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Quasi-one-dimensional compressible flow across face seals and narrow slots. 1: AnalysisAn analysis is presented for compressible fluid flow across shaft face seals and narrow slots. The analysis includes fluid inertia, viscous friction, and entrance losses. Subsonic and choked flow conditions can be predicted and analyzed. The model is valid for both laminar and turbulent flows. Results agree with experiment and with solutions which are more limited in applicability. Results show that a parallel film can have a positive film stiffness under choked flow conditions.
Document ID
19720017818
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Zuk, J.
(NASA Lewis Research Center Cleveland, OH, United States)
Ludwig, L. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Johnson, R. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Machine Elements And Processes
Report/Patent Number
E-6819
NASA-TN-D-6668
Accession Number
72N25468
Funding Number(s)
PROJECT: RTOP 132-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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