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Turbulent properties of axisymmetric shock-wave/boundary-layer interaction flowsA combined experimental and computational investigation of an axisymmetric turbulent shock-wave boundary-layer interaction flow is presented. Experimental measurements include both mean and fluctuating data obtained by LDV techniques and identify large scale unsteady motions associated with shock induced separation. Computations using the compressible Navier-Stokes equations, and a two-equation turbulence model are in relatively good agreement with experimental measurements. It is found that the large scale unsteady motions do not appear to have a critical impact on the ability to compute the mean properties of the flows investigated in this paper.
Document ID
19880063934
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Brown, J. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Kussoy, M. I.
(NASA Ames Research Center Moffett Field, CA, United States)
Coakley, T. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Accession Number
88A51161
Distribution Limits
Public
Copyright
Other

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