Image from Coce

Aircraft structures for engineering students / T.H.G. Megson.

By: Material type: TextTextSeries: Elsevier aerospace engineering seriesPublisher: Oxford ; Burlington, MA : Butterworth-Heinemann, 2007Edition: Fourth editionDescription: xx, 804 pages : illustrations ; 25 cmContent type:
  • text
Media type:
  • unmediated
Carrier type:
  • volume
ISBN:
  • 0750667397
  • 9780750667395
Subject(s): DDC classification:
  • 629.13431 22
LOC classification:
  • TL671.6 .M36 2007
Contents:
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.
Review: "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.
Tags from this library: No tags from this library for this title. Log in to add tags.
Holdings
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.

There are no comments on this title.

to post a comment.

Powered by Koha