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Aircraft Structures for Engineering Students, Fourth Edition

Aircraft Structures for Engineering Students, Fourth Edition

by T.H.G. Megson

2007 (825 pages)

ISBN:9780750667395

Featuring case studies and worked examples that make the text accessible, this resource covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity.

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Table of Contents

Aircraft Structures for Engineering Students, Fourth Edition
Preface
Preface to Second Edition
Preface to Third Edition
Preface to Fourth Edition
Part A - Fundamentals of Structural Analysis
Section A1 - Elasticity
Chapter 1	-	Basic Elasticity
Chapter 2	-	Two-Dimensional Problems in Elasticity
Chapter 3	-	Torsion of Solid Sections
Section A2 - Virtual Work, Energy and Matrix Methods
Chapter 4	-	Virtual Work and Energy Methods
Chapter 5	-	Energy Methods
Chapter 6	-	Matrix Methods
Section A3 - Thin Plate Theory
Chapter 7	-	Bending of Thin Plates
Section A4 - Structural Instability
Chapter 8	-	Columns
Chapter 9	-	Thin Plates
Section A5 - Vibration of Structures
Chapter 10	-	Structural Vibration
Part B - Analysis of Aircraft Structures
Section B1 - Principles of Stressed Skin Construction
Chapter 11	-	Materials
Chapter 12	-	Structural Components of Aircraft
Section B2 - Airworthiness and Airframe Loads
Chapter 13	-	Airworthiness
Chapter 14	-	Airframe Loads
Chapter 15	-	Fatigue
Section B3 - Bending, Shear and Torsion of Thin-Walled Beams
Chapter 16	-	Bending of Open and Closed, Thin-Walled Beams
Chapter 17	-	Shear of Beams
Chapter 18	-	Torsion of Beams
Chapter 19	-	Combined Open and Closed Section Beams
Chapter 20	-	Structural Idealization
Section B4 - Stress Analysis of Aircraft Components
Chapter 21	-	Wing Spars and Box Beams
Chapter 22	-	Fuselages
Chapter 23	-	Wings
Chapter 24	-	Fuselage Frames and Wing Ribs
Chapter 25	-	Laminated Composite Structures
Section B5 - Structural and Loading Discontinuities
Chapter 26	-	Closed Section Beams
Chapter 27	-	Open Section Beams
Section B6 - Introduction to Aeroelasticity
Chapter 28	-	Wing Problems
Appendix A	-	Design of a Rear Fuselage