Initiation of Kerosene Combustion in a Supersonic Air Flow by a Bunch of Gas-Dynamic Pulses


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Abstract

In this paper, we propose a method to initiate combustion of kerosene in a supersonic air flow in part of a combustion chamber with a constant cross section and experimentally confirm the possibility of its implementation. An intensive combustion mode is implemented using a bunch of pulses with variable energy and is maintained when the exposure is turned off after the combustion is arranged in the diverging part of the combustion chamber.

About the authors

P. K. Tretyakov

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences

Author for correspondence.
Email: paveltr@itam.nsc.ru
Russian Federation, Novosibirsk, 630090

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