An investigation of three transonic fuselage air inlets at Mach numbers from 0.4 to 0.94 and at a Mach number of 1.19

Author:	Pendley, Robert E.
Additional Authors:	Robinson, Harold L.
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50H24
Link:	https://digital.library.unt.edu/ark:/67531/metadc58616/