Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds

Author:	Mugler, John P.
Year:	1956
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L56G12a
Series:	NACA research memorandum ;
Report Number:	L56G12a
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Drag (Aerodynamics)
	Leading edges (Aerodynamics)
	Airplanes--Wings, Triangular
	Airplanes--Models--Testing
	Aerodynamics, Transonic
Link:	https://hdl.handle.net/2027/mdp.39015086507145