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

Autor:	Ishchenko, A. N., Maslov, E. A., Skibina, N. P., Faraponov, V. V.
Předmět:	GAS flow WIND tunnels TEMPERATURE distribution SHOCK waves ENGINES GASWORKS
Zdroj:	Journal of Engineering Physics & Thermophysics; Mar2021, Vol. 94 Issue 2, p450-457, 8p
Abstrakt:	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. [ABSTRACT FROM AUTHOR]
Databáze:	Complementary Index
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