9781402016639 - Mathematical Methods in Aerodynamics von Dragos, Lazãr (6 Ergebnisse)

Zustand: New. Brand New. Soft Cover International Edition. Different ISBN and Cover Image. Priced lower than the standard editions which is usually intended to make them more affordable for students abroad. The core content of the book is generally the same as the standard edition. The country selling restrictions may be printed on the book but is no problem for the self-use. This Item maybe shipped from US or any other country as we have multiple locations worldwide.

Zustand: New. pp. 592 68:B&W 7 x 10 in or 254 x 178 mm Case Laminate on White w/Gloss Lam.

Zustand: New. In.

Zustand: New.

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.