
Introduction to Aircraft Structural Analysis
by T.H.G. Megson
3rd Edition
Publisher: Butterworth-Heinemann
Book Details
| Print ISBN | 9780081020760 |
| eText ISBN | 9780081021002 |
| Publisher | Butterworth-Heinemann |
| Publishing Year | 2017 |
| Edition | 3rd Edition |
| Language | English |
| Pages | 758 |
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
Chapter 1: Basic elasticity
Chapter 2: Two-dimensional problems in elasticity
Chapter 3: Torsion of solid sections
Chapter 4: Virtual work and energy methods
Chapter 5: Energy methods
Chapter 6: Matrix methods
Chapter 7: Bending of thin plates
Chapter 8: Columns
Chapter 9: Thin plates
Chapter 10: Materials
Chapter 11: Structural components of aircraft
Chapter 12: Airworthiness
Chapter 13: Airframe loads
Chapter 14: Fatigue
Chapter 15: Bending of open and closed thin-walled beams
Chapter 16: Shear of beams
Chapter 17: Torsion of beams
Chapter 18: Combined open and closed section beams
Chapter 19: Structural idealization
Chapter 20: Wing spars and box beams
Chapter 21: Fuselages
Chapter 22: Wings
Chapter 23: Fuselage frames and wing ribs
Chapter 24: Laminated composite structures
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