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