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

Evgeny Maslov, Irina Zharova, Evgeny Kozlov, Valery Faraponov, Nadezhda Savkina, Nikolay Zolotorev, Vladislav Matskevich

Научно-образовательный центр И.Н.Бутакова

Результат исследований: Материалы для журнала › Статья

3 Цитирования (Scopus)

Аннотация

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.

Язык оригинала	Английский
Номер статьи	02012
Журнал	MATEC Web of Conferences
Том	115
DOI	https://doi.org/10.1051/matecconf/201711502012
Состояние	Опубликовано - 10 июл 2017

ASJC Scopus subject areas

Chemistry(all)
Engineering(all)
Materials Science(all)

Доступ к документу

10.1051/matecconf/201711502012

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Цитировать

Maslov, E., Zharova, I., Kozlov, E., Faraponov, V., Savkina, N., Zolotorev, N., & Matskevich, V. (2017). Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer. MATEC Web of Conferences, 115, [02012]. https://doi.org/10.1051/matecconf/201711502012

Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer. / Maslov, Evgeny; Zharova, Irina; Kozlov, Evgeny; Faraponov, Valery; Savkina, Nadezhda; Zolotorev, Nikolay; Matskevich, Vladislav.

В: MATEC Web of Conferences, Том 115, 02012, 10.07.2017.

Результат исследований: Материалы для журнала › Статья

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