1.

Record Nr.

UNINA9910707497503321

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

Pubbl/distr/stampa

Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996

Descrizione fisica

1 online resource (9 pages) : illustrations

Collana

NASA technical memorandum ; ; 107392

Soggetti

Boundary layer control

Pressure measurement

Flow visualization

Turbulent boundary layer

Mass flow rate

Static pressure

Shock waves

Lingua di pubblicazione

Inglese

Formato

Materiale a stampa

Livello bibliografico

Monografia

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).