A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver

Author:	Sternfield, Leonard.
Year:	1956
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L56F04
Series:	NACA research memorandum ;
Report Number:	L56F04
Subjects:	Charts, diagrams, etc
	Mathematics
	Airplanes--Control
	Rolling (Aerodynamics)
Link:	https://hdl.handle.net/2027/mdp.39015086466037