Aerospace Engineering > GATE 2009 > Stress Analysis
For a plane strain problem, the stresses satisfy the condition
A
τxz=τyz=σz=0
B
τxz=τyz=0, σz=ν(σx+σy)
C
τxz=τyz=0, σz=ντxy
D
τxz=τyz=0, σz=ν(σx+σy)+(1-ν)τxy

Correct : b

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