Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60° delta-wing airplane model, by Lewis R. Fisher et al.

Title:	Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60° delta-wing airplane model
Author:	Fisher, Lewis R.
Author:	United States. National Adviosry Committee for Aeronautics
Author:	Langley Aeronautical Laboratory
Note:	National Advisory Committee for Aeronautics, 1958

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Subject:	Airplanes -- Wings, Triangular
Subject:	Angle of attack (Aerodynamics)
Subject:	Flutter
Subject:	Flutter (Aerodynamics)
Subject:	Oscillating wings (Aerodynamics)
Subject:	Rolling (Aerodynamics)
Subject:	Stability of airplanes, Lateral
Subject:	Vibration (Aeronautics)
Subject:	Vibration (Aeronautics) -- Damping
Subject:	Yawing (Aerodynamics)
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