28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-2.4.2
NUMERICAL SIMULATION OF THREE-DIMENSIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION ON SHARP AND BLUNTED FLAT PLATE
V. Borovoy, I. Egorov, D. Ivanov
TsAGI, Russian Federation
Keywords: numerical simulation, boundary layer, shock wave, flat plate
Numerical investigation of gas supersonic flow on a flat plate near a single fin and a fin pair, generating crossings shocks, is performed. The study is focused upon the plate bluntness influence on the flow field and heat transfer in the interaction region.
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