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A parametric study of blade-motion stability boundaries for an articulated rotorNumerical solution of coupled, nonlinear, equation of motion for rigid blade to simulate response sensitivity and blade-motion stability of fully articulated rotor
Document ID
19690007957
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Jenkins, J. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5032
Accession Number
69N17289
Funding Number(s)
CONTRACT_GRANT: 721-01-00-29-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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