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Dynamic inflow for practical applicationsA derivation is presented which gives both the nonlinear dynamic inflow model and the perturbation dynamic inflow model in a general coordinate system. The perturbation model includes perturbations in hub motions, in skew angle, and in yaw angle. The governing equations may be switched to their dimensional forms prior to application.
Document ID
19890032254
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Peters, David A.
(Georgia Institute of Technology Atlanta, United States)
Haquang, Ninh
(Boeing Helicopters Philadelphia, PA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1988
Publication Information
Publication: American Helicopter Society, Journal
Volume: 33
ISSN: 0002-8711
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0002-8711
Accession Number
89A19625
Funding Number(s)
CONTRACT_GRANT: NAS2-12341
Distribution Limits
Public
Copyright
Other

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