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Identification of a coupled flapping/inflow model for the PUMA helicopter from flight test dataA model validation procedure is applied to a coupled flapping/inflow model of a PUMA helicopter blade. The structure of the baseline model is first established. Model structure and flight test data are checked for consistency. Parameters of the model are then identified from the flight test data.
Document ID
19900025712
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Du Val, Ronald
(Advanced Rotorcraft Technology, Inc. Mountain View, CA, United States)
Bruhis, Ofer
(Advanced Rotorcraft Technology, Inc. Mountain View, CA, United States)
Green, John
(Advanced Rotorcraft Technology, Inc. Mountain View, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Publication Information
Publication: Vertica
Volume: 13
Issue: 3, 19
ISSN: 0360-5450
Subject Category
Aircraft Stability And Control
Accession Number
90A12767
Distribution Limits
Public
Copyright
Other

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