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|a 020282913
|2 Uk
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|a 1277062508
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|a 9780323902113
|q (ePub ebook)
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|z 9780128228685 (pbk.)
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|b 020282913
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|b 000069957228
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|a (OCoLC)1276788888
|z (OCoLC)1277062508
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|a 9780323902113
|b Ingram Content Group
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|a Internet Access
|b AEU
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|a 629.13431
|2 23
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|a UAMI
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1 |
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|a Megson, T. H. G.
|q (Thomas Henry Gordon),
|e author.
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| 245 |
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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 Seventh edition.
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| 264 |
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1 |
|a Amsterdam :
|b Butterworth-Heinemann,
|c 2021.
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| 300 |
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|a 1 online resource :
|b illustrations.
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| 336 |
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|a text
|2 rdacontent
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|a still image
|2 rdacontent
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|a computer
|2 rdamedia
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|a online resource
|2 rdacarrier
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|a Aerospace engineering
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| 504 |
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|a Includes bibliographical references and index.
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| 500 |
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|a <p><b>Part A: Fundamentals of Structural Analysis </b><i>Section A1: Elasticity </i>1. Basic elasticity 2. Two-dimensional problems in elasticity 3. Torsion of solid sections <i>Section A2: Virtual work, energy, and matrix methods </i>4. Virtual work and energy methods 5. Energy methods 6. Matrix methods <i>Section A3: Thin plate theory </i>7. Bending of thin plates <i>Section A4: Structural instability </i>8. Columns 9. Thin plates <i>Section A5: Vibration of structures </i>10. Structural vibration</p> <p><b>Part B: Analysis of Aircraft Structures </b><i>Section B1: Principles of stressed skin construction </i>11. Materials 12. Structural components of aircraft <i>Section B2: Airworthiness and airframe loads </i>13. Airworthiness 14. Airframe loads 15. Fatigue <i>Section B3: Bending, shear and torsion of thin-walled beams </i>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 <i>Section B4: Stress analysis of aircraft components </i>21. Wing spars and box beams 22. Fuselages 23. Wings 24. Fuselage frames and wing ribs 25. Laminated composite structures <i>Section B5: Structural and loading discontinuities </i>26. Closed section beams 27. Open section beams <i>Section B6: Introduction to aeroelasticity </i>28. Wing problems</p>
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|a Description based on CIP data; resource not viewed.
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| 590 |
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|a Knovel
|b ACADEMIC - Mechanics & Mechanical Engineering
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| 590 |
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
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| 650 |
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|a Airframes.
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| 650 |
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6 |
|a Cellules (Aéronautique)
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| 650 |
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7 |
|a airframes.
|2 aat
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| 650 |
|
7 |
|a Airframes.
|2 fast
|0 (OCoLC)fst00802910
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| 776 |
0 |
8 |
|i Print version :
|z 9780128228685
|
| 856 |
4 |
0 |
|u https://appknovel.uam.elogim.com/kn/resources/kpASESE011/toc
|z Texto completo
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| 938 |
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|a Askews and Holts Library Services
|b ASKH
|n AH38503821
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| 994 |
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|a 92
|b IZTAP
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