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Supersonic flow over a triangular wing

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Literature cited

  1. M. D. Ladyzhenskii, “Three-dimensional hypersonic flow over thin wings,” Prikl. Mat. Mekh.,28, No. 5 (1964).

  2. V. Ya. Neiland, “Propagation of perturbations upstream in the interaction of a hypersonic flow and a boundary layer,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4 (1970).

  3. I. G. Kozlova and V. V. Mikhailov, “Strong viscous interaction on triangular and slipflow wings,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 6 (1970).

  4. V. Ya. Neiland, “Theory of interaction of a hypersonic stream with a boundary layer for separated two-dimensional and three-dimensional flows. Part 2. Two-dimensional flows and a triangular wing,” Uch. Zap. Tsentr. Aero. Gidro. Inst.,5, No. 3 (1974).

  5. G. N. Dudin, “Characteristics of a three-dimensional hypersonic boundary layer in the vicinity of the plane of symmetry of a triangular wing,” Tr. Tsentr. Aero. Gidro. Inst., No. 2177 (1983).

  6. G. N. Dudin, “Computation of the boundary layer on a triangular plate in the strong viscous interaction regime,” Uchebn. Zap. Tsentr. Aero. Gidro. Inst.,9, No. 5 (1978).

  7. G. N. Dudin and D. O. Lyzhin, “One method of computing the regime of strong viscous interaction on a triangular wing,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4 (1983).

  8. V. Ya. Neiland, “Theory of interaction of a hypersonic stream with a boundary layer for separated two-dimensional and three-dimensional flows. Part 1. Three-dimensional flows,” Uchen. Zap. Tsentr. Aero. Gidro. Inst.,5, No. 2 (1974).

  9. W. D. Hayes and R. F. Probstein (eds.), Hypersonic Flow Theory, Academic Press (1967).

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Authors and Affiliations

  1. Moscow

    G. N. Dudin & I. I. Lipatov

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  1. G. N. Dudin
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  2. I. I. Lipatov
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Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 3, pp. 100–106, May–June, 1985.

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Dudin, G.N., Lipatov, I.I. Supersonic flow over a triangular wing. J Appl Mech Tech Phys 26, 391–396 (1985). https://doi.org/10.1007/BF00910376

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  • DOI: https://doi.org/10.1007/BF00910376

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