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Fizika Goreniya i Vzryva, 2015, Volume 51, Issue 3, Pages 41–45
DOI: https://doi.org/10.15372/FGV20150305 (Mi fgv225) 		 
Numerical study of mixing in an air-breathing rocket engine

L. L. Kartovitskii, V. M. Levin, A. A. Yakovlev

Moscow Aviation Institute (National Research University), Moscow, 125993, Russia
Full-text PDF (227 kB)
DOI: https://doi.org/10.15372/FGV20150305
Abstract: A method of increasing the efficiency of mixing in an air-breathing rocket engine is discussed. Three-dimensional simulations confirm the advantages of the proposed method based on using normal supply of products of incomplete combustion of a pasty propellant into the wake zone behind a bluff body in an air flow.
Keywords: air-breathing rocket engine, mixing, efficiency, afterburning chamber.
Received: 18.11.2013
Revised: 16.06.2014
English version:
Combustion, Explosion and Shock Waves, 2015, Volume 51, Issue 3, Pages 319–323
DOI: https://doi.org/10.1134/S0010508215030053
Bibliographic databases:
Document Type: Article
UDC: 629.735.33.016
Language: Russian
Citation: L. L. Kartovitskii, V. M. Levin, A. A. Yakovlev, “Numerical study of mixing in an air-breathing rocket engine”, Fizika Goreniya i Vzryva, 51:3 (2015), 41–45; Combustion, Explosion and Shock Waves, 51:3 (2015), 319–323
Citation in format AMSBIB
\Bibitem{KarLevYak15}
\by L.~L.~Kartovitskii, V.~M.~Levin, A.~A.~Yakovlev
\paper Numerical study of mixing in an air-breathing rocket engine
\jour Fizika Goreniya i Vzryva
\yr 2015
\vol 51
\issue 3
\pages 41--45
\mathnet{http://mi.mathnet.ru/fgv225}
\crossref{https://doi.org/10.15372/FGV20150305}
\elib{https://elibrary.ru/item.asp?id=23767567}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2015
\vol 51
\issue 3
\pages 319--323
\crossref{https://doi.org/10.1134/S0010508215030053}
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