Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction /

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Bibliographic Details
Author / Creator:	Kim, Hyun Dae, author.
Imprint:	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.
Description:	1 online resource (9 pages) : illustrations.
Language:	English
Series:	NASA technical memorandum ; 107392 NASA technical memorandum ; 107392.
Subject:	Boundary layer control. Flow visualization. Pressure -- Measurement. Shock waves. Turbulent boundary layer.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10914635

Hidden Bibliographic Details
Other authors / contributors:	Hingst, Warren R., author. Davis, David O., author. Lewis Research Center, issuing body.
Notes:	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." Includes bibliographical references (page 9). Technical memorandum. Sponsored by the National Aeronautics and Space Administration WU-505-62-52 E-10592
Other form:	Microfiche version: Kim, Hyun D. Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:107392

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