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Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition [[electronic resource] /] / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009



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Autore: Slater John W Visualizza persona
Titolo: Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition [[electronic resource] /] / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009 Visualizza cluster
Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica: 1 online resource (27 pages) : illustrations
Soggetto topico: Computational fluid dynamics 241
Data simulation
Hypersonics
Static pressure
Supersonic combustion ramjet engines
Wind tunnel tests
Aerodynamics
Boundary layers
Altri autori: SaundersJohn D  
Note generali: Title from title screen (viewed on March 3, 2011).
"May 2010."
"AIAA-2009-7349."
Nota di bibliografia: Includes bibliographical references (page 27)
Altri titoli varianti: Computational fluid dynamics
Titolo autorizzato: Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910699653003321
Lo trovi qui: Univ. Federico II
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Serie: NASA technical memorandum ; ; 216362.