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On the linear stability of compressible plane Couette flowThe linear stability of compressible plane Couette flow is investigated. The correct and proper basic velocity and temperature distributions are perturbed by a small amplitude normal mode disturbance. The full small amplitude disturbance equations are solved numerically at finite Reynolds numbers, and the inviscid limit of these equations is then investigated in some detail. It is found that instability can occur, although the stability characteristics of the flow are quite different from unbounded flows. The effects of viscosity are also calculated, asymptotically, and shown to have a stabilizing role in all the cases investigated. Exceptional regimes to the problem occur when the wavespeed of the disturbances approaches the velocity of either of the walls, and these regimes are also analyzed in some detail. Finally, the effect of imposing radiation-type boundary conditions on the upper (moving) wall (in place of impermeability) is investigated, and shown to yield results common to both bounded and unbounded flows.
Document ID
19910020783
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Duck, Peter W.
(Manchester Univ. Hampton, VA, United States)
Erlebacher, Gordon
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Hussaini, M. Yousuff
(Institute for Computer Applications in Science and Engineering)
Date Acquired
September 6, 2013
Publication Date
July 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-187610
NAS 1.26:187610
ICASE-91-64
AD-A240688
Report Number: NASA-CR-187610
Report Number: NAS 1.26:187610
Report Number: ICASE-91-64
Report Number: AD-A240688
Accession Number
91N30097
Funding Number(s)
CONTRACT_GRANT: NAS1-18605
PROJECT: RTOP 505-90-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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