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Publish Date
1990
Publisher
National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
For sale by the National Technical Information Service]
Language
English
Pages
56
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1
The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
1990, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Microform
in English
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Book Details
Edition 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.
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- Created September 22, 2008
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August 9, 2012 | Edited by VacuumBot | Updated format '[microform] /' to 'Microform'; cleaned up pagination; Removed author from Edition (author found in Work) |
December 15, 2009 | Edited by WorkBot | link works |
September 22, 2008 | Created by ImportBot | Imported from Oregon Libraries MARC record |