Pressure Recovery at Supersonic Speeds Through Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer 2: Effect of an Oblique Shock Wave Immediately Ahead of the Inlet

Author:	Brajnikoff, George B.
Year:	1948
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A8F08
Link:	https://digital.library.unt.edu/ark:/67531/metadc57700/