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Traction contact performance evaluation at high speedsThe results of traction tests performed on two fluids are presented. These tests covered a pressure range of 1.0 to 2.5 GPa, an inlet temperature range of 30 'C to 70 'C, a speed range of 10 to 80 m/sec, aspect ratios of .5 to 5 and spin from 0 to 2.1 percent. The test results are presented in the form of two dimensionless parameters, the initial traction slope and the maximum traction peak. With the use of a suitable rheological fluid model the actual traction curves measured can now be reconstituted from the two fluid parameters. More importantly, the knowledge of these parameters together with the fluid rheological model, allow the prediction of traction under conditions of spin, slip and any combination thereof. Comparison between theoretically predicted traction under these conditions and those measured in actual traction tests shows that this method gives good results.
Document ID
19820008535
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tevaarwerk, J. L.
(Applied Tribology Ltd.)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-165226
DOE/NASA/0035-1
Report Number: NASA-CR-165226
Report Number: DOE/NASA/0035-1
Accession Number
82N16409
Funding Number(s)
CONTRACT_GRANT: DEN3-35
CONTRACT_GRANT: EC-77-A-31-1011
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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