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Supersonic flow over sharp-edged wings

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Journal of Applied Mechanics and Technical Physics Aims and scope

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Literature cited

  1. G. P. Voskresenskii, A. S. Il'ina, and V. S. Tatarenchik, “Supersonic flow over wings with attached shock waves,” Tr. Tsentr. Aéro-Gidrodin. Inst., No. 1950 (1974).

  2. G. P. Voskresenskii, “Numerical solution of flow over an arbitrary surface of a triangular wing in the expanded supersonic region,” Izv. Akad. Nauk SSSR. Mekh. Zhidk. Gaza, No. 4 (1968).

  3. G. P. Voskresenskii, “Numerical solution of the flow over the top surface of a triangular wing in the expanded supersonic region,” Zh. Prikl. Mekh. Tekh. Fiz., No. 6 (1973).

  4. G. P. Voskresenskii, A. S. Il'ina, and V. S. Tatarenchik, Supersonic Flow over Wings, Institute of Applied Mathematics, Preprint 104 (1976).

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Authors and Affiliations

  1. Moscow

    G. P. Voskresenskii, A. S. Il'ina & V. S. Tatarenchik

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  1. G. P. Voskresenskii
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  2. A. S. Il'ina
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  3. V. S. Tatarenchik
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Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 6, pp. 35–42, November– December, 1977.

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Voskresenskii, G.P., Il'ina, A.S. & Tatarenchik, V.S. Supersonic flow over sharp-edged wings. J Appl Mech Tech Phys 18, 763–768 (1977). https://doi.org/10.1007/BF00851147

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  • DOI: https://doi.org/10.1007/BF00851147

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