NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flow induced force of labyrinth sealFlow induced instability force due to a labyrinth seal is analyzed. An approximate solution is given for the partial differential equation representing the flow in labyrinth seal and it is compared with the finite difference method in order to verify the accuracy of both methods. The effects of difference of inlet and outlet pressures of the seal, deflection of pressure and mass flow from the steady state, rotor diameter, seal clearance, seal interval and seal number on the flow induced force of the seal are investigated and it is known that some of these factors are very influential on the flow induced force.
Document ID
19830007372
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Iwatsubo, T.
(Kobe Univ.)
Motooka, N.
(Kobe Univ.)
Kawai, R.
(Kobe Univ.)
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Rotordyn. Instability Probl. in High-Performance Tubomachinery
Subject Category
Mechanical Engineering
Accession Number
83N15643
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available