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| Autore: |
Kim Hyun Dae
|
| Titolo: |
Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction / / Hyun D. Kim, Warren R. Hingst, and David O. Davis
|
| 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 ![]() |
| Formato: | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910707497503321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |