYSIS CASES USED
Three different analysis cases are run for this example. They are described in the
following table. It is important to note that the 3D-BASIS-ME model uses 3%modal damping for all modes associated with the superstructure. No modal
damping is associated with the isolation system in 3D-BASIS-ME.
Analysis Case Description
RITZ Modal analysis case for Ritz vectors. Ninety-nine modes
are requested. The program will automatically determinethat a maximum of twenty-seven modes are possible andthus reduce the number of modes to twenty-seven. The
starting vectors are Ux acceleration, Uy acceleration, and all
link element nonlinear degrees of freedom.
NLMHIST1 Nonlinear modal time history analysis case that uses themodes in the RITZ analysis case. This case includes 3%
modal damping in all modes, except that modes 1, 2 and 3,
which are the modes associated with the isolation system,are assigned 0% modal damping. See the section titled
Linear Effective Stiffness of Rubber Isolator Elementslater in this example for more information.
NLDHIST1 Nonlinear direct integration time history analysis case. This
case includes proportional damping, which is defined to
provide damping similar to, but not exactly the same as, thedamping for the modal time history. See the section titled
Proportional Damping for Direct Integration Time
History later in this example for more information.
Note that the inherent viscous damping in the superstructure, which is specifiedto be 3% of critical damping, is accounted for differently in 3D-BASIS-ME, the
nonlinear modal time history in SAP2000, and the nonlinear direct integration
time history in SAP2000. Thus, slight differences in the results for each of thethree time history analyses (one in 3D-BASIS-ME and two in SAP2000) are
expected.
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EXAMPLE 6-010 - 6
EARTHQUAKE RECORD
The following figures show the earthquake records used in this example. They
are the recorded pair of horizontal ground acceleration time histories from the
1971 San Fernando earthquake at station number 211. The earthquake recordsare provided in files named EQ6-010-trans.txt and EQ6-010-long.txt. Those files
have one acceleration value per line, in g. The acceleration values are provided at
an equal spacing of 0.02 second.
Inside SAP2000 each of the two components is multiplied by a factor of 2.345,
as described in the SUNY Buffalo report, and also by a factor of 386.22 toconvert from g to in/sec2. The recorded north and west components are applied in
the transverse and longitudinal directions of the model, respectively.
-0.15
-0.10
-0.05
0.00
0.05
0.10
0.15
0 5 10 15 20 25 30 35 40 45
Time (sec)
GroundAcceleration(g)
Ground Acceleration for Transverse (X) Direction
-0.10
-0.05
0.00
0.05
0.10
0.15
0 5 10 15 20 25 30 35 40 45
Time (sec)
GroundAc
celeration(g)
Ground Acceleration for Longitudinal (Y) Direction
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EXAMPLE 6-010 - 7
LINK ELEMENT PROPERTIES
This section presents the properties used for all of the link elements in the model.
All link elements in the model are oriented such that the positive local 1 axis is
parallel to the positive global Z axis, the positive local 2 axis is parallel to thepositive global X axis and the local 3 axis is parallel to the positive global Y axis.
The superstructure linear link elements have an effective stiffness, ke, and for theshear degrees of freedom, a distance from the J-end to the shear spring, DJ.
Properties are specified for the U2, U3 and R1 degrees of freedom.
Between the Isolator Level and Level 3 (Property Name LINST123)
ke U2 = 3401.8 k/inDJ U2 = 72 inke U3 = 3401.8 k/in
DJ U3 = 72 in
ke R1 = 3.996 E+09 k-in/radian
Between the Level 3 and Level 6 (Property Name LINST456)
ke U2 = 2551.3 k/inDJ U2 = 72 in
ke U3 = 2551.3 k/in
DJ U3 = 72 in
ke R1 = 2.997 E+09 k-in/radian
Between the Level 7 and Level 8 (Property Name LINST78)
ke U2 = 1700.9 k/inDJ U2 = 72 in
ke U3 = 1700.9 k/in
DJ U3 = 72 inke R1 = 1.998 E+09 k-in/radian
The rubber isolator link elements have a linear effective stiffness, ke, a nonlinearinitial stiffness, k, a nonlinear yield strength, Fy, and a post yield stiffness ratio, r.
