Ebooks (Sách điện tử)Authors : James F. III, Marchman (2022)
In this textbook analytical methods are developed for the response and failure of the primary structural components
of aircraft. Newton's laws of motion, Hooke s law, and the first law of thermodynamics are the basis to
model the thermoelastic response of thin-walled, straight bars and coplanar curved bars. Analytical methods
include energy principles to develop Castigliano's theorems and to develop the cross-sectional material law for
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