VMR027-10A

VMR027-10A
2D Plane Stress - Biaxial (negative) Load Primary Creep

Test Description

A square of length L and height L is constrained in the Y-direction on the bottom edge and constrained in the X-direction on the left edge. A tensile distributed load, σ1, is applied on the right edge and a compressive distributed load, σ2, is applied to the top edge.

Geometic PropertiesMaterial PropertiesLoading
L = 100 mm
Boundary Conditions
Bottom Edge: uy = 0
Left Edge: ux = 0
E = 200 x 103 N/mm2
ν = 0.3
Creep Law: ε = Aσntm
n = 5
m = 0.5
Right Edge:
σ1 = 200 N/mm2
Top Edge:
σ2 = -200 N/mm2

Results

Results are tabulated and displayed as in the NAFEMS manual.


             |   Mechanical APDL   |   RATIO  |         INPUT         |
  
 SHELL181
  ECR6X                4.268           0.9997     vmr027-cr10a-181       
  EFFCR                4.928           0.9996     vmr027-cr10a-181       
 PLANE182
  ECR6X                4.268           0.9997     vmr027-cr10a-182       
  EFFCR                4.928           0.9996     vmr027-cr10a-182       
 PLANE183
  ECR6X                4.268           0.9997     vmr027-cr10a-183       
  EFFCR                4.928           0.9996     vmr027-cr10a-183       
 SHELL281
  ECR6X                4.268           0.9997     vmr027-cr10a-281       
  EFFCR                4.928           0.9996     vmr027-cr10a-281             
  
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