Flight Determination of Drag of Normal-Shock Nose Inlets With Various Cowling Profiles at Mach Numbers From 0.9 to 1.5

Author:	Sears, R. I.
Additional Authors:	Merlet, C. F.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53I25a
Link:	https://digital.library.unt.edu/ark:/67531/metadc59890/