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Hypersonic flow past an airfoil with a mach system of shock waves |
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| Authors: | A. L. Gonor N. A. Ostapenko |
| Abstract: | A method based on the use of the two-approximation theory developed in [1, 2] is proposed for the computation of hypersonic flow past a conical wing with a Mach-type shock configuration.Moscow. Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 104–116, May–June, 1972. |
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