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

摘要

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.