Calculation of flow past rectangular wings and their combinations in subsonic flow using a discrete vortex scheme

  • N. F. Vorob'ev
  • G. N. Shashkina


Vortex Mathematical Modeling Mechanical Engineer Industrial Mathematic Subsonic Flow 
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Literature cited

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    V. V. Golubev, Lectures on the Theory of Wings [in Russian], Gostekhizdat, Moscow (1949).Google Scholar
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    A. A. Nikol'skii, “Second form of motion of an ideal fluid near a circumfluous body (investigation of detached flows),” Dokl. Akad. Nauk SSSR,116, No. 3 (1957).Google Scholar
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    S. M. Belotserkovskii, “Calculation of flow past wings with arbitrary shape in the plane over a wide range of angles of attack,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4 (1968).Google Scholar
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    N. F. Vorob'ev and G. N. Shashkina, “Problem of selecting a discrete vortex scheme of a wing,” in: Problems of Flow Past Bodies with Three-Dimensional Configuration [in Russian], Izd. ITPM Sib. Otd. Akad. Nauk SSSR, Novosibirsk (1978).Google Scholar
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    G. N. Shashkina and N. F. Vorob'ev, “Modeling conditions of vortex sheet detachment in calculating flow past a wing using a discrete vortex scheme,” ChMMSS,10, No. 3 (1979).Google Scholar
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    S. M. Belotserkovskii and M. I. Nisht, Detached and Undetached Ideal Fluid Flow Past Thin Wings [in Russian], Nauka, Moscow (1978).Google Scholar
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    S. D. Ermolenko, Yu. A. Rogozin, et al., “Modeling of aircraft by a thin flat surface having the shape of the projection of the aircraft in the plane,” Uch. Zap. TsAGI,10, No. 2 (1979).Google Scholar
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    N. E. Kochin, I. A. Kibel', and N. V. Roze, Theoretical Hydrodynamics [in Russian], Part 1, Fizmatgiz, Moscow (1963).Google Scholar

Copyright information

© Plenum Publishing Corporation 1984

Authors and Affiliations

  • N. F. Vorob'ev
    • 1
  • G. N. Shashkina
    • 1
  1. 1.Novosibirsk

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