See the following section titled Linear Effective Stiffness of Rubber IsolatorElements for more information about ke. Properties are specified for the U2, and
U3 degrees of freedom and the properties are the same for the two degrees offreedom. The rubber isolator property name is BILIN and its properties are:
ke = 6.55 k/in Fy = 12.8 k
k = 25.6k/in r = 0.1887
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EXAMPLE 6-010 - 8
LINEAR EFFECTIVE STIFFNESS OF RUBBER ISOLATOR ELEMENTS
This verification example uses the calculated linear effective stiffness, ke, of 6.55kip/in for the isolators. The SUNY Buffalo report used an artificially small
effective stiffness of 0.0001 kip/in in their SAP2000 model to match the 3D-
BASIS-ME results. The report further shows that when they used the actualisolator effective stiffness of 6.55 kip/in in their SAP2000 model, their SAP2000
results underestimated the 3D-BASIS-ME results.
The calculated isolator effective stiffness of 6.55 kips/in is the appropriate
value to use and, as shown in this verification example, leads to results thatmatch the 3D-BASIS-ME results when the SAP2000 model is made
essentially equivalent to the 3D-BASIS-ME model.
It is important to recognize that the 3D-BASIS-ME model has 3% modal
damping in the superstructure and no modal damping in the isolation system.
Thus, for the SAP2000 model to be essentially equivalent to the 3D-BASIS-MEmodel, it must have 3% damping in all modes, except for modes 1, 2 and 3,
which are dominated by the isolation system behavior. Thus, to be equivalent to
the 3D-BASIS-ME model, modes 1, 2 and 3 in the SAP2000 model must be
assigned 0% damping with all other modes assigned 3% damping.
The SUNY Buffalo report SAP2000 model underestimated the 3D-BASIS-MEresults when using a linear effective stiffness of 6.55 kip/in for the isolators
because the SAP2000 model had 3% damping in all modes, including modes 1, 2
and 3. Thus, the SAP2000 model was not equivalent to the 3D-BASIS-MEmodel.
When the SUNY Buffalo report SAP2000 model used a linear effective stiffnessof 0.0001 kip/in for the isolators, the results matched the 3D-BASIS-ME results.
Using 0.0001 kip/in effective stiffness for the isolators made the periods of the
isolated modes (modes 1, 2 and 3) 528, 512 and 435 seconds, respectively.
Noting that the entire earthquake duration is approximately 44 seconds, it isapparent that very little energy can be absorbed by modes 1, 2 and 3, thus making
the damping associated with them approximately 0%, which is consistent withthe 3D-BASIS-ME model.
Again, we recommend using the actual effective stiffness and adjusting themodal damping associated with the isolated modes, rather than using an
artificially small effective stiffness.
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EXAMPLE 6-010 - 9
Note that the preceding explanation is only relevant for the nonlinear modal timehistory analysis case. It is not relevant for the nonlinear direct integration time
history analysis case. The linear effective stiffness of the isolators is only used in
linear analysis cases. In this verification example, the only linear analysis case isthe modal analysis case, RITZ. Both the nonlinear modal time history and the
nonlinear direct integration time history analysis cases use the nonlinear
properties of the isolator, not the linear properties. However, the nonlinear modaltime history uses modes from the modal analysis case RITZ that are based on the
linear effective stiffness of the isolators. Thus, the nonlinear modal time history
analysis case is indirectly affected by the linear effective stiffness of the isolators,
whereas the nonlinear direct integration time history analysis case is unaffected
by the linear isolator properties.
PROPORTIONAL DAMPING FOR DIRECT INTEGRATION TIME HISTORY
The nonlinear direct integration time history analysis case NLDHIST1 uses massand stiffness proportional damping. For this analysis case the challenge is to
designate appropriate proportional damping that approximates 3% damping in all
modes, except the isolator modes (modes 1, 2 and 3), which are to have 0%damping. The isolator modes have periods of approximately 2 seconds, and the
superstructure periods range from approximately 0.06 to 0.60 second.
For this example, theproportional damping is
specified as stiffnessproportional damping
only. The mass coefficient
for the damping is setequal to zero and the
stiffness coefficient is set
equal to 0.0040. The solidline in the chart to the
right plots the resulting
proportional dampingused. The dashed lineshows a constant 3%
damping.
0
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
0.45
0.5
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6
Period (sec)
DampingRatio
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EXAMPLE 6-010 - 10
TECHNICAL FEATURES OF SAP2000 TESTED
Rubber isolator links Linear links Zero-length, two-joint link elements
Diaphragm constraints
Modal analysis for ritz vectors Nonlinear modal time history analysis
Nonlinear direct integration time history analysis
Generalized displacements
RESULTS COMPARISON
Independent results are obtained using the computer program 3D-BASIS-ME(see Tsopelas, Constantinou and Reinhorn 1994).
