Anbieter: Romtrade Corp., STERLING HEIGHTS, MI, USA
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.
Soft cover. Zustand: New. ISBN:9788184894370,Territorial restriction maybe printed on the book. This is an Int'l edition, ISBN and cover may differ from US edition, Contents same as US edition.
Zustand: New. Brand New, Softcover edition. This item may ship from the US or our Overseas warehouse depending on your location and stock availability.
Zustand: New. Brand New, Softcover edition. This item may ship from the US or our Overseas warehouse depending on your location and stock availability.
Anbieter: Anybook.com, Lincoln, Vereinigtes Königreich
EUR 31,11
Anzahl: 1 verfügbar
In den WarenkorbZustand: Fair. Volume 2. This is an ex-library book and may have the usual library/used-book markings inside.This book has hardback covers. Clean from markings. In fair condition, suitable as a study copy. No dust jacket. Please note the Image in this listing is a stock photo and may not match the covers of the actual item,700grams, ISBN:0471290467.
Anbieter: UK BOOKS STORE, London, LONDO, Vereinigtes Königreich
EUR 40,54
Anzahl: 20 verfügbar
In den WarenkorbPaperback. Zustand: New. Brand New ! Fast Delivery "International Edition " and ship within 24-48 hours. Deliver by FedEx and Dhl, & Aramex, UPS, & USPS and we do accept APO and PO BOX Addresses. Order can be delivered worldwide within 4-6 Working days .and we do have flat rate for up to 2LB. Extra shipping charges will be requested This Item May be shipped from India, United states & United Kingdom. Depending on your location and availability.
Zustand: New. pp. 592.
EUR 99,26
Anzahl: 1 verfügbar
In den WarenkorbZustand: New. pp. 592 68:B&W 7 x 10 in or 254 x 178 mm Case Laminate on White w/Gloss Lam.
Zustand: New. pp. 592.
Zustand: New. pp. 592.
Sprache: Englisch
Verlag: Kluwer Academic Publishers, Bucharest, 2003
ISBN 10: 1402016638 ISBN 13: 9781402016639
Anbieter: Ye Old Bookworm, Odessa, TX, USA
Hardcover. Zustand: Very Good. Small 4to 9" - 11" tall; 573 pages; Glossy Illustrated Boards, No Dust Jacket, Book Tight, Text is clean no markings seen; BX260.
EUR 180,07
Anzahl: Mehr als 20 verfügbar
In den WarenkorbZustand: New.
EUR 228,71
Anzahl: 1 verfügbar
In den WarenkorbZustand: New. pp. 592 67:B&W 6.69 x 9.61 in or 244 x 170 mm (Pinched Crown) Perfect Bound on White w/Gloss Lam.
Hardcover. Zustand: New. In shrink wrap. Looks like an interesting title!
Anbieter: Ria Christie Collections, Uxbridge, Vereinigtes Königreich
EUR 225,13
Anzahl: Mehr als 20 verfügbar
In den WarenkorbZustand: New. In.
Anbieter: Ria Christie Collections, Uxbridge, Vereinigtes Königreich
EUR 225,13
Anzahl: Mehr als 20 verfügbar
In den WarenkorbZustand: New. In.
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.
Sprache: Englisch
Verlag: Kluwer Academic Publishers, 2003
ISBN 10: 1402016638 ISBN 13: 9781402016639
Anbieter: Kennys Bookshop and Art Galleries Ltd., Galway, GY, Irland
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. . . . .
EUR 227,74
Anzahl: Mehr als 20 verfügbar
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.
EUR 291,78
Anzahl: 1 verfügbar
In den WarenkorbPaperback. Zustand: Like New. Like New. book.
EUR 305,32
Anzahl: 2 verfügbar
In den WarenkorbPaperback. Zustand: Brand New. 580 pages. 10.00x6.50x1.34 inches. In Stock.
EUR 292,97
Anzahl: 1 verfügbar
In den WarenkorbHardcover. Zustand: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.
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.
Sprache: Englisch
Verlag: Springer Netherlands Dez 2010, 2010
ISBN 10: 9048164451 ISBN 13: 9789048164455
Anbieter: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Deutschland
Taschenbuch. Zustand: Neu. This item is printed on demand - it takes 3-4 days longer - 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. 592 pp. Englisch.
Sprache: Englisch
Verlag: Springer Netherlands, Springer Netherlands Dez 2010, 2010
ISBN 10: 9048164451 ISBN 13: 9789048164455
Anbieter: buchversandmimpf2000, Emtmannsberg, BAYE, Deutschland
Taschenbuch. Zustand: Neu. This item is printed on demand - Print on Demand Titel. 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.Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 592 pp. Englisch.
Anbieter: Biblios, Frankfurt am main, HESSE, Deutschland
Zustand: New. PRINT ON DEMAND pp. 592.