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Evaluation of the possibility of using combustion promoters in hydrocarbon fuels for perspective jet engines
- Authors: Petrukhin N.V.1, Sergeev S.M.2, Prokopenko O.A.2, Grek M.O.3
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Affiliations:
- 25-th State Research Institute of Chemmotology, Ministry of Defence of Russian Federation
- “25 State Scientific and Research Institute of Chemmotology of the Russian Ministry of Defense”, Moscow
- Military Academy of Strategic Rocket Forces named after Peter the Great, Moscow
- Issue: Vol 12, No 3-2 (2013): Vestnik SSAU
- Pages: 152-157
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/1836
- DOI: https://doi.org/10.18287/1998-6629-2013-0-3-2(41)-152-157
- ID: 1836
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Abstract
The article presents the analysis of published data and results of experimental studies performed by the authors regarding the effect of combustion promoters – peroxides and hydro-peroxides on the turbulent burning rate of fuel TS-1. It was determined that the specific pulse thrust of the model pulse-detonating engine may be increased by 2.5 - 3.0 times. The same goes for the degree and burning rate of the fuel-air mixture. The authors explain the mechanism of action of promoters for increasing the activity of the fuel-air mixture in the process of combustion.
About the authors
N. V. Petrukhin
25-th State Research Institute of Chemmotology, Ministry of Defence of Russian Federation
Author for correspondence.
Email: 25gosniihim@mail.ru
Doctor of Science (Engineering), Professor
Chief Researcher
Russian FederationS. M. Sergeev
“25 State Scientific and Research Institute of Chemmotology of the Russian Ministry of Defense”, Moscow
Email: ssm.58@mail.ru
Candidate of Science (Engineering), Associate Professor
Head of Laboratory
Russian FederationO. A. Prokopenko
“25 State Scientific and Research Institute of Chemmotology of the Russian Ministry of Defense”, Moscow
Email: procopenco@mail.ru
Candidate of Science (Engineering)
Senior Researcher
Russian FederationM. O. Grek
Military Academy of Strategic Rocket Forces named after Peter the Great, Moscow
Email: arvs@mail.ru
Candidate of Science (Engineering)
Lecturer
Russian FederationReferences
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- Тангирала В.Е. Численные исследования импульсного детонационного двигателя [Текст] // Импульсные детонационные двигатели; под ред. д.ф.-м.н. С.М. Фролова - М.: ТОРУСС ПРЕСС, 2006. - С. 373-412.
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