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Status:
Available4.3
38 reviews
ISBN-10 : 0521806984
ISBN-13 : 9780521806985
Author: Dewey H. Hodges, G. Alvin Pierce
This text provides an introduction structural dymanies and aeroelamcity,with un emphasis on consortional aircraft. The primary arvas considered are structural dynamics, static senselancity, and dynamic arroelasticity. The structural dynamics material uphines vibration, the modal representation, and dynamic napoоно Auroclastic phenomena discussed mclude divergence, aileron reversal, arload re distribution, urteady aerodynamics, flutter, and elasts taikering. Both cact and approximate salenion methodologies are stressed. Mom than 100 illustrations and tables help clarify the text, while apwants of 50 problems enhance student laarming. This test meets the need fin an up-to-date of structural dynamick and senselasticity for advanced undergraduate or beginning graduate scevspace engineering students
1 Introduction
2 Structural Dynamics
2.1 Uniform String Dynamics
2.1.1 Equations of Motion
2.1.2 Standing Wave (Modal) Solution
2.1.3 Orthogonality of Mode Shapes
2.1.4 Using Orthogonality
2.1.5 Traveling Wave Solution
2.1.6 Generalized Equations of Motion
2.1.7 Generalized Force
2.2 Uniform Beam Torsional Dynamics
2.2.1 Equation of Motion
2.2.2 Boundary Conditions
2.2.3 Example Solutions for Mode Shapes and Frequencies
2.3 Uniform Beam Bending Dynamics
2.3.1 Equation of Motion
2.3.2 General Solutions
2.3.3 Boundary Conditions
2.3.4 Example Solutions for Mode Shapes and Frequencies
2.4 Approximate Solution Techniques
2.4.1 The Ritz Method
2.4.2 Galerkin's Method
2.5 Epilogue
3 Static Aeroelasticity
3.1 Wind Tunnel Models
3.1.1 Wall-Mounted Model
3.1.2 Sting-Mounted Model
3.1.3 Strut-Mounted Model
3.1.4 Wall-Mounted Model for Application to Aileron Reversal
3.2 Uniform Lifting Surface
3.2.1 Equilibrium Equation
3.2.2 Torsional Divergence
3.2.3 Airload Distribution
3.2.4 Sweep Effects
3.3 Epilogue
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Tags: Introduction, Structural Dynamics, Aeroelasticity, Dewey Hodges, Alvin Pierce
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