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The plane stress condition is given by
(B) σzz=0,auyz=0,auzx=0\sigma_{zz} = 0, au_{yz} = 0, au_{zx} = 0σzz=0,auyz=0,auzx=0
(C) σzz=0,τyz=0,τzx=0\sigma_{zz} =0, \tau_{yz} = 0, \tau_{zx} =0σzz=0,τyz=0,τzx=0
(D) εzz≠0,γyz≠0,γzx≠0\varepsilon_{zz} \neq 0, \gamma_{yz} \neq 0, \gamma_{zx} \neq 0εzz=0,γyz=0,γzx=0
(A) εzz=0,γyz=0,γzx=0\varepsilon_{zz} = 0, \gamma_{yz} = 0, \gamma_{zx} = 0εzz=0,γyz=0,γzx=0
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