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EUR 12,11
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Lingua: Inglese
Editore: British Library, Historical Print Editions, 2011
ISBN 10: 1241784477 ISBN 13: 9781241784478
Da: Ria Christie Collections, Uxbridge, Regno Unito
EUR 25,26
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Aggiungi al carrelloCondizione: New. In.
Lingua: Inglese
Editore: British Library, Historical Print Editions 2011-06, 2011
ISBN 10: 1241784477 ISBN 13: 9781241784478
Da: Chiron Media, Wallingford, Regno Unito
EUR 20,61
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Aggiungi al carrelloPF. Condizione: New.
EUR 12,11
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EUR 14,22
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Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Lingua: Inglese
Editore: British Library, Historical Print Editions Jun 2011, 2011
ISBN 10: 1241784477 ISBN 13: 9781241784478
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 37,53
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. Neuware.
Da: Ammareal, Morangis, Francia
EUR 130,73
Quantità: 1 disponibili
Aggiungi al carrelloHardcover. Condizione: Très bon. Ancien livre de bibliothèque avec équipements. Edition 1995. Ammareal reverse jusqu'à 15% du prix net de cet article à des organisations caritatives. ENGLISH DESCRIPTION Book Condition: Used, Very good. Former library book. Edition 1995. Ammareal gives back up to 15% of this item's net price to charity organizations.
Da: moluna, Greven, Germania
EUR 180,07
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Da: moluna, Greven, Germania
EUR 180,07
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Aggiungi al carrelloGebunden. Condizione: New.
Da: Ria Christie Collections, Uxbridge, Regno Unito
EUR 228,94
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Da: Ria Christie Collections, Uxbridge, Regno Unito
EUR 228,94
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Aggiungi al carrelloCondizione: New. In.
Da: Buchpark, Trebbin, Germania
EUR 161,66
Quantità: 1 disponibili
Aggiungi al carrelloCondizione: Sehr gut. Zustand: Sehr gut | Seiten: 364 | Sprache: Englisch | Produktart: Bücher | The book is concerned with mathematical modelling of supersonic and hyper sonic flows about bodies. Permanent interest in this topic is stimulated, first of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of gas dynamic and physical effects caused by rarefaction, viscous-inviscid interaction, separation, various physical and chemical processes induced by gas heating in the intensive bow shock wave. The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat eral parts of the body surface. A conventional approach to calculation of shock layer flows consists in a successive solution of the inviscid gas and boundary layer equations. When the afore-mentioned effects become important, implementation of these models meets difficulties or even becomes impossible. In this case, one has to use a more general approach based on the viscous shock layer concept.
Lingua: Inglese
Editore: Kluwer Academic Publishers, 1995
ISBN 10: 0792336267 ISBN 13: 9780792336266
Da: Kennys Bookshop and Art Galleries Ltd., Galway, GY, Irlanda
EUR 258,09
Quantità: 15 disponibili
Aggiungi al carrelloCondizione: New. This volume examines the numerical simulation of supersonic and hypersonic flows around bodies. It takes account of the effects of rarefaction, viscous-inviscid interaction, separation, chemical and thermal non-equilibria, and radiation. A number of example calculations are given. Series: Fluid Mechanics and its Applications. Num Pages: 358 pages, biography. BIC Classification: PH; TGMF1. Category: (P) Professional & Vocational; (UP) Postgraduate, Research & Scholarly. Dimension: 234 x 156 x 20. Weight in Grams: 686. . 1995. Hardback. . . . .
Condizione: New. pp. 364.
Condizione: New. pp. 364 Softcover reprint of hardcover 1st ed. 1995 edition.
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 223,11
Quantità: 1 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. Druck auf Anfrage Neuware - Printed after ordering - The book is concerned with mathematical modelling of supersonic and hyper sonic flows about bodies. Permanent interest in this topic is stimulated, first of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of gas dynamic and physical effects caused by rarefaction, viscous-inviscid interaction, separation, various physical and chemical processes induced by gas heating in the intensive bow shock wave. The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat eral parts of the body surface. A conventional approach to calculation of shock layer flows consists in a successive solution of the inviscid gas and boundary layer equations. When the afore-mentioned effects become important, implementation of these models meets difficulties or even becomes impossible. In this case, one has to use a more general approach based on the viscous shock layer concept.
