An Engineering Approach to the Calculation of Aerodynamic Flows

Tuncer Cebeci

ISBN 10: 3540661816 ISBN 13: 9783540661818

Edit� par Springer, 1999

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Synopsis :

This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. The contents include two-dimensional and three-dimensional steady and unsteady flows with and without compressibility effects. The former theory is based on the numerical solutions of the reduced Navier-Stokes equations in which Euler and boundary-layer equations are coupled with an interaction law. The latter theory is based on the linear stability theory and employs the so-called en method. The book details applications of this approach to airfoils, wings and high lift systems. It is intended for undergraduate and graduate students and practicing engineers interested in aerodynamics, hydrodynamics and modern numerical methods and computer programs for solving linear and nonlinear ordinary and parabolic partial differential equations.

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Titre : An Engineering Approach to the Calculation ...
�diteur : Springer
Date d'�dition : 1999
Reliure : Buch
Etat : Neu

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An Engineering Approach to the Calculation of Aerodynamic Flows

Cebeci, Tuncer

Edit� par Springer Verlag, 1999

ISBN 10 : 3540661816 ISBN 13 : 9783540661818

Ancien ou d'occasion Couverture rigide

Vendeur : Libreria sottomarina - Studio Bibliografico, ROMA, RM, Italie

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rilegato hardcover. Etat : Fine. Book. N� de r�f. du vendeur G7204dz06

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An Engineering Approach to the Calculation of Aerodynamic Flows

Cebeci, Tuncer

Edit� par J.B. Metzler, 1999

ISBN 10 : 3540661816 ISBN 13 : 9783540661818

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Vendeur : Buchpark, Trebbin, Allemagne

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Etat : Sehr gut. Zustand: Sehr gut | Seiten: 416 | Sprache: Englisch | Produktart: B�cher | This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. The contents include two-dimensional and three-dimensional steady and unsteady flows with and without compressibility effects. The former theory is based on the numerical solutions of the reduced Navier-Stokes equations in which Euler and boundary-layer equations are coupled with an interaction law. The latter theory is based on the linear stability theory and employs the so-called en method. The book details applications of this approach to airfoils, wings and high lift systems. It is intended for undergraduate and graduate students and practicing engineers interested in aerodynamics, hydrodynamics and modern numerical methods and computer programs for solving linear and nonlinear ordinary and parabolic partial differential equations. N� de r�f. du vendeur 187895/202

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An Engineering Approach to the Calculation of Aerodynamic Flows

Tuncer Cebeci

Edit� par Springer Berlin Heidelberg, 1999

ISBN 10 : 3540661816 ISBN 13 : 9783540661818

Neuf Couverture rigide

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Gebunden. Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. This is the first time the powerful computational techniques developed by the author are published in book formHis algorithms are used in the airplane industry (Douglas-McDonald, Boeing)This book describes an engineering approach based on interac. N� de r�f. du vendeur 4897558

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An Engineering Approach to the Calculation of Aerodynamic Flows

Tuncer Cebeci

Edit� par Springer Berlin Heidelberg, Springer Nov 1999, 1999

ISBN 10 : 3540661816 ISBN 13 : 9783540661818

Neuf Couverture rigide

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Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne

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Buch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. The contents include two-dimensional and three-dimensional steady and unsteady flows with and without compressibility effects. The former theory is based on the numerical solutions of the reduced Navier-Stokes equations in which Euler and boundary-layer equations are coupled with an interaction law. The latter theory is based on the linear stability theory and employs the so-called en method. The book details applications of this approach to airfoils, wings and high lift systems. It is intended for undergraduate and graduate students and practicing engineers interested in aerodynamics, hydrodynamics and modern numerical methods and computer programs for solving linear and nonlinear ordinary and parabolic partial differential equations.Springer-Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 416 pp. Englisch. N� de r�f. du vendeur 9783540661818

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An Engineering Approach to the Calculation of Aerodynamic Flows

Tuncer Cebeci

Edit� par Springer Berlin Heidelberg Nov 1999, 1999

ISBN 10 : 3540661816 ISBN 13 : 9783540661818

Neuf Couverture rigide

impression � la demande

Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne

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Buch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. This is the first time these powerful computational techniques have been published in book form. 416 pp. Englisch. N� de r�f. du vendeur 9783540661818

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An Engineering Approach to the Calculation of Aerodynamic Flows

Tuncer Cebeci

Edit� par Springer Berlin Heidelberg, Springer Berlin Heidelberg, 1999

ISBN 10 : 3540661816 ISBN 13 : 9783540661818

Neuf Couverture rigide

Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne

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Buch. Etat : Neu. Druck auf Anfrage Neuware - Printed after ordering - This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. The contents include two-dimensional and three-dimensional steady and unsteady flows with and without compressibility effects. The former theory is based on the numerical solutions of the reduced Navier-Stokes equations in which Euler and boundary-layer equations are coupled with an interaction law. The latter theory is based on the linear stability theory and employs the so-called en method. The book details applications of this approach to airfoils, wings and high lift systems. It is intended for undergraduate and graduate students and practicing engineers interested in aerodynamics, hydrodynamics and modern numerical methods and computer programs for solving linear and nonlinear ordinary and parabolic partial differential equations. N� de r�f. du vendeur 9783540661818

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