The eight figures shown on the following four pages plot results from 3D-
BASIS-ME and from the SAP2000 analysis case NLMHIST1 (nonlinear modal
time history). The results for SAP2000 analysis case NLDHIST1 (nonlinear
direct integration time history) are similar. The following plots are shown:
Level 8 X direction displacement relative to the isolation system Level 8 Y direction displacement relative to the isolation system
Level 8 rotation about Z relative to the isolation system Base shear in the X direction Level 3 absolute acceleration in the X direction
Level 3 absolute acceleration in the Y direction
Link 23 force-deformation in the X direction Link 23 force-deformation in the Y direction
In SAP2000, the level 8 displacements and rotations relative to the isolation
system are determined using generalized displacements. The generalized
displacements are defined to subtract the displacement or rotation at joint 23
from that at joint 62.
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EXAMPLE 6-010 - 11
-3.00
-2.50
-2.00
-1.50
-1.00
-0.50
0.00
0.50
1.00
1.50
2.00
2.50
3.00
3.50
4.00
0 5 10 15 20 25 30
Time (sec)
Level8Ux
Displacem
entRelativetoIsolationSystem(
in)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 8 Ux
Displacement Relative to Isolation System
-3.00
-2.50
-2.00
-1.50
-1.00
-0.50
0.00
0.50
1.00
1.50
2.00
2.50
3.00
3.50
4.00
0 5 10 15 20 25 30
Time (sec)
Level8Ux
Displacem
entRelativetoIsolationSystem(
in)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 8 Ux
Displacement Relative to Isolation System
-2.50
-2.00
-1.50
-1.00
-0.50
0.00
0.50
1.00
1.50
2.00
2.50
3.00
0 5 10 15 20 25 30
Time (sec)
Level8Uy
Displa
cementRelativetoIsolationSystem(
in)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 8 Uy Displacement Relative to Isolation System
-2.50
-2.00
-1.50
-1.00
-0.50
0.00
0.50
1.00
1.50
2.00
2.50
3.00
0 5 10 15 20 25 30
Time (sec)
yDispla
cementRelativetoIsolationSystem(
in)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 8 Uy Displacement Relative to Isolation System
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EXAMPLE 6-010 - 12
-0.0008
-0.0006
-0.0004
-0.0002
0.0000
0.0002
0.0004
0.0006
0.0008
0.0010
0 5 10 15 20 25 30
Time (sec)
Level8Rz
RotationRelativetoIsolationSystem(radians)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 8 Rz Rotation Relative to Isolation System
-0.0008
-0.0006
-0.0004
-0.0002
0.0000
0.0002
0.0004
0.0006
0.0008
0.0010
0 5 10 15 20 25 30
Time (sec)
Level8Rz
RotationRelativetoIsolationSystem(radians)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 8 Rz Rotation Relative to Isolation System
-2500
-2000
-1500
-1000
-500
0
500
1000
1500
2000
0 5 10 15 20 25 30
Time (sec)
BaseFx
(kip)
3D-BASIS-ME
SAP2000 NLMHIST1
Base Shear Fx
-2500
-2000
-1500
-1000
-500
0
500
1000
1500
2000
0 5 10 15 20 25 30
Time (sec)
BaseFx
(kip)
3D-BASIS-ME
SAP2000 NLMHIST1
Base Shear Fx
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EXAMPLE 6-010 - 13
-80
-60
-40
-20
0
20
40
60
80
0 5 10 15 20 25 30
Time (sec)
Level3UxA
bsoluteAcceleration(in/sec
2)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 3 Ux Absolute Acceleration
-80
-60
-40
-20
0
20
40
60
80
0 5 10 15 20 25 30
Time (sec)
Level3UxA
bsoluteAcceleration(in/sec
2)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 3 Ux Absolute Acceleration
-60
-40
-20
0
20
40
60
80
0 5 10 15 20 25 30
Time (sec)
Level3U
