NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Theory versus experiment for the rotordynamic coefficients of labyrinth gas seals. II - A comparison to experimentAn experimental test facility is used to measure the leakage and rotordynamic coefficients of teeth-on-rotor and teeth-on-stator labyrinth gas seals. The test results are presented along with the theoretically predicted values for the two seal configurations at three different radial clearances and shaft speeds to 16,000 cpm. The test results show that the theory accurately predicts the cross-coupled stiffness for both seal configurations and shows improvement in the prediction of the direct damping for the teeth-on-rotor seal. The theory fails to predict a decrease in the direct damping coefficient for an increase in the radial clearance for the teeth-on-stator seal.
Document ID
19880044309
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Childs, D. W.
(Texas A&M Univ. College Station, TX, United States)
Scharrer, J. K.
(Texas A & M University College Station, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Mechanical Engineering
Accession Number
88A31536
Funding Number(s)
CONTRACT_GRANT: F49620-82-K-0033
CONTRACT_GRANT: NAS3-181
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available