Wind-tunnel investigation of effects of ventral fins at two positions on lateral-stability derivatives of 45©� high-wing model oscillating in yaw

Author:	Jaquet, Byron M.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L56J31a
Series:	NACA research memorandum ;
Report Number:	L56J31a
Subjects:	Charts, diagrams, etc
	Oscillations
	Wind tunnel testing
	Airplanes--Tail surfaces
	Airplanes--Models--Testing
	Stability of airplanes, Lateral
	Yawing (Aerodynamics)
Link:	https://hdl.handle.net/2027/mdp.39015086507160