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

Bibliographic Details
Main Authors: Kim, Hyun Dae (Author), Hingst, Warren R. (Author), Davis, David O. (Author)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.
Series:NASA technical memorandum ; 107392.
Subjects:
Boundary layer control.
Pressure measurement.
Flow visualization.
Turbulent boundary layer.
Mass flow rate.
Static pressure.
Shock waves.
Online Access:https://purl.fdlp.gov/GPO/gpo70927
Description
Item Description: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."
Physical Description:1 online resource (9 pages) : illustrations.
Bibliography:Includes bibliographical references (page 9).