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Testing of turbulent seals for rotordynamic coefficientsA facility has been developed for dynamic testing of straight and convergent tapered seals with the capability of measuring the radial and tangential force components which result from a circular centered orbit. The test apparatus causes the seal journal to execute small-eccentricity centered circular orbits within its clearance circle. Dynamic measurements are made and recorded of the seal displacement-vector components, and of the pressure field. The pressure field is integrated to yield seal tangential and radial reaction-force components. Representative test data are provided and discussed for straight seals.
Document ID
19830007369
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Childs, D. W.
(Texas A&M Univ. College Station, TX, United States)
Dressman, J. B.
(Louisville Univ. Ky., United States)
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Rotordyn. Instability Probl. in High-Performance Turbomachinery
Subject Category
Mechanical Engineering
Accession Number
83N15640
Funding Number(s)
CONTRACT_GRANT: NSG-3200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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