NASA NTRS ยท 19940000352
Limit-Cycle Vibrations In Turbomachinery
Abstract
Paper presents theoretical study of vibrations in high-speed turbomachinery. Addresses relationship between two classes of vibrational phenomena previously studied separately: dynamic instabilities, including both those subject to linear analysis and limit-cycle instabilities in cases of nonlinear vibrational response, and subharmonic response to excitation caused by unbalance of rotor.
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Ryan, S. G.. 1994-06-01. Limit-Cycle Vibrations In Turbomachinery. https://ntrs.nasa.gov/citations/19940000352
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