Lingua: Inglese
Editore: Springer Netherlands, Springer Netherlands, 1995
ISBN 10: 0792336267 ISBN 13: 9780792336266
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 223,11
Quantità: 1 disponibili
Aggiungi al carrelloBuch. Condizione: Neu. Druck auf Anfrage Neuware - Printed after ordering - The book is concerned with mathematical modelling of supersonic and hyper sonic flows about bodies. Permanent interest in this topic is stimulated, first of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of gas dynamic and physical effects caused by rarefaction, viscous-inviscid interaction, separation, various physical and chemical processes induced by gas heating in the intensive bow shock wave. The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat eral parts of the body surface. A conventional approach to calculation of shock layer flows consists in a successive solution of the inviscid gas and boundary layer equations. When the afore-mentioned effects become important, implementation of these models meets difficulties or even becomes impossible. In this case, one has to use a more general approach based on the viscous shock layer concept.
Da: Revaluation Books, Exeter, Regno Unito
EUR 304,63
Quantità: 2 disponibili
Aggiungi al carrelloPaperback. Condizione: Brand New. 346 pages. 9.25x6.25x0.82 inches. In Stock.
Da: Mispah books, Redhill, SURRE, Regno Unito
EUR 306,40
Quantità: 1 disponibili
Aggiungi al carrelloPaperback. Condizione: Like New. Like New. book.
Da: Mispah books, Redhill, SURRE, Regno Unito
EUR 306,40
Quantità: 1 disponibili
Aggiungi al carrelloHardcover. Condizione: Like New. Like New. book.
Lingua: Inglese
Editore: Kluwer Academic Publishers, 1995
ISBN 10: 0792336267 ISBN 13: 9780792336266
Da: Kennys Bookstore, Olney, MD, U.S.A.
Condizione: New. This volume examines the numerical simulation of supersonic and hypersonic flows around bodies. It takes account of the effects of rarefaction, viscous-inviscid interaction, separation, chemical and thermal non-equilibria, and radiation. A number of example calculations are given. Series: Fluid Mechanics and its Applications. Num Pages: 358 pages, biography. BIC Classification: PH; TGMF1. Category: (P) Professional & Vocational; (UP) Postgraduate, Research & Scholarly. Dimension: 234 x 156 x 20. Weight in Grams: 686. . 1995. Hardback. . . . . Books ship from the US and Ireland.
Da: BUCHSERVICE / ANTIQUARIAT Lars Lutzer, Wahlstedt, Germania
EUR 429,90
Quantità: 1 disponibili
Aggiungi al carrelloHardcover. Condizione: gut. Numerical Simulation of Viscous Shock Layer Flows (Fluid Mechanics and Its Applications, 33) In englischer Sprache. pages.
Da: PBShop.store US, Wood Dale, IL, U.S.A.
EUR 14,49
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Aggiungi al carrelloPAP. Condizione: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
Lingua: Inglese
Editore: British Library, Historical Print Editions, 2011
ISBN 10: 1241784477 ISBN 13: 9781241784478
Da: PBShop.store US, Wood Dale, IL, U.S.A.
EUR 28,24
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Aggiungi al carrelloPAP. Condizione: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
Lingua: Inglese
Editore: British Library, Historical Print Editions, 2011
ISBN 10: 1241784477 ISBN 13: 9781241784478
Da: PBShop.store UK, Fairford, GLOS, Regno Unito
EUR 25,20
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Aggiungi al carrelloPAP. Condizione: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
Da: PBShop.store UK, Fairford, GLOS, Regno Unito
EUR 13,62
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Aggiungi al carrelloPAP. Condizione: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
Editore: British Library, Historical Print Editions, 2011
ISBN 10: 1241784477 ISBN 13: 9781241784478
Da: moluna, Greven, Germania
EUR 30,25
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Aggiungi al carrelloCondizione: New.
Lingua: Inglese
Editore: British Library, Historical Print Editions, 2011
ISBN 10: 1241784477 ISBN 13: 9781241784478
Da: Majestic Books, Hounslow, Regno Unito
EUR 43,45
Quantità: 4 disponibili
Aggiungi al carrelloCondizione: New. Print on Demand pp. 292.