Initiation of Kerosene Combustion in a Supersonic Air Flow by a Bunch of Gas-Dynamic Pulses
- Authors: Tretyakov P.K.1
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Affiliations:
- Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences
- Issue: Vol 64, No 11 (2019)
- Pages: 438-441
- Section: Mechanics
- URL: https://journals.rcsi.science/1028-3358/article/view/193687
- DOI: https://doi.org/10.1134/S1028335819110077
- ID: 193687
Cite item
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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