Fluid Dynamics

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

Linear problem for triangular and V-shaped wings

  • M. I. Follé
Article
  • 11 Downloads

Keywords

Linear Problem 

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Literature cited

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    R. M. Zaidel', “Shock wave from a slightly bent piston”, Prikl. Matem. i Mekhan.,24, No. 2 (1960).Google Scholar
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    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
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    M. J. Lighthill, “The diffraction of blast, 1”, Proc. Roy. Soc., Ser. A,198, No. 1055, 454 (1949).Google Scholar
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    M. J. Lighthill, “The diffraction of blast, 2”, Proc. Roy. Soc., Ser. A,200, No. 1063, 554 (1950).Google Scholar
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    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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