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Leeward Separated Supersonic Flows

  • V. Ya. Borovoi
  • V. N. Brazhko
  • G. I. Maikapar
Conference paper
Part of the International Union of Theoretical and Applied Mechanics book series (IUTAM)

Summary

Using various experimental methods the “architecture” of the separated flows formed at the lee-side of a blunt cone and delta wing is investigated. The flow structure evolution during the variation of the angle of attack and the Mach number is discussed.

Keywords

Shock Wave Mach Number Separation Zone Leeward Side Primary Vortex 
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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Copyright information

© Springer-Verlag, Berlin Heidelberg 1991

Authors and Affiliations

  • V. Ya. Borovoi
    • 1
  • V. N. Brazhko
    • 1
  • G. I. Maikapar
    • 1
  1. 1.Central Aero-Hydrodynamic Institute ZhukovskyUSSR

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