We will assume that the stresses σx, σy, and τxy at a point are known. We need to compute the normal and shear stresses acting on an arbitrarily oriented face.
Note: τyx = τxy
We will assume that the stresses σx, σy, and τxy at a point are known. We need to compute the normal and shear stresses acting on an arbitrarily oriented face.
Note: τyx = τxy