Theoretical and Experimental Analysis of Low-Drag Supersonic Inlets Having a Circular Cross Section and a Central Body at Mach Numbers 3.30, 2.75, and 2.45

Author:	Ferri, Antonio
Year:	1948
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1189
Link:	https://digital.library.unt.edu/ark:/67531/metadc65573/