Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane 2: Inlets Utilizing Half of a Conical Spike

Author:	Allen, J. L.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E52G08
Link:	https://digital.library.unt.edu/ark:/67531/metadc59397/