Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer

Evgeny Maslov, Irina Zharova, Evgeny Kozlov, Valery Faraponov, Nadezhda Savkina, Nikolay Zolotorev, Vladislav Matskevich

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3 Citations (Scopus)


A technique of experimental determination of the parameters and structure of supersonic air flow around of axisymmetric bodies form in the range of Mach numbers M = (2 ÷ 5) are presented. The results of the investigation of the interaction a supersonic stream flowing around of an axisymmetric model with gas jet which inject into the boundary layer are given.

Original languageEnglish
Article number02012
JournalMATEC Web of Conferences
Publication statusPublished - 10 Jul 2017


ASJC Scopus subject areas

  • Chemistry(all)
  • Engineering(all)
  • Materials Science(all)

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