Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4

Author:	Knechtel, Earl D.
Additional Authors:	Lee, George.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/A57F06b
Series:	NACA research memorandum ;
Report Number:	A57F06b
Subjects:	Charts, diagrams, etc
	Flaps (Airplanes)
	Leading edges (Aerodynamics)
	Airplanes--Wings, Swept-back
	Airplanes--Models--Testing
	Stability of airplanes, Longitudinal
	Airplanes--Models--Wings
Link:	https://hdl.handle.net/2027/mdp.39015086429803