Effects of Internal-Area Distribution, Spike Translation, and Throat Boundary-Layer Control on Performance of a Double-Cone Axisymmetric Inlet at Mach Numbers From 3.0 to 2.0

Author:	Connors, James F.
Additional Authors:	Lovell, J. Calvin
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E57F03
Link:	https://digital.library.unt.edu/ark:/67531/metadc63620/