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Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer E. A. Maslov, I. K. Zharova, E. Kozlov [et al.]
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ArticleSubject(s): сверхзвуковой воздушный поток | газовые струи | осесимметричные моделиGenre/Form: статьи в журналах Online resources: Click here to access online
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MATEC Web of conferences Vol. 115. P. 02012 (1-4)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.
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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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