T.H.G. Megson (Professor Emeritus, Department of Civil Engineering,

Aircraft Structures for Engineering Students

• Broschiertes Buch

Produktbeschreibung

Aircraft Structures for Engineering Students, Seventh Edition, is the leading self-contained aircraft structures course text suitable for one or more semesters. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its seventh edition, the author has continued to expand the book's coverage of analysis and design of composite materials for use in aircraft and has added more real-world and design-based examples, along with new end-of-chapter problems of varying complexity.

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Produktdetails

• Aerospace Engineering
• Verlag: Elsevier - Health Sciences Division
• 7 ed
• Seitenzahl: 960
• Erscheinungstermin: 22. September 2021
• Englisch
• Abmessung: 235mm x 190mm x 35mm
• Gewicht: 1458g
• ISBN-13: 9780128228685
• ISBN-10: 0128228687
• Artikelnr.: 62110858

Autorenporträt

T.H.G. Megson was a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he wrote the market leading Butterworth Heinemann textbooks Aircraft Structures for Engineering Students and Introduction to Aircraft Structural Analysis (a briefer derivative of the aircraft structures book), as well as the text/ref hybrid Structural and Stress Analysis.

Inhaltsangabe

Part A: Fundamentals of Structural Analysis Section A1: Elasticity 1. Basic
elasticity 2. Two-dimensional problems in elasticity 3. Torsion of solid
sections Section A2: Virtual work, energy, and matrix methods 4. Virtual
work and energy methods 5. Energy methods 6. Matrix methods Section A3:
Thin plate theory 7. Bending of thin plates Section A4: Structural
instability 8. Columns 9. Thin plates Section A5: Vibration of structures
10. Structural vibration
Part B: Analysis of Aircraft Structures Section B1: Principles of stressed
skin construction 11. Materials 12. Structural components of aircraft
Section B2: Airworthiness and airframe loads 13. Airworthiness 14. Airframe
loads 15. Fatigue Section 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 Section 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 Section B5: Structural and
loading discontinuities 26. Closed section beams 27. Open section beams
Section B6: Introduction to aeroelasticity 28. Wing problems