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Author

Bousman, William G.

Title The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover [electronic resource] / William G. Bousman.

Imprint

Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.

Connect to
Connect to http://purl.access.gpo.gov/GPO/LPS65436

Copies

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.60:3002	---	Available

Description	vii, 56 p. : ill. ; 28 cm.
Series	NASA technical paper ; 3002
	AVSCOM technical report ; 89-A-002
Note	Prepared at Ames Research Center and the Aeroflightdynamics Directorate, U.S. Army Aviation Research and Technology Activity.
Bibliography	Includes bibliographical references : (p. 56).
Form	Mode of access via the NTRS web site.
Subject	Rotors (Helicopters) -- Stability.
	Rotors (Helicopters) -- Aerodynamics.
	Aeroelasticity.
	Coupling.
	Hovering.
	Hovering stability.
	Mathematical models.
	Rigid rotors.
	Rotary wings.
Added Author	Ames Research Center.
	United States. Army Aviation Research and Technology Activity.
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.60:3002