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    Prediction of secondary separation in shock wave boundary-layer interactions (1989)
    In:  Other Sources
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    Publication Date: 2011-08-19
    Description: A complex three-dimensional shock-wave/turbulent boundary layer interaction at Mach 4 has been investigated experimentally and computationally, using two turbulence models with substantial refinement. With the use of a fine grid model, secondary flow separation was successfully computed, and grid changes did not improve agreement with experiment for the extent of upstream influence. The use of a non-isotropic turbulence model gave a slight improvement in upstream influence, but the size of the interaction was still significantly less than in the experiment.
    Keywords: AERODYNAMICS
    Type: Computers and Fluids (ISSN 0045-7930); 17; 4, 19
    Format: text
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