Aircraft structures for engineering students

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Bibliographic Details
Main Author Megson, T. H. G. (Author)
Format Electronic eBook
LanguageEnglish
Published Amsterdam : Butterworth-Heinemann, 2021.
EditionSeventh edition.
SeriesAerospace engineering
Subjects
Online AccessFull text
ISBN9780323902113
0323902111
9780128228685 (pbk.)
Physical Description1 online resource : illustrations.

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020 |a 9780323902113  |q (ePub ebook) 
020 |a 0323902111 
020 |z 9780128228685 (pbk.) 
035 |a (OCoLC)1276788888  |z (OCoLC)1277062508 
100 1 |a Megson, T. H. G.  |q (Thomas Henry Gordon),  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PCjFTf8w6mmWwWktgqyjMrm 
245 1 0 |a Aircraft structures for engineering students /  |c T.H.G. Megson. 
250 |a Seventh edition. 
264 1 |a Amsterdam :  |b Butterworth-Heinemann,  |c 2021. 
300 |a 1 online resource :  |b illustrations. 
336 |a text  |2 rdacontent 
336 |a still image  |2 rdacontent 
337 |a computer  |2 rdamedia 
338 |a online resource  |2 rdacarrier 
490 0 |a Aerospace engineering 
504 |a Includes bibliographical references and index. 
500 |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> 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Airframes. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
776 0 8 |i Print version :  |z 9780128228685 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpASESE011/aircraft-structures-for?kpromoter=marc  |y Full text