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Nonlinear Composite Beam Theory

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Pub Date: April 15, 2006

Dewey: 629.1

LCCN: 2007531073

Lexile Code: 0000

Target Age Group: NA to NA

Physical Info: 0.89" H x 9.36" L x 6.32" W ( 1.21 lbs) 304 pages

Series: Progress in Astronautics and Aeronautics

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Description: From an authoritative expert whose work on modern helicopter rotor blade analysis has spanned over three decades, comes the first consistent and rigorous presentation of beam theory. Beginning with an overview of the theory developed over the last 60 years, Dr. Hodges addresses the kinematics of beam deformation, provides a simple way to characterize strain in an initially curved and twisted beam, and offers cross-sectional analysis for beams with arbitrary cross sections and composed of arbitrary materials. He goes on to present a way to accurately recover all components of cross-sectional strain and stress before providing a natural one-dimensional (1D) theory of beams. Sample results for both cross-sectional and 1D analysis are presented, as is a parallel treatment for thin-walled beams.

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