|
This article is cited in 1 scientific paper (total in 1 paper)
Application of synthesis gas to intensify kerosene combustion in a supersonic flow
P. K. Tret'yakova, A. V. Tupikina, A. L. Kuranovb, S. V. Kolosenokb, A. A. Savarovskiyb, V. M. Abashevc a Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, 630090, Novosibirsk, Russia
b Scientific Research Facility of Hypersonic Systems (Leninets), 196066, St. Petersburg, Russia
c Moscow Aviation Institute (National Research University), 125993, Moscow, Russia
Abstract:
This study experimentally confirms the intensification of kerosene combustion in the case where a mixture simulating steam reformation products in a model combustion chamber with a supersonic velocity of the flow at the inlet. It is shown that the used mixture has a higher chemical activity than ethylene. The use of steam reformation products of hydrocarbon or synthetic propellants in schemes with pulse-periodic combustion control increases combustion efficiency without the use of special design solutions for organizing initiation and stable combustion.
Keywords:
ramjet engine, working process, propellant combustion efficiency, pressure loss, combustion chamber (CC).
Received: 05.12.2019 Revised: 24.12.2019 Accepted: 24.12.2019
Citation:
P. K. Tret'yakov, A. V. Tupikin, A. L. Kuranov, S. V. Kolosenok, A. A. Savarovskiy, V. M. Abashev, “Application of synthesis gas to intensify kerosene combustion in a supersonic flow”, Fizika Goreniya i Vzryva, 56:5 (2020), 45–48; Combustion, Explosion and Shock Waves, 56:5 (2020), 533–536
Linking options:
https://www.mathnet.ru/eng/fgv706 https://www.mathnet.ru/eng/fgv/v56/i5/p45
|
Statistics & downloads: |
Abstract page: | 44 |
|