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OverviewThe purpose of the work described in this book is to verify with a FEM analysis a preliminary design of the wing structure of a 250 seats PrandtlPlane aircraft, made up in aluminum alloy. The wing structure has been optimized with a multistep process. Moreover, a composite design of the structure is here investigated, with a preliminary sizing of the wing and a FEM analysis of the system together with the buckling analysis of the compressed skins is accomplished. The results in terms of weight and stress distribution are shown, and a comparison between the metal and the composite solution is performed. Full Product DetailsAuthor: Flavio Quattrone , Francesco ContiniPublisher: LAP Lambert Academic Publishing Imprint: LAP Lambert Academic Publishing Dimensions: Width: 15.20cm , Height: 0.70cm , Length: 22.90cm Weight: 0.186kg ISBN: 9783848440863ISBN 10: 3848440865 Pages: 120 Publication Date: 12 April 2012 Audience: General/trade , General Format: Paperback Publisher's Status: Active Availability: In stock We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately. Table of ContentsReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |