Investigation at Mach numbers 1.5 and 1.7 of twin-duct side intake system with two-dimensional 6 degree compression ramps mounted on a supersonic airplane

Author:	Davids, Joseph
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E53H19
Link:	https://digital.library.unt.edu/ark:/67531/metadc59677/