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Problem Description

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  •  Three-dimensional analysis using shell elements
  •  Self weight applied to shell elements
  •  Gravity load applied to shell elements
  •  Uniform load applied to shell elements

Result Comparison

Output ParameterOpenBrIMSAP2000Independent

Percent Difference

(SAP2000 vs Independent)

Percent Difference

(OpenBrIM vs Independent)

Uz(jt49) ft-0.3072
-0.3068
-0.3086-1%
0.47%


AngleOutput ParameterOpenBrIMSAP2000Independent

Percent Difference

(SAP2000 vs Independent)

Percent Difference

(OpenBrIM vs Independent)

0Uy(jt1) ft
3e-5
0.00000.0004-3%-3%
6.67Uy(jt2) ft
0.0005
0.00050.0010-4%-4%
13.33Uy(jt3) ft
0.0018
0.00180.0021-2%-2%
20Uy(jt4) ft
0.0029
0.00290.0030-1%-1%
26.67Uy(jt5) ft
0.0024
0.00240.00212%2%
33.33Uy(jt6) ft-0.0017-0.0017-0.0025-6%-6%
40Uy(jt7) ft
-0.0118
-0.0118-0.0125-6%-6%

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AngleOutput ParameterOpenBrIMSAP2000Independent

Percent Difference

(SAP2000 vs Independent)

Percent Difference

(OpenBrIM vs Independent)

0Uz(jt43) ft
0.0463
0.0460.0004-1%-1%
6.67Uz(jt44) ft
0.0309
0.0310.0010+1%+1%
13.33Uz(jt45) ft
-0.0131
-0.0130.0021-1%-1%
20Uz(jt46) ft
-0.0786
-0.0780.0030-1%-1%
26.67Uz(jt47) ft
-0.1556
-0.1550.0021-1%-1%
33.33Uz(jt48) ft
-0.234
-0.234-0.0025-2%-2%

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