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Aircraft Structures for Engineering Students cover

Aircraft Structures for Engineering Students

by T.H.G. Megson

6th Edition

Publisher: Elsevier Butterworth Heinemann

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Aeronautics & Astronautics

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Book Details

Print ISBN9780081009147
eText ISBN9780081009987
PublisherElsevier Butterworth Heinemann
Publishing Year2017
Edition6th Edition
LanguageEnglish
Pages910

Aircraft Structures for Engineering Students, 6th Edition, by T.H.G. Megson presents fundamental principles and analytical techniques for evaluating aerospace structures. The textbook introduces core concepts in elasticity, energy formulations, and matrix methods.

Coverage addresses airworthiness, airframe loads, structural instability, and thin-plate bending. It also examines structural components of aircraft, including thin-walled beams, wing ribs, and fuselages.

For the 2017 sixth edition, the volume expanded its treatment of composite materials and added practical, design-based examples and problems to connect theoretical concepts to engineering applications.

Table of Contents

  1. Chapter 1: Basic elasticity

  2. Chapter 2: Two-dimensional problems in elasticity

  3. Chapter 3: Torsion of solid sections

  4. Chapter 4: Virtual work and energy methods

  5. Chapter 5: Energy methods

  6. Chapter 6: Matrix methods

  7. Chapter 7: Bending of thin plates

  8. Chapter 8: Columns

  9. Chapter 9: Thin plates

  10. Chapter 10: Structural vibration

  11. Chapter 11: Materials

  12. Chapter 12: Structural components of aircraft

  13. Chapter 13: Airworthiness

  14. Chapter 14: Airframe loads

  15. Chapter 15: Fatigue

  16. Chapter 16: Bending of open and closed, thin-walled beams

  17. Chapter 17: Shear of beams

  18. Chapter 18: Torsion of beams

  19. Chapter 19: Combined open and closed section beams

  20. Chapter 20: Structural idealization

  21. Chapter 21: Wing spars and box beams

  22. Chapter 22: Fuselages

  23. Chapter 23: Wings

  24. Chapter 24: Fuselage frames and wing ribs

  25. Chapter 25: Laminated composite structures

  26. Chapter 26: Closed section beams

  27. Chapter 27: Open section beams

  28. Chapter 28: Wing problems

  29. Chapter Appendix: Design of a rear fuselage

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