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The effects on nonuniform swash plate stiffness on coupled blade control system dynamics and stability. Part 1 - Analysis and applicationMathematical models for calculating flexible swash-plate effects on vibratory and mechanical stability characteristics of helicopter rotor systems
Document ID
19710023917
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Piarulli, V. J. (Rochester Applied Science Associates Inc., NY, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1971
Publication Information
Publisher: NASA
Subject Category
Aircraft
Report/Patent Number
REPT-70-70
NASA-CR-1817
Report Number: REPT-70-70
Report Number: NASA-CR-1817
Accession Number
71N33393
Funding Number(s)
CONTRACT_GRANT: NAS1-9496
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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