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Methods of Predicting Helicopter StabilitySome of the methods of predicting rotor stability derivatives have been reviewed. The methods by which these rotor derivatives are employed to estimate helicopter stability characteristics have been summarized. It is concluded that, although these methods are not always feasible for predicting absolute values of the stability of the helicopter, the effects on stability of changes in individual derivatives can generally be estimated satisfactorily.
Document ID
19930090308
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Robert J Tapscott
(Langley Aeronautical Laboratory Langley Field, Virginia, United States)
F B Gustafson
(Langley Aeronautical Laboratory Langley Field, Virginia, United States)
Date Acquired
August 15, 2013
Publication Date
November 2, 1954
Publication Information
Publisher: National Advisory Committee for Aeronautics
Subject Category
Aircraft Stability And Control
Report/Patent Number
NACA-RM-L54G05
Accession Number
93R19598
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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