Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section.Transonic-bump method

Author:	Sleeman, William C.
Additional Authors:	Becht, Robert E.
Year:	1949
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L9G22A
Series:	NACA research memorandum ;
Report Number:	L9G22A
Subjects:	Charts, diagrams, etc
	Lift (Aerodynamics)
	Wind tunnel testing
	Pitching (Aerodynamics)
	Drag (Aerodynamics)
	Airplanes--Wings, Swept-back
	Airplanes--Wings, Triangular
	Aerofoils--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086464503