Complex Investigation of Nonstationary Flow with Shock Waves in the Working Path of a Hypersonic Ramjet Engine

被引：0

作者：

A. N. Ishchenko

E. A. Maslov

N. P. Skibina

V. V. Faraponov

机构：

[1] National Research Tomsk State University,

来源：

Journal of Engineering Physics and Thermophysics | 2021年 / 94卷

关键词：

experimental investigation; mathematical simulation; ramjet engine; shock wave; drainage tests; thermometric method;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Results of a complex experiment-calculated investigation of the structure of a nonstationary gas flow in the working path of a hypersonic ramjet engine are presented. Methods of experimental determining the pressure and temperature distributions over the wall of an axisymmetric channel of complex geometry with a sudden widening are proposed and described. The problem on the gas flow over a ramjet engine positioned in a wind tunnel was solved.

引用

页码：450 / 457

页数：7

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