HomeIntroduction to Aircraft Structural Analysis
Skip to product information
1 of 1

Introduction to Aircraft Structural Analysis

paperbackFebruary 16, 2010
Regular price $318.20 USD
Regular price Sale price $318.20 USD
Sale Sold out
Shipping calculated at checkout.
Secure Checkout
Quality Guaranteed
New In Stock
ISBN-13: 9781856179324 ISBN-10: 185617932X
Publisher
Butterworth-Heinemann
Binding
paperback
Published
February 16, 2010
Weight
2.3 lbs
Dimensions
22.90×3.20×18.40 cm

About this book

Introduction to Aircraft Structural Analysis by Megson, T.H.G.. paperback edition. ISBN: 9781856179324.

Introduction to Aircraft Structural Analysis is an essential resource for learning aircraft structural analysis. Based on the authors best-selling book Aircraft Structures for Engineering Students, this brief text introduces the reader to the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work sets the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations, and sample problems show how to apply the concepts to realistic situations. The book covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aero elasticity. It consists of 23 chapters covering a variety of topics from basic elasticity to torsion of solid sections; energy methods; matrix methods; bending of thin plates; structural components of aircraft; airworthiness; airframe loads; bending of open, closed, and thin walled beams; combined open and closed section beams; wing spars and box beams; and fuselage frames and wing ribs. This book will appeal to undergraduate and postgraduate students of aerospace and aeronautical engineering, as well as professional development and training courses. Based on the authors best-selling text Aircraft Structures for Engineering Students, this Intro version covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aeroelasticity Systematic step by step procedures in the worked examples Self-contained, with complete derivations for key equations