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Fluid Dynamics

, Volume 8, Issue 2, pp 334–338 | Cite as

Linear problem for triangular and V-shaped wings

  • M. I. Follé
Article

Keywords

Linear Problem 
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Literature cited

  1. 1.
    R. M. Zaidel', “Shock wave from a slightly bent piston”, Prikl. Matem. i Mekhan.,24, No. 2 (1960).Google Scholar
  2. 2.
    N. D. Malmuth, “Hypersonic flow over a delta wing of moderate aspect ratio”, AIAA J.,4, No. 3 (1966).Google Scholar
  3. 3.
    S. M. Ter-Minasyants, “The problem of supersonic flow over the lower surface of a triangular wing”, Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 6 (1966).Google Scholar
  4. 4.
    M. J. Lighthill, “The diffraction of blast, 1”, Proc. Roy. Soc., Ser. A,198, No. 1055, 454 (1949).Google Scholar
  5. 5.
    M. J. Lighthill, “The diffraction of blast, 2”, Proc. Roy. Soc., Ser. A,200, No. 1063, 554 (1950).Google Scholar
  6. 6.
    G. G. Chernyi, Flow of a Gas with Large Supersonic Velocity [in Russian], Fizmatgiz, Moscow (1959).Google Scholar

Copyright information

© Plenum Publishing Corporation 1975

Authors and Affiliations

  • M. I. Follé
    • 1
  1. 1.Moscow. Scientific-Research Institute of MechanicsMoscow State UniversityMoscow

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