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

Bibliographic Details
Parent link:MATEC Web of Conferences
Vol. 115 : XXXIII Siberian Thermophysical Seminar (STS-33).— 2017.— [02012, 4 p.]
Corporate Author: Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра атомных и тепловых электростанций (АТЭС)
Other Authors: Maslov E. A. Evgeny Anatolievich, Zharova I. K., Kozlov Е., Faraponov V. V., Savkina N., Zolotorev N., Matskevich V.
Summary:Title screen
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 ч 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.
Published: 2017
Series:Chapter 2 :Turbulent flows, heat and mass transfer in single-phase flows, heat transfer enhancement
Subjects:
электронный ресурс
труды учёных ТПУ
экспериментальные исследования
осесимметрические тела
сверхзвуковые потоки
пограничные слои
локальность
Online Access:https://doi.org/10.1051/matecconf/201711502012
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=655598

Internet

https://doi.org/10.1051/matecconf/201711502012

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