Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section.Transonic-bump method

Author:	Myers, Boyd C.
Additional Authors:	King, Thomas J.
Year:	1949
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L9E25
Series:	NACA research memorandum ;
Report Number:	L9E25
Subjects:	Charts, diagrams, etc
	Lift (Aerodynamics)
	Pitching (Aerodynamics)
	Drag (Aerodynamics)
	Airplane--Wings, Swept-back
Link:	https://hdl.handle.net/2027/mdp.39015086490524