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Characterization of a Transitional Hypersonic Boundary Layer: In Wind Tunnel and Flight Conditions - Softcover
Synopsis
Roughness induced boundary layer transition has been one of the main research topics for the hypersonic community over the last half- century. The major interest into the understanding of this phenomenon relies in the key role played by transition prediction methods on hypersonic vehicles thermal protection system (TPS) design. Several boundary layer transition predictions methods have been developed but a review of these transition criteria reveals a lack a physics associated with these engineering methods together with a lack of reliable flight data. The work presented in this thesis is a first step trying to fill this gap. First, the physical mechanisms associated with hypersonic roughness induced transition are investigated both experimentally and numerically. Secondly, an hypersonic roughness induced transition experiment has been developed for the EXPERT mission, aiming to obtain high quality flight data.
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About the Author
Dr Sandy Tirtey has been involved in several hypersonic re-entry flight projects: EXPERT, CubeSat, HIFiRE and more recently, the SCRAMSPACE project as the technical lead of the SCRAMSPACE I hypersonic flight experiment. His fields of expertise are: hypersonic flight testing, roughness induced transition, scramjets and thermo-structural analyses.
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- PublisherLAP LAMBERT Academic Publishing
- Publication date2010
- ISBN 10 3843353247
- ISBN 13 9783843353243
- BindingPaperback
- LanguageEnglish
- Number of pages240
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Characterization of a Transitional Hypersonic Boundary Layer
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LAP LAMBERT Academic Publishing Okt 2010, 2010
ISBN 10: 3843353247
ISBN 13: 9783843353243
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Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Roughness induced boundary layer transition has been one of the main research topics for the hypersonic community over the last half- century. The major interest into the understanding of this phenomenon relies in the key role played by transition prediction methods on hypersonic vehicles thermal protection system (TPS) design. Several boundary layer transition predictions methods have been developed but a review of these transition criteria reveals a lack a physics associated with these engineering methods together with a lack of reliable flight data. The work presented in this thesis is a first step trying to fill this gap. First, the physical mechanisms associated with hypersonic roughness induced transition are investigated both experimentally and numerically. Secondly, an hypersonic roughness induced transition experiment has been developed for the EXPERT mission, aiming to obtain high quality flight data. 240 pp. Englisch. Seller Inventory # 9783843353243
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Characterization of a Transitional Hypersonic Boundary Layer : In Wind Tunnel and Flight Conditions
Published by
LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843353247
ISBN 13: 9783843353243
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Taschenbuch
Seller: AHA-BUCH GmbH, Einbeck, Germany
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Roughness induced boundary layer transition has been one of the main research topics for the hypersonic community over the last half- century. The major interest into the understanding of this phenomenon relies in the key role played by transition prediction methods on hypersonic vehicles thermal protection system (TPS) design. Several boundary layer transition predictions methods have been developed but a review of these transition criteria reveals a lack a physics associated with these engineering methods together with a lack of reliable flight data. The work presented in this thesis is a first step trying to fill this gap. First, the physical mechanisms associated with hypersonic roughness induced transition are investigated both experimentally and numerically. Secondly, an hypersonic roughness induced transition experiment has been developed for the EXPERT mission, aiming to obtain high quality flight data. Seller Inventory # 9783843353243
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Characterization of a Transitional Hypersonic Boundary Layer
Published by
LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843353247
ISBN 13: 9783843353243
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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Tirtey SandyDr Sandy Tirtey has been involved in several hypersonic re-entry flight projects: EXPERT, CubeSat, HIFiRE and more recently, the SCRAMSPACE project as the technical lead of the SCRAMSPACE I hypersonic flight experiment. Seller Inventory # 5465332
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Characterization of a Transitional Hypersonic Boundary Layer: In Wind Tunnel and Flight Conditions
Published by
LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843353247
ISBN 13: 9783843353243
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