02220nam 2200565I 450 991070749750332120160809102728.0(CKB)5470000002464549(OCoLC)956368950(EXLCZ)99547000000246454920160809j199612 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierExperimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction /Hyun D. Kim, Warren R. Hingst, and David O. DavisCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,December 1996.1 online resource (9 pages) illustrationsNASA technical memorandum ;107392Title 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."Includes bibliographical references (page 9).Boundary layer controlnasatPressure measurementnasatFlow visualizationnasatTurbulent boundary layernasatMass flow ratenasatStatic pressurenasatShock wavesnasatBoundary layer control.Pressure measurement.Flow visualization.Turbulent boundary layer.Mass flow rate.Static pressure.Shock waves.Kim Hyun Dae1390070Hingst Warren R.Davis David O.Lewis Research Center,GPOGPOBOOK9910707497503321Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction3442386UNINA