Aircraft structures for engineering students / T.H.G. Megson.
Material type: TextSeries: Elsevier aerospace engineering seriesPublisher: Oxford ; Burlington, MA : Butterworth-Heinemann, 2007Edition: Fourth editionDescription: xx, 804 pages : illustrations ; 25 cmContent type:- text
- unmediated
- volume
- 0750667397
- 9780750667395
- 629.13431 22
- TL671.6 .M36 2007
Item type | Current library | Call number | Copy number | Status | Date due | Barcode | |
---|---|---|---|---|---|---|---|
Book | City Campus City Campus Main Collection | 629.13431 MEG (Browse shelf(Opens below)) | 1 | Available | A401667B |
Previous ed.: London : Arnold, 1999.
Includes bibliographical references and index.
Sect. A1. Elasticity -- 1. Basic elasticity -- 2. Two dimensional problems in elasticity -- 3. Torsion of solid sections -- Sect. A2. Virtual work, energy matrix methods -- 4. Virtual work and energy methods -- 5. Energy methods -- 6. Matrix methods -- Sect. A3. Thin plate theory -- 7. Bending of thin plates -- Sect. A4. Structural instability -- 8. Columns -- 9. Thin plates -- Sect. A5. Vibration of structures -- 10. Structural vibration -- Sect. B1. Principles of stressed skin construction -- 11. Materials -- 12. Structural components of aircraft -- Sect. B2. Airworthiness and airframe loads -- 13. Airworthiness -- 14. Airframe loads -- 15. Fatigue -- Sect. B3. Bending, shear and torsion of thin-walled beams -- 16. Bending of open and closed, thin-walled beams -- 17. Shear of beams -- 18. Torsion of beams -- 19. Combined open and closed section beams -- 20. Structural idealization -- Sect. B4. Stress analysis of aircraft components -- 21. Wing spars and box beams -- 22. Fuselages -- 23. Wings -- 24. Fuselage frames and wing ribs -- 25. Laminated composite structures -- Sect. B5. Structural and loading discontinuities -- 26. Closed section beams -- 27. Open section beams -- Sect. B6. Introduction to aeroelasticity -- 28. Wing problems.
"Aircraft Structures for Engineering Students is a self-contained text for students of aerospace and mechanical engineering. It covers all the fundamental subjects taken in an aircraft structural design and analysis course, including elasticity, structural mechanics and analysis, airworthiness and aeroelasticity. It is ideal for use as a textbook for a first course in aircraft structures or structural design and analysis, as well as a reference for graduate level courses."--BOOK JACKET.
Machine converted from AACR2 source record.
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