Introduction to Aircraft Structural Analysis - T.H.G. Megson

Introduction to Aircraft Structural Analysis

(Autor)

Buch | Softcover
728 Seiten
2013 | 2nd edition
Butterworth-Heinemann Ltd (Verlag)
978-0-08-098201-4 (ISBN)
77,30 inkl. MwSt
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Covers the basics of structural analysis as applied to aircraft structures. In this book, coverage of elasticity, energy methods and virtual work set the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. It also includes numerous worked examples, illustrations, and sample problems.
Introduction to Aircraft Structural Analysis, Second Edition, is an essential resource for learning aircraft structural analysis. Based on the author's best-selling text Aircraft Structures for Engineering Students, this brief book covers the basics of structural analysis as applied to aircraft structures.Coverage of elasticity, energy methods, and virtual work sets 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.This text is designed for undergraduate and postgraduate students of aerospace and aeronautical engineering as well as for professional development and training courses.

T.H.G. Megson is a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he has written 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.

Part A: Fundamentals of Structural Analysis
1. Basic Elasticity
2. 2D Problems in Elasticity
3. Torsion of Solid Sections
4. Virtual Work and Energy Methods
5. Energy Methods
6. Matrix Methods
7. Bending of Thin Plates
8. Columns
9. Thin Plates

Part B: Analysis of Aircraft Structures
10. Materials
11. Structural Components of Aircraft
12. Airworthiness
13. Airframe Loads
14. Fatigue
15. Bending of Open, Closed, and Thin Walled Beams
16. Shear of Beams
17. Torsion of Beams
18. Combined Open and Closed Section Beams
19. Structural Idealization
20. Wing Spars and Box Beams
21. Fuselages
22. Wings
23. Fuselage frames and wing ribs

Erscheint lt. Verlag 22.10.2013
Verlagsort Oxford
Sprache englisch
Maße 191 x 235 mm
Gewicht 1330 g
Themenwelt Technik Fahrzeugbau / Schiffbau
Technik Luft- / Raumfahrttechnik
ISBN-10 0-08-098201-8 / 0080982018
ISBN-13 978-0-08-098201-4 / 9780080982014
Zustand Neuware
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