| Issue |
Volume 5, Juin 2013
Progress in Flight Physics
|
|
|---|---|---|
| Page(s) | 415 - 422 | |
| Section | Chapter Six. Hypersonics | |
| DOI | https://doi.org/10.1051/eucass/201305415 | |
| Published online | 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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