The problems for Sections 2.5-2.8 involve displacements, deformations, and strain states at a point in a structural or machine member. These quantities, as with then stress counterparts, are important in design and failure criteria.
A square panel in the side of a ship (Figure P2.55) is loaded so that the panel is in a state of plane strain (ϵzz = ϵzx = ϵzy = 0).
a. Determine the displacements for the panel given the deformations shown and the strain components for the (x, y) coordinate axes.
b. Determine the strain components for the (X, Y) axes.
FIGURE P2.55
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