Aircraft Structures for Engineering Students (6th Ed)(gnv64)

Aircraft Structures for Engineering Students (6th Ed)
Bt T. H. G. Megson
Butterworth-Heinemann | December 2016 | ISBN-10: 0081009143 | PDF | 910 pages | 12 mb
https://www.amazon.com/Aircraft-Structures-Engineering-Students-Sixth/dp/0081009143

Aircraft Structures for Engineering Students, Sixth Edition, is the leading self-contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its sixth edition, the author has expanded the book’s coverage of analysis and design of composite materials for use in aircraft, and has added new, real-world and design-based examples, along with new end-of-chapter problems of varying complexity.

- Expanded coverage of composite materials and structures
- New practical and design-based examples and problems throughout the text aid
- understanding and relate concepts to real world applications
- Updated and additional Matlab examples and exercises support use of computational tools in analysis and design
- Available online teaching and learning tools include downloadable Matlab code, solutions manual, and image bank of figures from the book

About the Author
T.H.G. Megson is a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he has written 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.

CONTENTS
Preface
Part A: Fundamentals of Structural Analysis
Section A1: Elasticity
Section A2: Virtual work, energy, and matrix methods
Section A3: Thin plate theory
Section A4: Structural instability
Section A5: Vibration of structures
Part B: Analysis of Aircraft Structures
Section B1: Principles of stressed skin construction
Section B2: Airworthiness and airframe loads
Section B3: Bending, shear and torsion of thin-walled beams
Section B4: Stress analysis of aircraft components
Section B5: Structural and loading discontinuities
Section B6: Introduction to aeroelasticity
Appendix: Design of a rear fuselage
Appendix: Design of a rear fuselage

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