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A numerical method for studing the transient blade motions of a rotor with flapping and lead-lag degrees of freedomNumerical method for determining transient blade motions of rotor with flapping and lead-lag degrees of freedom
Document ID
19670028687
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Jenkins, J. L., Jr. (NASA Space Task Group Langley Station, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4195
Report Number: NASA-TN-D-4195
Accession Number
67N38016
Funding Number(s)
CONTRACT_GRANT: 721-01-00-29-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRANSIENT RESPONSE
ROTOR BLADE
DYNAMIC STABILITY
MOTION EQUATION
NUMERICAL ANALYSIS
HELICOPTER ROTOR

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