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Robert Wright, trading as 'The Bookman' /AbebooksUK
dealer size: 16
ISBN10: 3540058079, ISBN13: 9783540058076, [publisher: Springer-Verlag, Berlin] Softcover First Edition Scientific/mathematical/aeronautical exposition. First Edn., 1972; [iv]+[ii]+211pp. +[i]p. publisher's catalogue; illus. bw. diagrams. Slightly faded spine very lightly rubbed at tail, but complete/intact/clean; front cover very slightly faded at fore-ede, with very small crease to bottom corner, but covers clean; fore-edge faintly tanned, but pages clean/crisp/very bright. No creasing to spine. Name in ink to front cover, but no highlighting/annotations to text. VG- PRICE INCLUDES UK POSTAGE & PACKING. [Norwich, United Kingdom] [Publication Year: 1972]
ISBN10: 3540058079, ISBN13: 9783540058076, [publisher: Springer] Hardcover Ex-library with the usual features. The interior is clean and tight. Binding and cover are good. The book has been rebound in a hard cover library binding. 211 pages. [Russell, IA, U.S.A.] [Publication Year: 1972]
ISBN10: 3540058079, ISBN13: 9783540058076, [publisher: Springer Berlin Heidelberg] Softcover Druck auf Anfrage Neuware - Printed after ordering - At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and making them as weak as possible. The purpose of this report is to make available to the engineering public mathematical methods for the design of supercritical wings. These methods depend on the numerical solution of the partial differential equations of two-dimensional gas dynamics. The main contribution is a computer program for the design of shockless transonic airfoils using the hodograph transformation and analytic continuation into the complex domain. Another contribution is a program for the analysis of transonic flow with shocks past an airfoil at off-design conditions. In our design work we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part. In Part III and in Appendices II and III we give numerical examples and discuss computa tional results. The main substance of the report, however, ...
ISBN10: 3540058079, ISBN13: 9783540058076, [publisher: Springer Berlin Heidelberg] Softcover Druck auf Anfrage Neuware - Printed after ordering - At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and making them as weak as possible. The purpose of this report is to make available to the engineering public mathematical methods for the design of supercritical wings. These methods depend on the numerical solution of the partial differential equations of two-dimensional gas dynamics. The main contribution is a computer program for the design of shockless transonic airfoils using the hodograph transformation and analytic continuation into the complex domain. Another contribution is a program for the analysis of transonic flow with shocks past an airfoil at off-design conditions. In our design work we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part. In Part III and in Appendices II and III we give numerical examples and discuss computa tional results. The main substance of the report, however, ...
Paperback / softback. New. At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The main contribution is a computer program for the design of shockless transonic airfoils using the hodograph transformation and analytic continuation into the complex domain. ISBN 3540058079 9783540058076 [GB]
ISBN10: 3540058079, ISBN13: 9783540058076, [publisher: Springer] Softcover Very Good [Redhill, SURRE, United Kingdom] [Publication Year: 1972]
DISCLOSURE:
When you click on links to various merchants on this site and make a purchase, this can result in this site earning a commission at no extra cost to you. Affiliate programs and affiliations include, but are not limited to, the eBay Partner Network, Amazon and Alibris.
