An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds

Author:	Howell, Robert R.
Additional Authors:	Braslow, Albert L.
Year:	1955
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L54L31A
Series:	NACA research memorandum ;
Report Number:	L54L31A
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Drag (Aerodynamics)
	Airplanes--Fuselage
	Airplanes--Wings, Swept-back
	Aerodynamics, Transonic
	Airplanes--Wings--Design and construction
Link:	https://hdl.handle.net/2027/mdp.39015086465757