Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8

Author:	Sears, R. I.
Year:	1951
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L50L18
Series:	NACA research memorandum ;
Report Number:	L50L18
Subjects:	Charts, diagrams, etc
	Pressure
	Drag (Aerodynamics)
	Jet engines--Air intakes
	Noses (Aircraft)
Link:	https://hdl.handle.net/2027/mdp.39015086464743