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Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction / Hyun D. Kim, Warren R. Hingst, and David O. Davis.

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Format:
Book
Government document
Author/Creator:
Kim, Hyun Dae, author.
Hingst, Warren R., author.
Davis, David O., author.
Contributor:
Lewis Research Center, issuing body.
Series:
NASA technical memorandum ; 107392.
NASA technical memorandum ; 107392
Language:
English
Subjects (All):
Boundary layer control.
Pressure--Measurement.
Pressure.
Flow visualization.
Turbulent boundary layer.
Shock waves.
Genre:
Online resources.
Physical Description:
1 online resource (9 pages) : illustrations
Place of Publication:
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.
Notes:
Title from title screen (viewed August 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
Includes bibliographical references (page 9).
"AIAA-97-0608."
Other Format:
Microfiche version: Kim, Hyun D. Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction
OCLC:
956368950

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