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.
Show that Eqs. 2.65-2.67 yield Eqs. 2.68.
(2.65)
(2.66)
(2.67)
(2.68)
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