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Computation of laminar viscous-inviscid interactions in high-speed internal flowsA review is given of computations for a series of nominally 2-D laminar viscous-inviscid interactions. Comparisons were made with detailed experimental shock tunnel results. The shock wave boundary layer interactions considered were induced by a compression ramp in one case and by an externally generated incident shock in the second case. In general, good agreement was reached between the grid refined calculations and experiment for the incipient and small separation conditions. For the highly separated flow, 3-D calculations which included the finite span effects of the experiment were required in order to obtain agreement with the data.
Document ID
19910011774
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rudy, David H.
(NASA Langley Research Center Hampton, VA, United States)
Thomas, James L.
(NASA Langley Research Center Hampton, VA, United States)
Kumar, Ajay
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Lewis Research Center, Computational Fluid Dynamics Symposium on Aeropropulsion
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
91N21087
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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