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Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections

Author:	Runckel, Jack F.
Additional Authors:	Lee, Edwin E..
Year:	1956
Document Type:	MAIN
SUDOC:	Y 3.N 21/5:15/L56F12
Series:	NACA research memorandum ;
Report Number:	L56F12
Subjects:	Charts, diagrams, etc
	Aerodynamic load
	Wind tunnel testing
	Airplanes--Wings, Swept-back
	Aerodynamics, Transonic
Link:	https://hdl.handle.net/2027/mdp.39015095100999