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.
"Sinopsis" puede pertenecer a otra edición de este libro.
From the reviews
"This reviewer found Engineering Approach to the Calculation of Aerodynamic Flows a valuable addition to his library and an excellent reference on the viscous computational aerodynamics, which this reviewer will recommend to his graduate students in aerospace engineering. Practicing engineers with an interest in aerodynamic performance prediction will also benefit fom this book." (Applied Mechanics Review, 2001)
"The theoretical aspects and the mathematical formulation of all problems is clear, accurate and carefully explained in the assumptions and approximations made (...) The physical explanation of the described phenomena is very clear and correctly placed to introduce the subjects (...) The explanations are illustrated with many simple and clear figures, which support both the mathematical treatment and the physical understanding (...) An experiment to ask some students to make use of the panel program has shown that is was rather simple to use the programs by course students." (European Journal of Mechanics B, 2001)
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.
"Sobre este título" puede pertenecer a otra edición de este libro.
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Destinos, gastos y plazos de envíoLibrería: Buchpark, Trebbin, Alemania
Condición: Sehr gut. Zustand: Sehr gut | Seiten: 416 | Sprache: Englisch | Produktart: Bücher. Nº de ref. del artículo: 187895/202
Cantidad disponible: 1 disponibles
Librería: moluna, Greven, Alemania
Gebunden. Condición: 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. Nº de ref. del artículo: 4897558
Cantidad disponible: Más de 20 disponibles
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
Buch. Condición: 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. Nº de ref. del artículo: 9783540661818
Cantidad disponible: 2 disponibles
Librería: AHA-BUCH GmbH, Einbeck, Alemania
Buch. Condición: 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. Nº de ref. del artículo: 9783540661818
Cantidad disponible: 1 disponibles
Librería: Ria Christie Collections, Uxbridge, Reino Unido
Condición: New. In. Nº de ref. del artículo: ria9783540661818_new
Cantidad disponible: Más de 20 disponibles
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
Buch. Condición: Neu. 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. Nº de ref. del artículo: 9783540661818
Cantidad disponible: 2 disponibles
Librería: Lucky's Textbooks, Dallas, TX, Estados Unidos de America
Condición: New. Nº de ref. del artículo: ABLIING23Mar3113020174066
Cantidad disponible: Más de 20 disponibles
Librería: Books Puddle, New York, NY, Estados Unidos de America
Condición: New. pp. xv + 396 1st Edition. Nº de ref. del artículo: 26348835
Cantidad disponible: 4 disponibles
Librería: Majestic Books, Hounslow, Reino Unido
Condición: New. Print on Demand pp. xv + 396. Nº de ref. del artículo: 7531900
Cantidad disponible: 4 disponibles
Librería: Mispah books, Redhill, SURRE, Reino Unido
Hardcover. Condición: Like New. Like New. book. Nº de ref. del artículo: ERICA79735406618166
Cantidad disponible: 1 disponibles