27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-3.5.1

SHOCK WAVE IMPINGEMENT ON BOUNDARY AND ENTROPY LAYERS OF A BLUNT PLATE

V. Borovoy, I. Egorov, A. Skuratov
TsAGI, Russian Federation

Keywords: shock wave, boundary layer, interaction, stanton number, laminar-turbulent transition

The objective of this paper is an experimental and numerical investigation of oblique shock impingement on laminar and turbulent boundary layers of sharp and blunt plates. The present paper focuses on the bluntness influence in the interference region.

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