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The conical wing in hypersonic flow

  • A. L. Gonor
  • V. I. Lapygin
  • N. A. Ostapenko
Session V 1. Shock Waves 2. Turbulence
Part of the Lecture Notes in Physics book series (LNP, volume 8)

Keywords

Shock Wave Mach Number Hypersonic Flow Delta Wing Wing Surface 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

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    Gonor, A. L. & Shvetz, A. I. “Investigation of pressure distribution on certain star shaped bodies for Mach number M = 4,” Prik. Mekh. i Tekh. Fiz. 6, 1965.Google Scholar
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    Kücheman, D. “Hypersonic aircraft and their aerodynamic problems,” Progress in Aeronautical Science, Pergamon Press, Vol. 5, 1965.Google Scholar
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    Gonor, A. L. & Shvetz, A. I. “Investigation of shock systems for flow past star shaped bodies,“ Izv. Akad Nauk SSSR, Mechanics of Liquids and Gases 3, 1966.Google Scholar
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    Gonor, A. L. & Shvetz, A. I.“Flow past V shaped wings in a supersonic stream for Mach number M = 3.9,” Izv. Akad Nauk SSSR, Mechanics of Liquids and Gases 6, 1967.Google Scholar
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    Gonor, A. L.“Flow past delta wings in a hypersonic stream,” Prik. Mat. i Mekh. 34, 3, 1970.Google Scholar
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    Gonor, A. L. & Ostapenko, N. A.“Hypersonic flow past a delta wing of finite thickness,” Izv. Akad Nauk SSSR, Mechanics of Liquids and Gases 3, 1970.Google Scholar
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Copyright information

© Springer-Verlag 1971

Authors and Affiliations

  • A. L. Gonor
    • 1
  • V. I. Lapygin
    • 1
  • N. A. Ostapenko
    • 1
  1. 1.Institute of MechanicsMoscow State UniversityUSSR

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