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OverviewThis text provides students who have had statics and introductory strength of materials with the necessary tools to perform stress analysis on aerospace structures such as wings, tails, fuselages, and space frames. It progresses from introductory continuum mechanics through strength of materials of thin-walled structures to energy methods, culminating in an introductory chapter on the powerful finite element method. Full Product DetailsAuthor: David H. Allen , Walter HaislerPublisher: John Wiley and Sons Ltd Imprint: John Wiley & Sons Inc Dimensions: Width: 16.90cm , Height: 3.10cm , Length: 24.30cm Weight: 0.883kg ISBN: 9780471888390ISBN 10: 0471888397 Pages: 528 Publication Date: 06 February 1985 Audience: College/higher education , Professional and scholarly , Undergraduate , Postgraduate, Research & Scholarly Format: Paperback Publisher's Status: Active Availability: In Print ![]() This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us. Table of ContentsThe Structural Design Concept. Mechanics of Aerospace Structures. Constitution of Aerospace Materials. Theory and Analysis of Aerospace Beams. Work and Energy Principles. Deformation and Force Analysis of Aerospace Structures. Introduction to Finite Element Stiffness Method. Appendix.ReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |