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Seals For Cryogenic TurbomachinesAnalysis considers effects of seals on stability. Report presents method of calculation of flows of cryogenic fluids through shaft seals. Key to stability is local average velocity in seal. Local average velocity strongly influenced by effects of inlet and outlet and injection of fluid.
Document ID
19880000440
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Hendricks, Robert C. (NASA Lewis Research Center, Cleveland, Ohio.)
Tam, L. T. (CHAM)
Braun, M. J. (University of Akron)
Vlcek, B. L. (Rensselaer Polytechnic Institute)
Date Acquired
August 13, 2013
Publication Date
September 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 8
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14556
Accession Number
88B10440
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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