yAbsoluteAcceleration(in/sec
2)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 3 Uy Absolute Acceleration
-60
-40
-20
0
20
40
60
80
0 5 10 15 20 25 30
Time (sec)
Level3U
yAbsoluteAcceleration(in/sec
2)
3D-BASIS-ME
SAP2000 NLMHIST1
Level 3 Uy Absolute Acceleration
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EXAMPLE 6-010 - 14
-50
-40
-30
-20
-10
0
10
20
30
40
50
-7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8
Isolator 23 Ux Deformation (in)
Isolator23Fx
Force(kip)
3D-BASIS-ME
SAP2000 NLMHIST1
Isolator 23 Force-Deformation in the X Direction
-50
-40
-30
-20
-10
0
10
20
30
40
50
-7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8
Isolator 23 Ux Deformation (in)
Isolator23Fx
Force(kip)
3D-BASIS-ME
SAP2000 NLMHIST1
Isolator 23 Force-Deformation in the X Direction
-40
-30
-20
-10
0
10
20
30
40
-5 -4 -3 -2 -1 0 1 2 3 4 5 6 7
Isolator 23 Uy Deformation (in)
Isolator23Fy
Force(kip)
3D-BASIS-ME
SAP2000 NLMHIST1
Isolator 23 Force-Deformation in the Y Direction
-40
-30
-20
-10
0
10
20
30
40
-5 -4 -3 -2 -1 0 1 2 3 4 5 6 7
Isolator 23 Uy Deformation (in)
yForce(kip)
3D-BASIS-ME
SAP2000 NLMHIST1
Isolator 23 Force-Deformation in the Y Direction
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EXAMPLE 6-010 - 15
The following table compares the maximum and minimum values of the outputitems shown in the charts on the previous four pages. Results are compared for
both the modal time history analysis case, NLMHIST1, and the direct integration
time history analysis case, NLDHIST1.
OutputParameter
Dir andMax/Min
AnalysisCase SAP2000
Independent3D-BASIS-ME
PercentDifference
NLMHIST1 3.521 +1%UxMax
NLDHIST1 3.504
3.494
0%NLMHIST1 -2.875 +3%Ux
Min NLDHIST1 -2.911-2.804
+4%
NLMHIST1 2.642 +4%UyMax NLDHIST1 2.729
2.538+8%
NLMHIST1 -2.167 +7%
Level 8
displacement
relative toisolation system
(in)
UyMin NLDHIST1 -2.211
-2.029+9%
NLMHIST1 0.00080 +7%Rz
Max NLDHIST1 0.00077 0.00075 +3%
NLMHIST1 -0.00077 +1%
Level 8 rotationrelative to
isolation system
(rad)Rz
Min NLDHIST1 -0.00076-0.00076
0%
NLMHIST1 1854 +2%FxMax NLDHIST1 1873
1818+3%
NLMHIST1 -2109 +1%
Base shear in the
X direction
(kip) FxMin NLDHIST1 -2091
-20890%
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EXAMPLE 6-010 - 16
OutputParameter
Dir andMax/Min
AnalysisCase SAP2000
Independent3D-BASIS-ME
PercentDifference
NLMHIST1 65.76 -3%UxMax NLDHIST1 70.03
67.73+3%
NLMHIST1 -72.71 +2%UxMin NLDHIST1 -72.85
-71.47+2%
NLMHIST1 70.36 +8%UyMax NLDHIST1 61.60
64.96-5%
NLMHIST1 -58.35 +1%
Level 3 (jt 57)absolute
acceleration
(in/sec2)
UyMin NLDHIST1 -57.65
-57.780%
NLMHIST1 48.66 +1%FxMax NLDHIST1 48.18
48.170%
NLMHIST1 -43.55 +2%FxMin NLDHIST1 -43.54
-42.68+2%
NLMHIST1 36.65 +1%FyMax NLDHIST1 36.53
36.380%
NLMHIST1 -30.91 +1%
Isolator 23
shear force
(kip)
FyMin NLDHIST1 -30.78
-30.54+1%
NLMHIST1 7.935 +1%UxMax NLDHIST1 7.828
7.8450%
NLMHIST1 -6.916 +3%UxMin NLDHIST1 -6.905
-6.746+2%
NLMHIST1 6.247 +2%UyMax NLDHIST1 6.200
6.150+1%
NLMHIST1 -4.419 +3%
Isolator 23
deformation(in)
UyMin NLDHIST1 -4.400
-4.304+2%
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EXAMPLE 6-010 - 17
COMPUTER FILE: Example 6-010
CONCLUSION
The SAP2000 results show an acceptable comparison with the independentresults considering that SAP2000 and 3D-BASIS-ME use different modeling and
solution techniques for the isolated structure. The clearest comparison of results
is evident in the graphical comparisons.