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ISSN 在线: 2152-209X

Archives: Volume 1, 2011 to Volume 9, 2019

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DOI: 10.1615/VisMechProc.2018026474

OBLIQUE SHOCK-WAVE INCIDENCE ON A PLATE (TWO-DIMENSIONAL FLOW)

Volf Ya. Borovoy
Central Aerohydrodynamic Institute (TsAGI), 1 Zhukovsky Str., Zhukovsky, Moscow Region, 140180 Russian Federation
Ivan Vladimirovich Egorov
Central Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky Str., Zhukovsky, Moscow Region, 140180, Russian Federation
Arkadii Sergeyevich Skuratov
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia

ABSTRACT

Experimental and numerical results of airflow and heat transfer in the vicinity of oblique shock-wave incidence on a flat plate are presented. Sharp and blunted leading edge of flat plates is conceded.