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Taschenbuch. Zustand: Neu. Mathematical Methods in Aerodynamics | Lazãr Dragos | Taschenbuch | xvi | Englisch | 2010 | Springer Netherland | EAN 9789048164455 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu.
EUR 227,74
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In den WarenkorbZustand: New.
Sprache: Englisch
Verlag: Springer Netherlands, Springer Netherlands, 2010
ISBN 10: 9048164451 ISBN 13: 9789048164455
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Taschenbuch. Zustand: Neu. Druck auf Anfrage Neuware - Printed after ordering - The researchers in Aerodynamics know that there is not a unitary method of investigation in this field. The first mathematical model of the air plane wing, the model meaning the integral equation governing the phe nomenon, was proposed by L. Prandtl in 1918. The integral equation deduced by Prandtl, on the basis of some assumptions which will be specified in the sequeL furnishes the circulation C(y) (see Chapter 6). U sing the circulation, one calculates the lift and moment coefficients, which are very important in Aerodynamics. The first hypothesis made by Prandtl consists in replacing the wing by a distribution of vortices on the plan-form D of the wing (i. e. the projection of the wing on the plane determined by the direction of the uniform stream at infinity and t he direction of the span of the wing). Since such a distribution leads to a potential flow in the exterior of D and the experiences show that downstream the flow has not this character, Prandtl introduces as a sup plementary hypothesis another vortices distribution on the trace of the domain D in the uniform stream. The first kind of vortices are called tied vortices and the second kind of vortices are called free vortices.
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In den WarenkorbPaperback. Zustand: Brand New. 580 pages. 10.00x6.50x1.34 inches. In Stock.
Sprache: Englisch
Verlag: Kluwer Academic Publishers, 2004
ISBN 10: 1402016638 ISBN 13: 9781402016639
Anbieter: Kennys Bookstore, Olney, MD, USA
Zustand: New. Offers a unitary mathematical foundation of the basic and advanced principles of aerodynamics. This book uses a rigorous mathematical approach to present and explain classic and modern results in this field of science. Num Pages: 573 pages, biography. BIC Classification: PBW; TGMF1; TJF. Category: (P) Professional & Vocational. Dimension: 254 x 178 x 31. Weight in Grams: 1235. . 2003. Hardback. . . . . Books ship from the US and Ireland.
Buch. Zustand: Neu. Neuware - The researchers in Aerodynamics know that there is not a unitary method of investigation in this field. The first mathematical model of the air plane wing, the model meaning the integral equation governing the phe nomenon, was proposed by L. Prandtl in 1918. The integral equation deduced by Prandtl, on the basis of some assumptions which will be specified in the sequeL furnishes the circulation C(y) (see Chapter 6). U sing the circulation, one calculates the lift and moment coefficients, which are very important in Aerodynamics. The first hypothesis made by Prandtl consists in replacing the wing by a distribution of vortices on the plan-form D of the wing (i. e. the projection of the wing on the plane determined by the direction of the uniform stream at infinity and t he direction of the span of the wing). Since such a distribution leads to a potential flow in the exterior of D and the experiences show that downstream the flow has not this character, Prandtl introduces as a sup plementary hypothesis another vortices distribution on the trace of the domain D in the uniform stream. The first kind of vortices are called tied vortices and the second kind of vortices are called free vortices.