A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel

Author:	Hasel, Lowell E.
Additional Authors:	Sinclair, Archibald R.
Year:	1950
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L50B14a
Series:	NACA research memorandum
Report Number:	L50B14a
Subjects:	Supersonic planes
	Airplanes--Fuselage
	Aerodynamics, Supersonic
Link:	https://hdl.handle.net/2027/mdp.39015086429902