Isbn: 9783540229322 - analysis of low-speed unsteady airfoil flows (13 resultados)

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    • Idioma: Inglés

      Editorial: Springer, New York, NY, 2005

      3540229329 / 9783540229322

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      Librería: Book Bear, West Brookfield, MA, Estados Unidos de AmericaBook Bear

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      Condición: Usado - Excelente

      EUR 71,93

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      Cloth. Condición: Fine. Estado de la sobrecubierta: Printed Boards. 230 pp. Tightly bound. Corners not bumped. Text is free of markings. Book still in original shrink wrap. Contains CD-ROM.

    • Idioma: Inglés

      Editorial: Springer, 2005

      3540229329 / 9783540229322

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      Librería: Books Puddle, New York, NY, Estados Unidos de AmericaBooks Puddle

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      Condición: Nuevo

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      Condición: New. pp. xii + 226 2005th edition.

    • Idioma: Inglés

      Editorial: Springer, 2005

      3540229329 / 9783540229322

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      Librería: Majestic Books, Hounslow, Reino UnidoMajestic Books

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      Cantidad disponible: 1 disponibles

      Condición: New. pp. xii + 226.

    • Idioma: Inglés

      Editorial: Springer, 2005

      3540229329 / 9783540229322

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      Librería: Biblios, frankfurt am main, HESSE, AlemaniaBiblios

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      Condición: Nuevo

      EUR 85,90

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      Cantidad disponible: 1 disponibles

      Condición: New. pp. xii + 226.

    • Idioma: Inglés

      Editorial: Springer, 2005

      3540229329 / 9783540229322

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      Librería: Mispah books, Redhill, SURRE, Reino UnidoMispah books

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      Condición: Usado - Como Nuevo

      EUR 78,07

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      Cantidad disponible: 1 disponibles

      Hardcover. Condición: Like New. Like NewLIKE NEW. book.

    • Idioma: Inglés

      Editorial: Springer, 2005

      3540229329 / 9783540229322

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      Librería: BennettBooksLtd, Los Angeles, CA, Estados Unidos de AmericaBennettBooksLtd

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      Condición: Nuevo

      EUR 117,02

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      Cantidad disponible: 1 disponibles

      hardcover. Condición: New. In shrink wrap. Looks like an interesting title.

    • Idioma: Inglés

      Editorial: Springer, 2005

      3540229329 / 9783540229322

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      Librería: Ria Christie Collections, Uxbridge, Reino UnidoRia Christie Collections

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      EUR 116,37

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      Cantidad disponible: Más de 20 disponibles

      Condición: New. In.

    • Idioma: Inglés

      Editorial: Springer Berlin Heidelberg, 2005

      3540229329 / 9783540229322

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      Librería: moluna, Greven, Alemaniamoluna

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      Condición: Nuevo

      EUR 92,27

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      Cantidad disponible: Más de 20 disponibles

      Gebunden. Condición: New.

    • Idioma: Inglés

      Editorial: Springer Verlag, 2005

      3540229329 / 9783540229322

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      Librería: Revaluation Books, Exeter, Reino UnidoRevaluation Books

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      Condición: Nuevo

      EUR 154,33

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      Cantidad disponible: 2 disponibles

      Hardcover. Condición: Brand New. hardback/cd-rom edition. 226 pages. 9.50x6.50x0.50 inches. In Stock.

    • Idioma: Inglés

      Editorial: Springer Berlin Heidelberg, Springer Berlin Heidelberg, 2005

      3540229329 / 9783540229322

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      Librería: AHA-BUCH GmbH, Einbeck, AlemaniaAHA-BUCH GmbH

