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Introduction to Aircraft Structural Analysis cover

Introduction to Aircraft Structural Analysis

by T.H.G. Megson

3rd Edition

Publisher: Butterworth-Heinemann

(0 reviews)
Aeronautics & Astronautics

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Book Details

Print ISBN9780081020760
eText ISBN9780081021002
PublisherButterworth-Heinemann
Publishing Year2017
Edition3rd Edition
LanguageEnglish
Pages758

Introduction to Aircraft Structural Analysis, 3rd Edition, is a textbook that covers fundamental structural analysis principles for aircraft applications. Developed as a briefer derivative of Aircraft Structures for Engineering Students, the work establishes core mechanics for evaluating flight vehicles.

The volume explores elasticity, virtual work, and energy methods as a basis for examining airworthiness, airframe loads, and major aircraft components. Readers study the behavior of thin plates, beams, wings, and fuselages.

Intended for undergraduate and postgraduate aerospace and aeronautical engineering students, the text also suits professional development courses. Numerous worked examples, illustrations, and sample problems show how to apply structural analysis concepts to realistic scenarios.

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: Materials

  11. Chapter 11: Structural components of aircraft

  12. Chapter 12: Airworthiness

  13. Chapter 13: Airframe loads

  14. Chapter 14: Fatigue

  15. Chapter 15: Bending of open and closed thin-walled beams

  16. Chapter 16: Shear of beams

  17. Chapter 17: Torsion of beams

  18. Chapter 18: Combined open and closed section beams

  19. Chapter 19: Structural idealization

  20. Chapter 20: Wing spars and box beams

  21. Chapter 21: Fuselages

  22. Chapter 22: Wings

  23. Chapter 23: Fuselage frames and wing ribs

  24. Chapter 24: Laminated composite structures

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