Aerodynamic performance of several techniques for spike-position control of a blunt-lip nose inlet having internal contraction; Mach numbers of 0.63 and 1.5 to 2.0

Author:	Anderson, Arthur A
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E57D15
Link:	https://digital.library.unt.edu/ark:/67531/metadc63487/