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Effect of shaft rotation on the incompressible flow in a labyrinth sealThe incompressible flow in a labyrinth seal at low leakage rates was computationally and experimentally investigated over a wide range of seal rotation rates. QUICK differencing was employed in the finite difference code to reduce the effects of false diffusion. The use of measured inlet boundary conditions for the axial and swirl velocity components and for the turbulent kinetic energy resulted in good agreement between velocity predictions and hot-film measurements. It was found that when the rotation rate is increased beyond a certain point, a second recirculation zone forms inside the seal cavity, altering the flow field in the cavity and resulting in a substantial increase in the pressure drop across it.
Document ID
19880043255
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Demko, J. A.
(General Dynamics Corp. Fort Worth, TX, United States)
Morrison, G. L.
(General Dynamics Corp. Fort Worth, TX, United States)
Rhode, D. L.
(Texas A & M University College Station, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Numerical methods in laminar and turbulent flow
Location: Montreal
Country: Canada
Start Date: July 6, 1987
End Date: July 10, 1987
Accession Number
88A30482
Distribution Limits
Public
Copyright
Other

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