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Hypersonic flow past blunt-edged delta wings |
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| Authors: | S A Gorokhov V V Eremin A M Polyakov |
| Abstract: | A method is proposed for calculating hypersonic ideal-gas flow past blunt-edged delta wings with aspect ratios  = 100–200. Systematic wing flow calculations are carried out on the intervals 6  M 20, 0  20 , 60  80; the results are analyzed in terms of hypersonic similarity parameters.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 5, pp. 175–179, September–October, 1990. |
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