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

Author

Ishchenko, A. N., Maslov, E. A., Skibina, N. P., and Faraponov, V. V.

Subjects
*GAS flow, *WIND tunnels, *TEMPERATURE distribution, *SHOCK waves, *ENGINES, *GASWORKS
Abstract

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]

Published
2019
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