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Record Nr. |
UNINA9910704277603321 |
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Autore |
Davis David O. |
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Titolo |
CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / / David O. Davis |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015 |
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Descrizione fisica |
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1 online resource (13 pages) : color illustrations |
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Collana |
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Soggetti |
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Boundary layers |
Computational fluid dynamics |
Shock wave interaction |
Flow measurement |
Turbulent flow |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from title screen (viewed on Feb. 2, 2016). |
"September 2015." |
"Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015 |
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Nota di bibliografia |
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Includes bibliographical references (page 13). |
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