Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88

Author:	Kelly, John A.
Additional Authors:	Hayter, Nora-Lee F.
Year:	1951
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/A51H23
Series:	NACA research memorandum ;
Report Number:	A51H23
Subjects:	Charts, diagrams, etc
	Lift (Aerodynamics)
	Aerodynamic load
	Wind tunnel testing
	Pitching (Aerodynamics)
	Drag (Aerodynamics)
	Airplanes--Wings, Swept-back
	Airplanes--Models--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086489971