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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Abstract

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
Volume115
DOIs
Publication statusPublished - 10 Jul 2017

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ASJC Scopus subject areas

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

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