Correct option is (c) \(Γ_{xz} =\frac{∂u}{∂z}+\frac{∂w}{∂x} \)
Easiest explanation: In order to find the shearing strain component in Z-X plane, let us consider a plane lamina of size dx, dz in Z-X plane. If w is the displacement in z-direction and u is the displacement in x-direction, the shearing strain component is,
\(Γ_{xz} =\frac{∂u}{∂z}+\frac{∂w}{∂x}. \)