EUR 71,15
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloCloth. Condizione: Fine. 230 pp. Tightly bound. Corners not bumped. Text is free of markings. Book still in original shrink wrap. Contains CD-ROM.
EUR 87,06
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloCondizione: New. pp. xii + 226 1st Edition.
EUR 87,91
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloCondizione: New. pp. xii + 226.
EUR 101,68
Convertire valutaQuantità: 15 disponibili
Aggiungi al carrelloCondizione: New.
Editore: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG, Berlin, 2014
ISBN 10: 3642444962 ISBN 13: 9783642444968
Lingua: Inglese
Da: Grand Eagle Retail, Mason, OH, U.S.A.
EUR 104,01
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloPaperback. Condizione: new. Paperback. 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. 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. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.
EUR 101,70
Convertire valutaQuantità: 15 disponibili
Aggiungi al carrelloCondizione: New.
EUR 96,14
Convertire valutaQuantità: 2 disponibili
Aggiungi al carrelloCondizione: New. SUPER FAST SHIPPING.
EUR 96,14
Convertire valutaQuantità: 2 disponibili
Aggiungi al carrelloCondizione: New. SUPER FAST SHIPPING.
EUR 91,38
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloCondizione: New. pp. xii + 226.
EUR 101,95
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
EUR 102,28
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
EUR 115,96
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Editore: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG, Berlin, 2005
ISBN 10: 3540229329 ISBN 13: 9783540229322
Lingua: Inglese
Da: Grand Eagle Retail, Mason, OH, U.S.A.
EUR 117,70
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloHardcover. Condizione: new. Hardcover. This book provides an introduction to unsteady aerodynamics with emphasis on the analysis and computation of inviscid and viscous two-dimensional flows over airfoils at low speeds. It begins with a discussion of the physics of unsteady flows and an explanation of lift and thrust generation, airfoil flutter, gust response and dynamic stall. This is followed by an exposition of the four major calculation methods in currents use, namely inviscid-panel, boundary-layer, viscous-inviscid interaction and Navier-Stokes methods. Examples are provided to demonstrate the use of each method and panel and interactive boundary layer codes are included on the CD-ROM. Undergraduate and graduate students, teachers, scientists and engineers concerned with aeronautical, hydronautical and mechanical engineering problems will gain understanding of the physics of unsteady low-speed flows and an ability to analyze these flows with modern computational methods. 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. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.
EUR 88,83
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloCondizione: Fair. This is an ex-library book and may have the usual library/used-book markings inside.This book has soft covers. In fair condition, suitable as a study copy. Please note the Image in this listing is a stock photo and may not match the covers of the actual item,500grams, ISBN:9783642444968.
EUR 115,72
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrellohardcover. Condizione: New. In shrink wrap. Looks like an interesting title!
EUR 120,74
Convertire valutaQuantità: 15 disponibili
Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
EUR 121,12
Convertire valutaQuantità: 15 disponibili
Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
EUR 111,18
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New. In.
EUR 111,18
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New. In.
EUR 126,50
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Editore: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG, 2014
ISBN 10: 3642444962 ISBN 13: 9783642444968
Lingua: Inglese
Da: Kennys Bookshop and Art Galleries Ltd., Galway, GY, Irlanda
EUR 128,43
Convertire valutaQuantità: 15 disponibili
Aggiungi al carrelloCondizione: New. Num Pages: 238 pages, 3 black & white tables, biography. BIC Classification: PBKS; PHD; PHDF; PHU; TGB. Category: (G) General (US: Trade). Dimension: 235 x 155 x 13. Weight in Grams: 379. . 2014. Paperback. . . . .
Da: Kennys Bookshop and Art Galleries Ltd., Galway, GY, Irlanda
EUR 129,73
Convertire valutaQuantità: 15 disponibili
Aggiungi al carrelloCondizione: New. 2005. 2005th Edition. hardcover. . . . . .
EUR 141,55
Convertire valutaQuantità: 4 disponibili
Aggiungi al carrelloCondizione: New.
Editore: Springer Berlin Heidelberg, 2014
ISBN 10: 3642444962 ISBN 13: 9783642444968
Lingua: Inglese
Da: moluna, Greven, Germania
EUR 92,27
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Editore: Springer Berlin Heidelberg, 2005
ISBN 10: 3540229329 ISBN 13: 9783540229322
Lingua: Inglese
Da: moluna, Greven, Germania
EUR 92,27
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloGebunden. Condizione: New.
Editore: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG, 2014
ISBN 10: 3642444962 ISBN 13: 9783642444968
Lingua: Inglese
Da: Kennys Bookstore, Olney, MD, U.S.A.
EUR 159,87
Convertire valutaQuantità: 15 disponibili
Aggiungi al carrelloCondizione: New. Num Pages: 238 pages, 3 black & white tables, biography. BIC Classification: PBKS; PHD; PHDF; PHU; TGB. Category: (G) General (US: Trade). Dimension: 235 x 155 x 13. Weight in Grams: 379. . 2014. Paperback. . . . . Books ship from the US and Ireland.
EUR 161,51
Convertire valutaQuantità: 15 disponibili
Aggiungi al carrelloCondizione: New. 2005. 2005th Edition. hardcover. . . . . . Books ship from the US and Ireland.
Editore: Springer Berlin Heidelberg Nov 2014, 2014
ISBN 10: 3642444962 ISBN 13: 9783642444968
Lingua: Inglese
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
EUR 106,99
Convertire valutaQuantità: 2 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. 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.Springer-Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 244 pp. Englisch.
Editore: Springer Berlin Heidelberg, Springer Berlin Heidelberg Feb 2005, 2005
ISBN 10: 3540229329 ISBN 13: 9783540229322
Lingua: Inglese
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
EUR 106,99
Convertire valutaQuantità: 2 disponibili
Aggiungi al carrelloBuch. Condizione: Neu. 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.
Editore: Springer Berlin Heidelberg, 2014
ISBN 10: 3642444962 ISBN 13: 9783642444968
Lingua: Inglese
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 106,99
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: 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.