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Introduction to aircraft structural analysis /

Introduction to Aircraft Structure Analysis, Third Edition covers the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work set the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Num...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Megson, T. H. G. (Thomas Henry Gordon) (Autor)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Amsterdam : Butterworth-Heinemann, 2017.
Edición:Third edition.
Temas:
Acceso en línea:Texto completo

MARC

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100 1 |a Megson, T. H. G.  |q (Thomas Henry Gordon),  |e author. 
240 1 0 |a Aircraft structures for engineering structures 
245 1 0 |a Introduction to aircraft structural analysis /  |c T.H.G. Megson. 
250 |a Third edition. 
264 1 |a Amsterdam :  |b Butterworth-Heinemann,  |c 2017. 
300 |a 1 online resource 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
500 |a Previous edition: published as Aircraft structures for engineering structures. 2014. 
500 |a 1. Basic elasticity 2. Two-dimensional problems in elasticity 3. Torsion of solid sections 4. Virtual work and energy methods 5. Energy methods 6. Matrix methods 7. Bending of thin plates 8. Columns 9. Thin plates 10. Materials 11. Structural components of aircraft 12. Airworthiness 13. Airframe loads 14. Fatigue 15. Bending of open and closed thin-walled beams 16. Shear of beams 17. Torsion of beams 18. Combined open and closed section beams 19. Structural idealization 20. Wing spars and box beams 21. Fuselages 22. Wings 23. Fuselage frames and wing ribs 24. Laminated composite structures. 
588 0 |a CIP data; item not viewed. 
520 |a Introduction to Aircraft Structure Analysis, Third Edition covers the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work set the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations and sample problems show how to apply the concepts to realistic situations. As a self-contained guide, this value-priced book is an excellent resource for anyone learning the subject. 
650 0 |a Airframes. 
650 0 |a Structural analysis (Engineering) 
650 6 |a Cellules (A�eronautique)  |0 (CaQQLa)201-0033526 
650 6 |a Th�eorie des constructions.  |0 (CaQQLa)201-0015598 
650 7 |a airframes.  |2 aat  |0 (CStmoGRI)aat300212612 
650 7 |a structural analysis.  |2 aat  |0 (CStmoGRI)aat300056397 
650 7 |a Airframes  |2 fast  |0 (OCoLC)fst00802910 
650 7 |a Structural analysis (Engineering)  |2 fast  |0 (OCoLC)fst01135602 
776 0 8 |i Print version:  |z 9780081020760 
856 4 0 |u https://sciencedirect.uam.elogim.com/science/book/9780081020760  |z Texto completo