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Entrance and exit region friction factor models for annular seal analysisThe Mach number definition and boundary conditions in Nelson's nominally-centered, annular gas seal analysis are revised. A method is described for determining the wall shear stress characteristics of an annular gas seal experimentally. Two friction factor models are developed for annular seal analysis; one model is based on flat-plate flow theory; the other uses empirical entrance and exit region friction factors. The friction factor predictions of the models are compared to experimental results. Each friction model is used in an annular gas seal analysis. The seal characteristics predicted by the two seal analyses are compared to experimental results and to the predictions of Nelson's analysis. The comparisons are for smooth-rotor seals with smooth and honeycomb stators. The comparisons show that the analysis which uses empirical entrance and exit region shear stress models predicts the static and stability characteristics of annular gas seals better than the other analyses. The analyses predict direct stiffness poorly.
Document ID
19880016537
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Elrod, David Alan
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:183084
NASA-CR-183084
TL-SEAL-5-88
Report Number: NAS 1.26:183084
Report Number: NASA-CR-183084
Report Number: TL-SEAL-5-88
Accession Number
88N25921
Funding Number(s)
CONTRACT_GRANT: NAG3-181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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