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SSME interstage seal researchTest results comprising direct and transverse force coefficients and leakage coefficients are reported for six seal configurations. All seals tested use the same smooth rotor and have the same constant minimum clearance. The following stator configurations were tested: (1) Smooth, (2) knurled pattern, (3) axially-grooved pattern with end seals, (4) diamond-grid roughened, (5) diamond-grid roughened with end seals, and (6) round-hole pattern. Comparison of the seals shows the Knurled-pattern stator to be the stiffest and the round-hole pattern stator to yield the largest net damping and the least leakage. The theory of reference is shown to substantially underestimate the stiffness and effective-added-mass coefficients, but do a reasonable job in predicting the net-damping-force coefficient.
Document ID
19840012563
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Childs, D. W.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-170995
RD-1-84
NAS 1.26:170995
Report Number: NASA-CR-170995
Report Number: RD-1-84
Report Number: NAS 1.26:170995
Accession Number
84N20631
Funding Number(s)
CONTRACT_GRANT: NAS8-33716
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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