Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components

Author:	Ellis, Macon C.
Additional Authors:	Grigsby, Carl E.
Year:	1950
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L9L28a
Series:	NACA research memorandum ;
Report Number:	L9L28a
Subjects:	Charts, diagrams, etc
	Lift (Aerodynamics)
	Wind tunnel testing
	Pitching (Aerodynamics)
	Drag (Aerodynamics)
	Airplanes--Tail surfaces
	Airplanes--Wings, Rectangular
Link:	https://hdl.handle.net/2027/mdp.39015086490565