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Measurements of Pressure Distributions and Force Coefficients in a Squeeze Film Damper. Part 2: Partially Sealed ConfigurationExperimental results from a partially sealed squeeze film damper (SFD) test rig, executing a circular centered orbit are presented and discussed. A serrated piston ring is installed at the damper exit. This device involves a new sealing concept which produces high damping values while allowing for oil flow to cool the damper. In the partially sealed damper, large cavitation regions are observed in the pressure fields at orbit radii epsilon equals 0.5 and epsilon equals 0.8. The cavitated pressure distributions and the corresponding force coefficients are compared with a cavitated bearing solution. The experimental results show the significance of fluid inertia and vapor cavitation in the operation of squeeze film dampers. Squeeze film Reynolds numbers tested reach up to Re equals 50, spanning the range of contemporary applications.
Document ID
19920005135
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jung, S. Y.
(Texas A&M Univ. College Station, TX, United States)
Sanandres, Luis A.
(Texas A&M Univ. College Station, TX, United States)
Vance, J. M.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Publication Information
Publication: NASA. Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1990
Subject Category
Mechanical Engineering
Accession Number
92N14353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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