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OverviewThis book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including: -The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. - The linearized theories for compressible subsonic and supersonic aerodynamics. - The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. - Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations. There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows. A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis. Full Product DetailsAuthor: J. J. Chattot , M. M. HafezPublisher: Springer Imprint: Springer Edition: Softcover reprint of the original 1st ed. 2015 Weight: 1.305kg ISBN: 9789401777933ISBN 10: 9401777934 Pages: 620 Publication Date: 13 October 2016 Audience: Professional and scholarly , Professional & Vocational Format: Paperback Publisher's Status: Active Availability: Manufactured on demand We will order this item for you from a manufactured on demand supplier. Table of ContentsReviewsAuthor InformationJ.J. Chattot, University of California, Davis, Dept. Mechanical & Aeronautical, Davis, USA M.M. Hafez, University of California, Davis, Dept. Mechanical & Aeronautical, Davis, USA. Tab Content 6Author Website:Countries AvailableAll regions |