Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule

Author:	Palmer, William E.
Additional Authors:	Braslow, Albert L., Howell, Robert R.
Year:	1956
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L56D11a
Series:	NACA research memorandum ;
Report Number:	L56D11a
Subjects:	Airplanes--Fuselage
	Airplanes--Wings, Swept-back
	Aerodynamics, Transonic
Link:	https://hdl.handle.net/2027/mdp.39015086507111