Introduction to structural dynamics and aeroelasticity

Introduction to structural dynamics and aeroelasticity

by Hodges, Dewey H.

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"This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft"--

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Title Statements

  • Full title :Introduction to structural dynamics and aeroelasticity / Dewey H. Hodges, G. Alvin Pierce.

Summary

"This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft"--

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Edition Statements

  • Publication Date:2011.
  • Edition:2nd ed

Publication Statements

The Physical Object

  • Description:1 online resource

Edition Identifiers

  • ISBN:9780511997112, 0511997116, 9781107617094, 110761709X
  • oclc:ocn771283046
  • LC Classification:TL671.6
  • Dewey Decimal:629.134/31

Table of Contents

Cover; Title; Copyright; Contents; Figures; Tables; Foreword; From First Edition; Addendum for Second Edition; 1 Introduction; 2 Mechanics Fundamentals; 2.1 Particles and Rigid Bodies; 2.1.1 Newton's Laws; 2.1.2 Euler's Laws and Rigid Bodies; 2.1.3 Kinetic Energy; 2.1.4 Work; 2.1.5 Lagrange's Equations; 2.2 Modeling the Dynamics of Strings; 2.2.1 Equations of Motion; 2.2.2 Strain Energy; 2.2.3 Kinetic Energy; 2.2.4 Virtual Work of Applied, Distributed Force; 2.3 Elementary Beam Theory; 2.3.1 Torsion; 2.3.2 Bending; 2.4 Composite Beams

2.4.1 Constitutive Law and Strain Energy for Coupled Bending and Torsion2.4.2 Inertia Forces and Kinetic Energy for Coupled Bending and Torsion; 2.4.3 Equations of Motion for Coupled Bending and Torsion; 2.5 The Notion of Stability; 2.6 Systems with One Degree of Freedom; 2.6.1 Unforced Motion; 2.6.2 Harmonically Forced Motion; 2.7 Epilogue; Problems; 3 Structural Dynamics; 3.1 Uniform String Dynamics; 3.1.1 Standing Wave (Modal) Solution; 3.1.2 Orthogonality of Mode Shapes; 3.1.3 Using Orthogonality; 3.1.4 Traveling Wave Solution; 3.1.5 Generalized Equations of Motion

3.1.6 Generalized Force3.1.7 Example Calculations of Forced Response; 3.2 Unifor…

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