The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
By: William G. Bousman.
Contributors: Ames Research Center.; United States. Army Aviation Research and Technology Activity.
Series: NASA technical paper -- 3002.; AVSCOM technical report -- 89-A-002.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1990
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 56
Subjects: Rotors (Helicopters) -- Stability.; Rotors (Helicopters) -- Aerodynamics.; Aeroelasticity.; Coupling.; Hovering.; Hovering stability.; Mathematical models.; Rigid rotors.; Rotary wings.
Notes: Prepared at Ames Research Center and the Aeroflightdynamics Directorate, U.S. Army Aviation Research and Technology Activity.

Includes bibliographical references : (p. 56).

Also 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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche.