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Tr. Mat. Inst. Steklova, 2018, Volume 300, Pages 123–134 (Mi tm3866)  

Control of detonation combustion in a high-velocity gas mixture flow

V. A. Levinabc, T. A. Zhuravskayaab

a Institute of Mechanics, Moscow State University, Michurinskii pr. 1, Moscow, 119192 Russia
b Central Aerohydrodynamic Institute, ul. Zhukovskogo 1, Zhukovsky, Moscow oblast, 140180 Russia
c Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences, ul. Radio 5, Vladivostok, 690041 Russia

Abstract: Within the framework of a detailed kinetic mechanism of chemical interaction, we study detonation combustion of a stoichiometric hydrogen–air mixture flowing at a supersonic velocity into a plane symmetric channel with narrowing cross section (constriction). The goal of the study is to determine conditions that guarantee the formation of a thrust-producing flow with a stabilized detonation wave in the channel. With a view to increasing the efficiency of detonation combustion of the gas mixture, we analyze the effect of variations of the inflow Mach number, the concentration of inert particles added to the combustible mixture flowing into the channel, and the geometric parameters of the channel on the position of a stabilized detonation wave in the flow. We also study the possibility of formation without energy expenditure of a thrust-producing flow with a stabilized detonation wave in a channel with narrowing cross section.

Funding Agency Grant Number
Ministry of Education and Science of the Russian Federation 14.G39.31.0001
Russian Foundation for Basic Research 16-29-01092
18-01-00883
This work was performed according to the research plan of the Institute of Mechanics, Moscow State University, and supported by the Ministry of Education and Science of the Russian Federation (contract no. 14.G39.31.0001 of February 13, 2017). The study of the effect of inert particles added to a gas mixture on the stabilization of detonation combustion in a flow was supported by the Russian Foundation for Basic Research (project nos. 16-29-01092 and 18-01-00883).


DOI: https://doi.org/10.1134/S0371968518010090

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English version:
Proceedings of the Steklov Institute of Mathematics, 2018, 300, 114–125

Bibliographic databases:

UDC: 533.6.011.5+534.222.2
Received: October 20, 2017

Citation: V. A. Levin, T. A. Zhuravskaya, “Control of detonation combustion in a high-velocity gas mixture flow”, Modern problems and methods in mechanics, Collected papers. On the occasion of the 110th anniversary of the birth of Academician Leonid Ivanovich Sedov, Tr. Mat. Inst. Steklova, 300, MAIK Nauka/Interperiodica, Moscow, 2018, 123–134; Proc. Steklov Inst. Math., 300 (2018), 114–125

Citation in format AMSBIB
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\by V.~A.~Levin, T.~A.~Zhuravskaya
\paper Control of detonation combustion in a~high-velocity gas mixture flow
\inbook Modern problems and methods in mechanics
\bookinfo Collected papers. On the occasion of the 110th anniversary of the birth of Academician Leonid Ivanovich Sedov
\serial Tr. Mat. Inst. Steklova
\yr 2018
\vol 300
\pages 123--134
\publ MAIK Nauka/Interperiodica
\publaddr Moscow
\mathnet{http://mi.mathnet.ru/tm3866}
\crossref{https://doi.org/10.1134/S0371968518010090}
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