In this paper, the existing Modal Reduction Method, which was developed to handle symmetric mass and stiffness matrices, is extended utilizing state-space formulation to handle nonsymmetric mass, damping, and stiffness matrices. These type of matrices typically accompany rotor dynamic problems since journal bearings supporting the rotor have nonsymmetric stiffness and damping characteristics. The purpose of modal reduction is to eliminate unimportant modes and degrees of freedom from the analytical model after they are found, so that further numerical analysis can be accelerated. The reduction described here leaves the retained eigenvalues and mode shapes unaltered from their original values. This method is demonstrated for a simple rotor problem having nonsymmetric system matrices including gyroscopic effects.
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January 1991
Research Papers
The Extended Modal Reduction Method Applied to Rotor Dynamic Problems
K. Kane,
K. Kane
California State University, Long Beach, CA 90840
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B. J. Torby
B. J. Torby
California State University, Long Beach, CA 90840
Search for other works by this author on:
K. Kane
California State University, Long Beach, CA 90840
B. J. Torby
California State University, Long Beach, CA 90840
J. Vib. Acoust. Jan 1991, 113(1): 79-84 (6 pages)
Published Online: January 1, 1991
Article history
Received:
July 1, 1989
Online:
June 17, 2008
Citation
Kane, K., and Torby, B. J. (January 1, 1991). "The Extended Modal Reduction Method Applied to Rotor Dynamic Problems." ASME. J. Vib. Acoust. January 1991; 113(1): 79–84. https://doi.org/10.1115/1.2930159
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