Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: Books Puddle, New York, NY, U.S.A.
Condizione: New.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: Revaluation Books, Exeter, Regno Unito
EUR 42,20
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Aggiungi al carrelloPaperback. Condizione: Brand New. 60 pages. 8.66x5.91x0.14 inches. In Stock.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: moluna, Greven, Germania
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Aggiungi al carrelloKartoniert / Broschiert. Condizione: New.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: Majestic Books, Hounslow, Regno Unito
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Aggiungi al carrelloCondizione: New. Print on Demand.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing Nov 2016, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
EUR 23,90
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The characterization of rocket aerodynamics is a prerequisite for the design and operation of these vehicles. In order to determine its trajectory, it is necessary to know the aerodynamic characteristics in all phases of flight. One way to obtain the aerodynamic characteristics of a rocket is by means of numerical simulations of the flow along the rocket. To this end, the region around the rocket is discretized into a computational mesh that is then used for the numerical solution of the equations governing the flow. The purpose of this book is to show the work of generating computational meshes in rockets and assess their suitability for flow simulation at different speed regimes. These simulations will be performed with the NS3D program that numerically solves the 3-D Navier-Stokes of turbulent flows. These simulations will be validated by comparing the calculated results with experimental data. 60 pp. Englisch.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: Biblios, Frankfurt am main, HESSE, Germania
EUR 41,36
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Aggiungi al carrelloCondizione: New. PRINT ON DEMAND.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 23,90
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The characterization of rocket aerodynamics is a prerequisite for the design and operation of these vehicles. In order to determine its trajectory, it is necessary to know the aerodynamic characteristics in all phases of flight. One way to obtain the aerodynamic characteristics of a rocket is by means of numerical simulations of the flow along the rocket. To this end, the region around the rocket is discretized into a computational mesh that is then used for the numerical solution of the equations governing the flow. The purpose of this book is to show the work of generating computational meshes in rockets and assess their suitability for flow simulation at different speed regimes. These simulations will be performed with the NS3D program that numerically solves the 3-D Navier-Stokes of turbulent flows. These simulations will be validated by comparing the calculated results with experimental data.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing Nov 2016, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
EUR 23,90
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The characterization of rocket aerodynamics is a prerequisite for the design and operation of these vehicles. In order to determine its trajectory, it is necessary to know the aerodynamic characteristics in all phases of flight. One way to obtain the aerodynamic characteristics of a rocket is by means of numerical simulations of the flow along the rocket. To this end, the region around the rocket is discretized into a computational mesh that is then used for the numerical solution of the equations governing the flow. The purpose of this book is to show the work of generating computational meshes in rockets and assess their suitability for flow simulation at different speed regimes. These simulations will be performed with the NS3D program that numerically solves the 3-D Navier-Stokes of turbulent flows. These simulations will be validated by comparing the calculated results with experimental data.Books on Demand GmbH, Überseering 33, 22297 Hamburg 60 pp. Englisch.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Da: preigu, Osnabrück, Germania
EUR 22,35
Quantitą: 5 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. Numerical Simulation of the Flow Field Over Sounding Rockets | Frederico Farias (u. a.) | Taschenbuch | 60 S. | Englisch | 2016 | LAP LAMBERT Academic Publishing | EAN 9783659969980 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu Print on Demand.