タイトル | Nonlinear rotordynamics analysis |
本文(外部サイト) | http://hdl.handle.net/2060/19850014053 |
著者(英) | Day, W. B. |
著者所属(英) | Auburn Univ. |
発行日 | 1985-03-15 |
言語 | eng |
内容記述 | The special nonlinearities of the Jeffcott equations in rotordynamics are examined. The immediate application of this analysis is directed toward understanding the excessive vibrations recorded in the LOX pump of the SSME during hot firing ground testing. Deadband, side force and rubbing are three possible sources of inducing nonlinearity in the Jeffcott equations. The present analysis initially reduces these problems to the same mathematical description. A special frequency, named the nonlinear natural frequency is defined and used to develop the solutions of the nonlinear Jeffcott equations as asympotic expansions. This nonlinear natural frequency which is the ratio of the cross-stiffness and the damping, plays a major role in determining response frequencies. Numerical solutions are included for comparison with the analysis. Also, nonlinear frequency-response tables are made for a typical range of values. |
NASA分類 | AERODYNAMICS |
レポートNO | 85N22364 NASA-CR-171425 NAS 1.26:171425 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/156829 |
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