Published by LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Language: English
Seller: Books Puddle, New York, NY, U.S.A.
£ 33.83
Convert currencyQuantity: 4 available
Add to basketCondition: New.
Published by LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Language: English
Seller: moluna, Greven, Germany
£ 19.66
Convert currencyQuantity: Over 20 available
Add to basketCondition: New.
Published by LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Language: English
Seller: Revaluation Books, Exeter, United Kingdom
Paperback. Condition: Brand New. 60 pages. 8.66x5.91x0.14 inches. In Stock.
Published by LAP LAMBERT Academic Publishing Nov 2016, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Language: English
Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
£ 21.05
Convert currencyQuantity: 2 available
Add to basketTaschenbuch. Condition: 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.
Published by LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Language: English
Seller: AHA-BUCH GmbH, Einbeck, Germany
£ 21.05
Convert currencyQuantity: 1 available
Add to basketTaschenbuch. Condition: 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.
Published by LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Language: English
Seller: Majestic Books, Hounslow, United Kingdom
Condition: New. Print on Demand.
Published by LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Language: English
Seller: Biblios, Frankfurt am main, HESSE, Germany
£ 35.50
Convert currencyQuantity: 4 available
Add to basketCondition: New. PRINT ON DEMAND.
Published by LAP LAMBERT Academic Publishing Nov 2016, 2016
ISBN 10: 3659969982 ISBN 13: 9783659969980
Language: English
Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germany
£ 21.05
Convert currencyQuantity: 1 available
Add to basketTaschenbuch. Condition: 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.