MATEC Web Conf.
Volume 115, 2017XXXIII Siberian Thermophysical Seminar (STS-33)
|Number of page(s)||4|
|Section||Chapter 2 Turbulent flows, heat and mass transfer in single-phase flows, heat transfer enhancement|
|Published online||10 July 2017|
Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer
1 National Research Tomsk State University, Tomsk, Russia
2 National Research Tomsk Polytechnic University, Tomsk, Russia
* Corresponding author: firstname.lastname@example.org
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.
© The Authors, published by EDP Sciences, 2017
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