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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.

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

 
    
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