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:
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

MARC

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500 |a "December 1996"--Report documentation page. 
500 |a "Prepared for the 35th Aerospace Sciences Meeting and Exhibit cosponsored by AIAA, ASME, SAE, and ASME, Reno, Nevada, January 6-10, 1997." 
500 |a "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page. 
504 |a Includes bibliographical references (page 9). 
513 |a Technical memorandum. 
536 |a Sponsored by the National Aeronautics and Space Administration  |d WU-505-62-52  |d E-10592 
500 |a "AIAA-97-0608." 
650 7 |a Boundary layer control.  |2 nasat 
650 7 |a Pressure measurement.  |2 nasat 
650 7 |a Flow visualization.  |2 nasat 
650 7 |a Turbulent boundary layer.  |2 nasat 
650 7 |a Mass flow rate.  |2 nasat 
650 7 |a Static pressure.  |2 nasat 
650 7 |a Shock waves.  |2 nasat 
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