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.
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

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