Lift-curve slopes determined in flight on a flexible swept-wing jet bomber

Author:	Aiken, William S.,
Additional Authors:	Fisher, Raymond A.
Year:	1956
Document Type:	MAIN
SUDOC:	Y 3.N 21/5:15/L56E21a
Series:	NACA research memorandum ;
Report Number:	L56E21a
Subjects:	Charts, diagrams, etc
	Lift (Aerodynamics)
	Aerodynamic load
	Airplanes--Flight testing
	Airplanes--Wings, Swept-back
	Angle of attack (Aerodynamics)
	Airplanes, Military--Bombers
	Acceleration (Mechanics)--Measurement
Link:	https://hdl.handle.net/2027/mdp.39015095100981