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Linear stability of the confined compressible reacting mixing layerThis paper investigates the linear stability of confined mixing layers with special emphasis on the effects of heat release and compressibility. The results show that reflection of supersonic disturbances by the walls makes the confined supersonic mixing layer more unstable than the unconfined free shear layer. Decreasing the distance between the walls makes the flow more unstable. However, subsonic disturbances are relatively unaffected by the walls. Heat release and Mach number hardly change the growth rates of supersonic disturbances. The most unstable supersonic disturbances are two-dimensional in rectangular channel flows, but three-dimensional in partially confined flows. Finally, the reactants are not strongly mixed by supersonic instabilities, which mainly disturb one side of the layer.
Document ID
19930045325
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Shin, D. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Ferziger, J. H.
(Stanford Univ. CA, United States)
Date Acquired
August 16, 2013
Publication Date
March 1, 1993
Publication Information
Publication: AIAA Journal
Volume: 31
Issue: 3
ISSN: 0001-1452
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
93A29322
Distribution Limits
Public
Copyright
Other

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