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Analytical study to define a helicoper stability derivative extraction method, volume 2The data generated during tests to determine helicopter stability derivatives are presented in the form of graphs. The data are based on CH-53A helicopters and CH-54B helicopters with various digital filters operating at various airspeeds. Curves are plotted for a time history comparison of identified derivative models against flight data for the helicopters at specific airspeeds and maneuvers.
Document ID
19740010562
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Molusis, J. A. (United Aircraft Corp. Stratford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-CR-132372
Report Number: NASA-CR-132372
Accession Number
74N18675
Funding Number(s)
CONTRACT_GRANT: NAS1-11613
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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