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Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction / / Hyun D. Kim, Warren R. Hingst, and David O. Davis



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Autore: Kim Hyun Dae Visualizza persona
Titolo: Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction / / Hyun D. Kim, Warren R. Hingst, and David O. Davis Visualizza cluster
Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996
Descrizione fisica: 1 online resource (9 pages) : illustrations
Soggetto topico: Boundary layer control
Pressure measurement
Flow visualization
Turbulent boundary layer
Mass flow rate
Static pressure
Shock waves
Persona (resp. second.): HingstWarren R.
DavisDavid O.
Note generali: Title from title screen (viewed Aug. 9, 2016).
"December 1996"--Report documentation page.
"Prepared for the 35th Aerospace Sciences Meeting and Exhibit cosponsored by AIAA, ASME, SAE, and ASME, Reno, Nevada, January 6-10, 1997."
"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
"AIAA-97-0608."
Nota di bibliografia: Includes bibliographical references (page 9).
Titolo autorizzato: Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910707497503321
Lo trovi qui: Univ. Federico II
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