Welcome to the Kids' Library!

Search for books, movies, music, magazines, and more.

Back to Search Results

Available items only

Record 34 of 122

Previous Record Next Record

ElectronicResource GovDoc

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