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      Condición: Nuevo

      EUR 106,99

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      Buch. Condición: Neu. Druck auf Anfrage Neuware - Printed after ordering - The standard textbooks on aerodynamics usually omit any discussion of un steady aerodynamics or, at most, consider it only in a single chapter, based on two justifications. The first is that unsteady aerodynamics should be regarded as a specialized subject required 'only' in connection with understanding and an alyzing aeroelastic phenomena such as flutter and gust response, and therefore should be dealt with in related specialist books. The second reason appears to be reluctance to discuss aerodynamics with the inclusion of the time-dependent terms in the conservation equations and the boundary conditions for fear that added complications may discourage the reader. We take the opposite view in this book and argue that a full understanding of the physics of lift generation is possible only by considering the unsteady aerody namics of the starting vortex generation process. Furthermore, certain 'steady' flows are inherently unsteady in the presence of flow separation, as for example the unsteady flow caused by the Karman vortex shedding downstream of a cylin der and 'static' airfoil stall which is an inherently unsteady flow phenomenon. Therefore, it stands to reason that a unified treatment of aerodynamics that yields steady-state aerodynamics as a special case offers advantages. This rea soning is strengthened by the developments in computational fluid dynamics over the past forty years, which showed that accurate steady-state solutions can be obtained efficiently by solving the unsteady flow equations.

    • Idioma: Inglés

      Editorial: Springer Berlin Heidelberg Feb 2005, 2005

      3540229329 / 9783540229322

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      Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, AlemaniaBuchWeltWeit Ludwig Meier e.K.

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      EUR 106,99

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      Buch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The standard textbooks on aerodynamics usually omit any discussion of un steady aerodynamics or, at most, consider it only in a single chapter, based on two justifications. The first is that unsteady aerodynamics should be regarded as a specialized subject required 'only' in connection with understanding and an alyzing aeroelastic phenomena such as flutter and gust response, and therefore should be dealt with in related specialist books. The second reason appears to be reluctance to discuss aerodynamics with the inclusion of the time-dependent terms in the conservation equations and the boundary conditions for fear that added complications may discourage the reader. We take the opposite view in this book and argue that a full understanding of the physics of lift generation is possible only by considering the unsteady aerody namics of the starting vortex generation process. Furthermore, certain 'steady' flows are inherently unsteady in the presence of flow separation, as for example the unsteady flow caused by the Karman vortex shedding downstream of a cylin der and 'static' airfoil stall which is an inherently unsteady flow phenomenon. Therefore, it stands to reason that a unified treatment of aerodynamics that yields steady-state aerodynamics as a special case offers advantages. This rea soning is strengthened by the developments in computational fluid dynamics over the past forty years, which showed that accurate steady-state solutions can be obtained efficiently by solving the unsteady flow equations. 240 pp. Englisch.

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      Idioma: Inglés

      Editorial: Springer-Verlag GmbH, 2005

      3540229329 / 9783540229322

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      Librería: preigu, Osnabrück, Alemaniapreigu

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      Buch. Condición: Neu. Analysis of Low-Speed Unsteady Airfoil Flows | Tuncer Cebeci (u. a.) | Buch | Englisch | 2005 | Springer-Verlag GmbH | EAN 9783540229322 | Verantwortliche Person für die EU: Springer-Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, productsafety[at]springernature[dot]com | Anbieter: preigu Print on Demand.

    • Idioma: Inglés

      Editorial: Springer Berlin Heidelberg, Springer Berlin Heidelberg Feb 2005, 2005

      3540229329 / 9783540229322

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      Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemaniabuchversandmimpf2000

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      Condición: Nuevo

      EUR 106,99

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      Buch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The standard textbooks on aerodynamics usually omit any discussion of un steady aerodynamics or, at most, consider it only in a single chapter, based on two justifications. The first is that unsteady aerodynamics should be regarded as a specialized subject required 'only' in connection with understanding and an alyzing aeroelastic phenomena such as flutter and gust response, and therefore should be dealt with in related specialist books. The second reason appears to be reluctance to discuss aerodynamics with the inclusion of the time-dependent terms in the conservation equations and the boundary conditions for fear that added complications may discourage the reader. We take the opposite view in this book and argue that a full understanding of the physics of lift generation is possible only by considering the unsteady aerody namics of the starting vortex generation process. Furthermore, certain 'steady' flows are inherently unsteady in the presence of flow separation, as for example the unsteady flow caused by the Karman vortex shedding downstream of a cylin der and 'static' airfoil stall which is an inherently unsteady flow phenomenon. Therefore, it stands to reason that a unified treatment of aerodynamics that yields steady-state aerodynamics as a special case offers advantages. This rea soning is strengthened by the developments in computational fluid dynamics over the past forty years, which showed that accurate steady-state solutions can be obtained efficiently by solving the unsteady flow equations. 240 pp. Englisch.