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Wing of given volume with maximum lift/drag ratio in hypersonic flow

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References

  1. W. D. Hayes and R. F. Probstein, Hypersonic Flow Theory [Russian translation], Izd-vo inostr. lit., Moscow, 1962.

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  2. G. G. Chernyi, Gas Flow at High Supersonic Speed [in Russian], Fizmatgiz, Moscow, 1959.

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  3. N. V. Banichuk, V. M. Petrov, and F. L. Chernous'ko, “Numerical solution of variational and boundary value problems by the method of local variations”, Zh. vychislit. matem. i matem. fiz., vol. 6, no. 6, 1966.

  4. G. I. Maikapar, “Wing with maximum aerodynamic efficiency at hypersonic speeds”, PMM, vol. 30, no. 1, 1966.

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Perminov, V.D. Wing of given volume with maximum lift/drag ratio in hypersonic flow. Fluid Dyn 4, 92–93 (1969). https://doi.org/10.1007/BF01015966

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  • DOI: https://doi.org/10.1007/BF01015966

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