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

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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Bibliographic Details
Published in:MATEC Web of conferences Vol. 115. P. 02012 (1-4)
Other Authors: Zharova, Irina K., Kozlov, Eugene 1946-, Faraponov, Valery V., Savkina, Nadezhda, Zolotorev, Nikolay N., Matskevich, Vladislav V., Maslov, Evgeny A.
Format: Article
Language:English
Subjects:
сверхзвуковой воздушный поток
газовые струи
осесимметричные модели
статьи в журналах
Online Access:http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000644732
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http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000644732
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