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Enhanced rotor modeling tailored for rub dynamic stability analysis and simulationNew methods are presented that allow straightforward application of complex nonlinearities to finite element based rotor dynamic analyses. The key features are: (1) the methods can be implemented with existing finite element or dynamic simulation programs, (2) formulation is general for simple application to a wide range of problems, and (3) implementation is simplified because nonlinear aspects are separated from the linear part of the model. The new techniques are illustrated with examples of inertial nonlinearity and torquewhirl which can be important in rubbing turbomachinery. The sample analyses provide new understanding of these nonlinearities which are discussed.
Document ID
19890013545
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davis, R. R.
(Aerojet TechSystems Co. Sacramento, CA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Publication Information
Publication: NASA, Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1988
Subject Category
Mechanical Engineering
Accession Number
89N22916
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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