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...
Main Authors: | , , , , , , |
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Format: | Article |
Language: | English |
Published: |
EDP Sciences
2017-01-01
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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. |
first_indexed | 2024-12-19T23:14:05Z |
format | Article |
id | doaj.art-baa25ef6a47e47789e5bc4f2bbffc501 |
institution | Directory Open Access Journal |
issn | 2261-236X |
language | English |
last_indexed | 2024-12-19T23:14:05Z |
publishDate | 2017-01-01 |
publisher | EDP Sciences |
record_format | Article |
series | MATEC Web of Conferences |
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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