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|a 993056508
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|z 9780081009147
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|z 0081009143
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|a 9780081009987
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|a 0081009984
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|a (OCoLC)973486002
|z (OCoLC)993056508
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|a TL671.6
|b .M36 2017eb
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|a 629.1/3431
|2 23
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|a Megson, T. H. G.
|q (Thomas Henry Gordon),
|e author.
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|a Aircraft structures for engineering students /
|c T.H.G. Megson.
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250 |
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|a Sixth edition.
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264 |
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|a Amsterdam ;
|a Boston :
|b Butterworth-Heinemann is an imprint of Elsevier,
|c [2017]
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300 |
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|a 1 online resource (xvii, 891 pages) :
|b illustrations.
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336 |
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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490 |
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|a Elsevier aerospace engineering series
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500 |
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|a Includes index.
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520 |
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|a Aircraft Structures for Engineering Students, Sixth Edition, is the leading self-contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its sixth edition, the author has expanded the book's coverage of analysis and design of composite materials for use in aircraft, and has added new, real-world and design-based examples, along with new end-of-chapter problems of varying complexity.
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|a Print version record.
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|a Part A. Fundamentals of structural analysis. Section A1. Elasticity. Basic elasticity -- Two-dimensional problems in elasticity -- Torsion of solid sections -- Section A2. Virtual work, energy, and matrix methods. Virtual work and energy methods -- Energy methods -- Matrix methods -- Section A3. Thin plate theory. Bending of thin plates -- Section A4. Structural instability. Columns -- Thin plates -- Section A5. Vibration of structures. Structural vibration -- Part B. Analysis of aircraft structures. Section B1. Principles of stressed skin construction. Materials -- Structural components of aircraft -- Section B2. Airworthiness and airframe loads. Airworthiness -- Airframe loads -- Fatigue -- Section B3. Bending, shear and torsion of thin-walled beams. Bending of open and closed, thin-walled beams -- Shear of beams -- Torsion of beams -- Combined open and closed section beams -- Structural idealization -- Section B4. Stress analysis of aircraft components. Wing spars and box beams -- Fuselages -- Wings -- Fuselage frames and wing ribs -- Laminated composite structures -- Section B5. Structural and loading discontinuities. Closed section beams -- Open section beams -- Section B6. Introduction to aeroelasticity. Wing problems -- Appendix : Design of a rear fuselage.
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|a Airframes
|v Textbooks.
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|a Structural analysis (Engineering)
|v Textbooks.
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|a Airframes
|2 fast
|0 (OCoLC)fst00802910
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|a Structural analysis (Engineering)
|2 fast
|0 (OCoLC)fst01135602
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|a Avions
|x Conception et construction.
|2 ram
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|a Avions
|x Vibrations.
|2 ram
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|a Textbooks
|2 fast
|0 (OCoLC)fst01423863
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|a Textbooks.
|2 lcgft
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776 |
0 |
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|i Print version:
|a Megson, T. H. G. (Thomas Henry Gordon).
|t Aircraft structures for engineering students.
|b Sixth edition.
|d Amsterdam ; Boston : Butterworth-Heinemann is an imprint of Elsevier, [2017]
|z 9780081009147
|w (OCoLC)954224012
|
830 |
|
0 |
|a Elsevier aerospace engineering series.
|
856 |
4 |
0 |
|u https://sciencedirect.uam.elogim.com/science/book/9780081009147
|z Texto completo
|