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Numerical study of boundary layer interaction with shocks: Method and code validationA major problem in modeling of turbulent supersonic flows is the correct assessment of viscous-inviscid interaction problems. Of particular interest is the interaction of boundary layers with shocks. Present turbulence models give in most cases unsatisfactory results in the region of rapid distortion and in the separation region (if one is present) in particular with regard to mean flow profiles and turbulence quantities. The objective of the present work is the direct numerical simulation of shock boundary layer interaction. This report summarizes the first phase during which a numerical method suitable for this problem has been developed and a computer code has been written and tested.
Document ID
19950016044
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Adams, Nikolaus A. (Stanford Univ. CA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1994
Publication Information
Publication: Annual Research Briefs, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
95N22461
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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