The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover /

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Bibliographic Details
Author / Creator:Bousman, William G. (William Giles)
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.
Description:vii, 56 pages : illustrations ; 28 cm.
Language:English
Series:NASA technical paper ; 3002
AVSCOM technical report ; 89-A-002
NASA technical paper ; 3002.
AVSCOM technical report ; 89-A-002.
Subject:Rotors (Helicopters) -- Stability.
Rotors (Helicopters) -- Aerodynamics.
Aeroelasticity.
Coupling.
Hovering.
Hovering stability.
Mathematical models.
Rigid rotors.
Rotary wings.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6508784
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Other authors / contributors:Ames Research Center.
United States. Army Aviation Research and Technology Activity.
Notes:Prepared at Ames Research Center and the Aeroflightdynamics Directorate, U.S. Army Aviation Research and Technology Activity.
Includes bibliographical references : (page 56).
Available via Internet from the NASA Technical Report Server web site. Address as of 12/2/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900019187%5F1990019187.pdf ; current access is available via PURL.
GPO item no.:0830-H-15 (MF)
0830-H-15 (online)
Govt.docs classification:NAS 1.60:3002