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

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...

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Main Authors: Maslov Evgeny, Zharova Irina, Kozlov Evgeny, Faraponov Valery, Savkina Nadezhda, Zolotorev Nikolay, Matskevich Vladislav
Format: Article
Language:English
Published: EDP Sciences 2017-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201711502012
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author Maslov Evgeny
Zharova Irina
Kozlov Evgeny
Faraponov Valery
Savkina Nadezhda
Zolotorev Nikolay
Matskevich Vladislav
author_facet Maslov Evgeny
Zharova Irina
Kozlov Evgeny
Faraponov Valery
Savkina Nadezhda
Zolotorev Nikolay
Matskevich Vladislav
author_sort Maslov Evgeny
collection DOAJ
description 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.
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spelling doaj.art-baa25ef6a47e47789e5bc4f2bbffc5012022-12-21T20:02:09ZengEDP SciencesMATEC Web of Conferences2261-236X2017-01-011150201210.1051/matecconf/201711502012matecconf_sts2017_02012Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layerMaslov EvgenyZharova Irina0Kozlov Evgeny1Faraponov Valery2Savkina Nadezhda3Zolotorev Nikolay4Matskevich Vladislav5National Research Tomsk Polytechnic UniversityNational Research Tomsk Polytechnic UniversityNational Research Tomsk State UniversityNational Research Tomsk State UniversityNational Research Tomsk State UniversityNational Research Tomsk State UniversityA 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.https://doi.org/10.1051/matecconf/201711502012
spellingShingle Maslov Evgeny
Zharova Irina
Kozlov Evgeny
Faraponov Valery
Savkina Nadezhda
Zolotorev Nikolay
Matskevich Vladislav
Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer
MATEC Web of Conferences
title Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer
title_full Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer
title_fullStr Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer
title_full_unstemmed Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer
title_short Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer
title_sort experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer
url https://doi.org/10.1051/matecconf/201711502012
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