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

Introduction to Aircraft Structural Analysis

(Autor)

Buch | Softcover
648 Seiten
2010
Butterworth-Heinemann Ltd (Verlag)
978-1-85617-932-4 (ISBN)
59,95 inkl. MwSt
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Covers the basics of structural analysis as applied to aircraft structures. This title offers coverage of elasticity, energy methods and virtual work that sets the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. It features worked examples, illustrations, and sample problems.
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 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

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
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