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Standard Methods for Aerospace Stress Analysis
book

Standard Methods for Aerospace Stress Analysis

by Amir Javidinejad
October 2025
Intermediate to advanced
272 pages
7h 54m
English
Wiley
Content preview from Standard Methods for Aerospace Stress Analysis

4Energy Methods

4.1 Introduction to Energy Methods

Chapter 4 explores the application of energy methods for the determination of structural behavior of determinate and indeterminate structures. The strain energy concept is examined for the determination of displacements and rotations in solid elastic bodies.

4.2 Strain Energy

Strain energy is usually defined as the energy stored within an elastic body when a solid body is deformed by a specified applied loading. Thus, the strain energy is equivalent to the work done by the external forces acting on a solid body. The general expression defining the strain energy is shown as follows:

(4.1)upper U equals one half integral Underscript upper V Endscripts left-parenthesis sigma Subscript italic x x Baseline epsilon Subscript italic x x Baseline plus sigma Subscript italic y y Baseline epsilon Subscript italic y y Baseline plus sigma Subscript italic z z Baseline epsilon Subscript italic z z Baseline plus tau Subscript italic x y Baseline gamma Subscript italic x y Baseline plus tau Subscript italic y z Baseline gamma Subscript italic y z Baseline plus tau Subscript italic x z Baseline gamma Subscript italic x z Baseline right-parenthesis normal d upper V

For any bar of the length, L, under only the axial loading of F, the expression above reduces to the following expression:

(4.2)upper U equals one half integral Underscript upper V Endscripts left-parenthesis sigma Subscript italic x x Baseline epsilon Subscript italic x x Baseline right-parenthesis normal d upper V

where the volume change is dV = Adx, the area times the change in length (L).

Substitute the terms for the axial stress and strain, and one would have

(4.3)upper U equals one half integral Underscript upper L Endscripts left-parenthesis StartFraction upper F Over upper A EndFraction StartFraction upper F Over italic upper E upper A EndFraction right-parenthesis upper A normal d x

This expression is solved and reduced as

(4.4)upper U equals StartFraction upper F squared upper L Over 2 italic upper E upper A EndFraction

Which, for a series of “n” bars joined together, the strain energy takes the series form

Likewise, for ...

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Publisher Resources

ISBN: 9781394330188