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Prediction of hypersonic shock-wave/turbulent-boundary-layer interaction flowsSolutions of the Reynolds-averaged Navier-Stokes equations are presented and compared with experimental surface data for a series of hypersonic shock-wave/turbulent-boundary-layer interaction flows. The turbulence models used include algebraic and two-equation eddy-viscosity models developed for transonic and supersonic flows. Also several additional modifications to the two-equation model to account for compressibility effects are developed and used. Although the modifications improve the agreement with the experimental data, no single model or modification correctly predicts all the test cases.
Document ID
19870055202
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Horstman, C. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 87-1367
Accession Number
87A42476
Distribution Limits
Public
Copyright
Other

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