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

Результат исследований: Материалы для журналаСтатья

3 Цитирования (Scopus)

Аннотация

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.

Язык оригиналаАнглийский
Номер статьи02012
ЖурналMATEC Web of Conferences
Том115
DOI
СостояниеОпубликовано - 10 июл 2017

ASJC Scopus subject areas

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

Fingerprint Подробные сведения о темах исследования «Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer». Вместе они формируют уникальный семантический отпечаток (fingerprint).

  • Цитировать