NASA NTRS · 19800000259
Rotor transient analysis
Abstract
Undamped modes approximate dynamic behavior of rotors and bearings. Application of modal analysis to uncouple equations of motion simplifies stability, steady-state unbalance response, and transient response analysis of system; nonlinear stability is predicted from calculated frequency spectra. Analysis provides designers with complete information without involving large-scale computational costs. Programs are written in FORTRAN IV for use on CDC 6600 computer.
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Allaire, P. E., Choy, K. C., Gunter, E. J.. 1980-09-01. Rotor transient analysis. https://ntrs.nasa.gov/citations/19800000259
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