Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles

Author:	Love, Eugene S.
Year:	1949
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L9D07
Series:	NACA research memorandum ;
Report Number:	L9D07
Subjects:	Charts, diagrams, etc
	Leading edges (Aerodynamics)
	Airplanes--Wings, Triangular
	Airplanes--Models--Testing
	Airplanes--Models--Wings
	Aerodynamics, Supersonic
Link:	https://hdl.handle.net/2027/mdp.39015086464453