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A Comparison of Experimental and Theoretical Results for Labyrinth Gas SealsThe basic equations are derived for a two control volume model for compressible flow in a labyrinth seal. The flow is assumed to be completely turbulent and isoenergetic. The wall friction factors are determined using the Blasius formula. Jet flow theory is used for the calculation of the recirculation velocity in the cavity. Linearized zeroth and first order perturbation equations are developed for small motion about a centered position by an expansion in the eccentricity ratio. The zeroth order pressure distribution is found by satisfying the leakage equation. The circumferential velocity distribution is determined by satisfying the momentum equations. The first order equations are solved by a separation of variable solution. Integration of the resultant pressure distribution along and around the seal defines the reaction force developed by the seal and the corresponding dynamic coefficients. The results of this analysis are compared to experimental test results.
Document ID
19870008663
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Scharrer, Joseph Kirk
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Subject Category
Mechanical Engineering
Report/Patent Number
TRC-SEAL-3-87
NAS 1.26:180194
NASA-CR-180194
Accession Number
87N18096
Funding Number(s)
CONTRACT_GRANT: NAG3-181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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