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Linear stability of compressible Taylor-Couette flowA temporal stability analysis of compressible Taylor-Couette flow is presented. The viscous flow studied in this paper is contained between two concentric cylinders of infinite length, which are rotating with different angular velocities and are kept at different surface temperatures. The effects of differential rotation and temperature difference on the stability of Taylor-Couette flow are contrasted for a range of Mach numbers ranging from incompressible to Mach 3.0. The relative motion of the cylinders dramatically affects the characteristics of the Couette flow at the onset of instability. The flow is stabilized or destabilized depending upon the temperature ratio and speeds of the two cylinders. Independent of Mach number and temperature ratio, increasing Reynolds number generally promotes a destabilizing effect, indicating the inviscid nature of the Taylor-Couette flow.
Document ID
19920053563
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Kao, Kai-Hsiung
(NASA Lewis Research Center Cleveland, OH, United States)
Chow, Chuen-Yen
(Colorado, University Boulder, United States)
Date Acquired
August 15, 2013
Publication Date
May 1, 1992
Publication Information
Publication: Physics of Fluids A
Volume: 4
Issue: 5 Ma
ISSN: 0899-8213
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92A36187
Funding Number(s)
CONTRACT_GRANT: NCC3-168
Distribution Limits
Public
Copyright
Other

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