Introduction to Aircraft Structural Analysis
Butterworth-Heinemann Ltd (Verlag)
978-1-85617-932-4 (ISBN)
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Introduction to Aircraft Structural Analysis is an essential resource for learning aircraft structural analysis. Based on the author's best-selling book Aircraft Structures for Engineering Students, this brief text introduces the reader to 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.
The book covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aero elasticity. It consists of 23 chapters covering a variety of topics from basic elasticity to torsion of solid sections; energy methods; matrix methods; bending of thin plates; structural components of aircraft; airworthiness; airframe loads; bending of open, closed, and thin walled beams; combined open and closed section beams; wing spars and box beams; and fuselage frames and wing ribs.
This book will appeal to undergraduate and postgraduate students of aerospace and aeronautical engineering, as well as professional development and training courses.
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.
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
Verlagsort | Oxford |
---|---|
Sprache | englisch |
Maße | 191 x 235 mm |
Gewicht | 1330 g |
Themenwelt | Technik ► Fahrzeugbau / Schiffbau |
Technik ► Luft- / Raumfahrttechnik | |
ISBN-10 | 1-85617-932-X / 185617932X |
ISBN-13 | 978-1-85617-932-4 / 9781856179324 |
Zustand | Neuware |
Informationen gemäß Produktsicherheitsverordnung (GPSR) | |
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