NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of coulomb spline on rotor dynamic responseA rigid rotor system coupled by a coulomb spline is modelled and analyzed by approximate analytical and numerical analytical methods. Expressions are derived for the variables of the resulting limit cycle and are shown to be quite accurate for a small departure from isotropy.
Document ID
19860020705
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nataraj, C.
(Arizona State Univ. Tempe, AZ, United States)
Nelson, H. D.
(Arizona State Univ. Tempe, AZ, United States)
Arakere, N.
(Arizona State Univ. Tempe, AZ, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1985
Publication Information
Publication: NASA. Lewis Research Center Instability in Rotating Machinery
Subject Category
Mechanical Engineering
Accession Number
86N30177
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available