Volume 5, Juin 2013Progress in Flight Physics
|415 - 422
|Chapter Six. Hypersonics
|14 June 2013
Delta wing with blunted leading edges at angle of attack in hypersonic flow
Institute of Theoretical and Applied Mechanics Siberian Branch of the Russian Academy of Sciences 4/1 Institutskaya Str., Novosibirsk 630090, Russia
A hypersonic rarefied diatomic gas flow around a delta wing with a blunted leading edge at an angle of attack of 10° is considered. Flow fields on the leeward and windward sides are obtained. Specific features of surface distributions of thermal characteristics on the side edge are studied.
© Owned by the authors, published by EDP Sciences, 2013
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