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Numerical solution of the problem of supersonic gas flow past an arbitrary delta wing surface in the compression region

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References

  1. K. I. Babenko and G. P. Voskresenskii, “Numerical method for calculating three-dimensional supersonic gas flow around bodies”, Zh. vychislit. matem. i matem. fiz., vol. 1, no. 6, 1051–1060, 1961.

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  2. K. I. Babenko, G. P. Voskresenskii, A. N. Lyubimov, and V. V. Rusanov, Three-Dimensional Ideal Gas Flow Past Smooth Bodies [in Russian], Nedra, Moscow, 1964.

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  3. D. A. Babaev, “Numerical solution of the problem of supersonic flow over the lower surface of a delta wing”, Zh. vychislit. matem. i matem. fiz., vol. 2, no. 6, 1086–1101, 1962.

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  4. R. F. Randall, D. Bell, and J. Burk, “Pressure distribution tests of several sharp leading edge wings, bodies and body-wing combinations at mach 5 and 8”, A. E. D. C. Techn. Note, no. 173, Sept., 1960.

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Authors and Affiliations

  1. Moscow

    G. P. Voskresenskii

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  1. G. P. Voskresenskii
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I would like to thank N. A. Zaitsev for valuable assistance in programming and carrying out the calculations.

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Voskresenskii, G.P. Numerical solution of the problem of supersonic gas flow past an arbitrary delta wing surface in the compression region. Fluid Dyn 3, 90–95 (1968). https://doi.org/10.1007/BF01019205

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  • DOI: https://doi.org/10.1007/BF01019205

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