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Supersonic annular jet

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Abstract

The flow in supersonic annular jets has been investigated experimentally. Schemes for shock interaction during reconstruction from an open to a closed base region are determined. The fundamental parameters characterizing the structure of the separation flow are extracted.

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Literature cited

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Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 2, pp. 59–69, March-April, 1975.

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Shvets, A.I. Supersonic annular jet. J Appl Mech Tech Phys 16, 201–208 (1975). https://doi.org/10.1007/BF00858914

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Keywords

  • Mathematical Modeling
  • Mechanical Engineer
  • Industrial Mathematic
  • Base Region
  • Separation Flow