Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord

Author:	Bertram, Mitchel H.
Additional Authors:	McCauley, William D.
Year:	1954
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L54G28
Series:	NACA research memorandum ;
Report Number:	L54G28
Subjects:	Charts, diagrams, etc
	Mach number
	Airplanes--Wings, Triangular
	Aerodynamics, Supersonic
	Wedges--Aerodynamics
Link:	https://hdl.handle.net/2027/mdp.39015086465658