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Aerodynamic characteristics of inverted-V wings at subsonic flight velocities

Fluid Dynamics volume 16, pages 886–891 (1981)Cite this article

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Literature cited

  1. T. Nonweiler, “Delta wings of shapes amenable to exact shock-wave theory,” J. R. Aeronaut. Soc.,67, 39 (1963).

    Google Scholar 

  2. A. L. Conor and A. I. Shvets, “Supersonic flow over V-shaped wings at M=3.9,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 6, 144 (1967).

    Google Scholar 

  3. V. V. Keldysh and G. I. Maikapar, “Gas-dynamic construction of hypersonic aircraft,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 177 (1969).

    Google Scholar 

  4. P. L. Roe, “Theory of waveriders,” AGARD LS-42,1, 3.1 (1972).

    Google Scholar 

  5. V. V. Kravets, N. V. Trifonova, and A. I. Shvets, “Subsonic flow over V-shaped wings,” Zh. Prikl. Mekh. Tekh. Fiz., No. 4, 102 (1975).

    Google Scholar 

  6. U. Ganzer, “Experimentelle Ergebnisse zum Nonweiler-Wellenreiter im Unterschall-, Transschall — und Überschallbereich,” Z. Flugwis.,21, 153 (1973).

    Google Scholar 

  7. S. M. Belotserkovskii, Thin Lifting Surfaces in a Subsonic Gas Stream [in Russian], Nauka, Moscow (1965), p. 242.

    Google Scholar 

  8. S. M. Belotserkovskii and M. I. Nisht, Flow of an Ideal Fluid Over Thin Wings with and without Separation [in Russian], Nauka, Moscow (1978), p. 351.

    Google Scholar 

  9. N. F. Vorob'ev and G. N. Shashkina, “On the choice of the discrete vortex scheme of a wing,” in: Problems of Flow Over Three-Dimensional Bodies (Proceedings of the Institute of Theoretical and Applied Mechanics) [in Russian], Izd. AN SSSR, Novosibirsk (1978), p. 65.

    Google Scholar 

  10. R. T. Jones and D. Cohen, “Aerodynamics of wings at high velocities,” in: Aerodynamics of Aircraft Parts at High Velocities [Russian translation], Izd. Inostr. Lit., Moscow (1959), p. 11.

    Google Scholar 

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Authors and Affiliations

  1. Moscow

    V. I. Voronin & A. I. Shvets

Authors
  1. V. I. Voronin
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  2. A. I. Shvets
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 104–109, October–December, 1981.

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Voronin, V.I., Shvets, A.I. Aerodynamic characteristics of inverted-V wings at subsonic flight velocities. Fluid Dyn 16, 886–891 (1981). https://doi.org/10.1007/BF01089718

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  • DOI: https://doi.org/10.1007/BF01089718

Keywords

  • Aerodynamic Characteristic
  • Flight Velocity
  • Subsonic Flight