Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3

Author:	Henning, Allen B.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L57D29
Series:	NACA research memorandum ;
Report Number:	L57D29
Subjects:	Charts, diagrams, etc
	Stability
	Lift (Aerodynamics)
	Mach number
	Drag (Aerodynamics)
	Aerofoils--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086507228