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A general approach for the prediction of localized instability generation in boundary layer flowsThe present approach to the prediction of instability generation that is due to the interaction of freestream disturbances with regions of subscale variations in surface boundary conditions can account for the finite Reynolds number effects, while furnishing a framework for the study of receptivity in compressible flow and in 3D boundary layers. The approach is illustrated for the case of Tollmien-Schlichting wave generation in a Blasius boundary layer, due to the interaction of a freestream acoustic wave with a localized wall inhomogeneity. Results are presented for the generation of viscous and inviscid instabilities in adverse pressure-gradient boundary layers, supersonic boundary layer instabilities, and cross-flow vortex instabilities.
Document ID
19930033279
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Choudhari, Meelan
(High Technology Corp. Hampton, VA, United States)
Ng, Lian
(Analytical Services and Materials Hampton, VA, United States)
Streett, Craig L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Boundary layer transition and control; Proceedings of the Conference, Univ. of Cambridge, United Kingdom, Apr. 8-12, 1991 (A93-17251 04-34)
Publisher: Royal Aeronautical Society
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
93A17276
Distribution Limits
Public
Copyright
Other

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