Introduction to Aircraft Structural Analysis

AvT.H.G. Megson

Häftad, Engelska, 2017

813 kr

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Beskrivning

Introduction to Aircraft Structure Analysis, Third Edition covers the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work set the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations and sample problems show how to apply the concepts to realistic situations. As a self-contained guide, this value-priced book is an excellent resource for anyone learning the subject.

Based on the author's best-selling text, Aircraft Structures for Engineering Students
Contains expanded coverage of composite materials and structures<
Includes new practical and design-based examples and problems throughout the text
Provides an online teaching and learning tool with downloadable MATLAB code, a solutions manual, and an image bank of figures from the book

Produktinformation

Utgivningsdatum:2017-06-14
Mått:191 x 235 x 43 mm
Vikt:1 560 g
Format:Häftad
Språk:Engelska
Antal sidor:758
Upplaga:3
Förlag:Elsevier Science
ISBN:9780081020760

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Flyg- och rymdteknik inom Naturvetenskap och teknik

Mer om författaren

T.H.G. Megson was a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he wrote the market leading Butterworth Heinemann textbooks Aircraft Structures for Engineering Students and Introduction to Aircraft Structural Analysis (a briefer derivative of the aircraft structures book), as well as the text/ref hybrid Structural and Stress Analysis.

Innehållsförteckning

1. Basic elasticity2. Two-dimensional problems in elasticity3. Torsion of solid sections4. Virtual work and energy methods5. Energy methods6. Matrix methods7. Bending of thin plates8. Columns9. Thin plates10. Materials11. Structural components of aircraft12. Airworthiness13. Airframe loads14. Fatigue15. Bending of open and closed thin-walled beams16. Shear of beams17. Torsion of beams18. Combined open and closed section beams19. Structural idealization20. Wing spars and box beams21. Fuselages22. Wings23. Fuselage frames and wing ribs24. Laminated composite structures