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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.
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"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)
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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.
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Engineering Approach to the Calculation of Aerodynamic Flows
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An Engineering Approach to the Calculation of Aerodynamic Flows
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An Engineering Approach to the Calculation of Aerodynamic Flows (Hardcover)
ISBN 10: 3540661816
ISBN 13: 9783540661818
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Hardcover. Zustand: new. Hardcover. 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. This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. Bestandsnummer des Verkäufers 9783540661818
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An Engineering Approach to the Calculation of Aerodynamic Flows
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An Engineering Approach to the Calculation of Aerodynamic Flows
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Springer Berlin Heidelberg Nov 1999, 1999
ISBN 10: 3540661816
ISBN 13: 9783540661818
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Buch. Zustand: 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. Bestandsnummer des Verkäufers 9783540661818
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An Engineering Approach to the Calculation of Aerodynamic Flows
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Gebunden. Zustand: 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. Bestandsnummer des Verkäufers 4897558
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An Engineering Approach to the Calculation of Aerodynamic Flows
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Zustand: New. pp. xv + 396 1st Edition. Bestandsnummer des Verkäufers 26348835
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An Engineering Approach to the Calculation of Aerodynamic Flows
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Zustand: New. pp. xv + 396. Bestandsnummer des Verkäufers 7531900
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An Engineering Approach to the Calculation of Aerodynamic Flows
ISBN 10: 3540661816
ISBN 13: 9783540661818
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Buch. Zustand: 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. Bestandsnummer des Verkäufers 9783540661818
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Buch. Zustand: 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. Bestandsnummer des Verkäufers 9783540661818
Anzahl: 1 verfügbar