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Fizika Goreniya i Vzryva, 2012, Volume 48, Issue 4, Pages 38–50 (Mi fgv2)  
This article is cited in 10 scientific papers (total in 10 papers)

Gas dynamics and thrust in the exhaust system of a jet engine with an annular nozzle

V. A. Levina, N. E. Afoninaa, V. G. Gromova, G. D. Smekhova, A. N. Khmelevskiia, V. V. Markovba

a Institute of Mechanics at the Lomonosov Moscow State University, Moscow, Russia
b Steklov Mathematical Institute, Russian Academy of Sciences, Moscow, Russia
Full-text PDF (770 kB) Citations (10)
Abstract: Results of a comprehensive numerical and experimental study of the dynamics of the flow of equilibrium combustion products of stoichiometric acetylene-air mixtures in the exhaust system of a jet engine with an annular nozzle are presented. Results of the numerical solution of unsteady Navier–Stokes equations for a chemically nonequilibrium model of a multispecies gas medium are reported. Experiments are performed in a hotshot aerodynamic setup. Thrust characteristics of the exhaust system of the jet engine are determined, and specific features of the structure of a steady flow formed there are found.
Keywords: annular nozzle, exhaust system, jet engine Navier–Stokes equations, combustion.
Funding agency Grant number
Russian Foundation for Basic Research 12-01-90416-Ukr_a
11-01-00068-a
Ministry of Education and Science of the Russian Federation NSh-8424.2010.1
This work was supported by the Russian Foundation for Basic Research (Grant Nos. 12-01-90416-Ukr_a and 11-01-00068a) and by the Grant of the President of the Russian Federation for Supporting the Leading Scientific Schools (Grant No. NSh-8424.2010.1).
Received: 22.06.2011
English version:
Combustion, Explosion and Shock Waves, 2012, Volume 48, Issue 4, Pages 406–417
DOI: https://doi.org/10.1134/S0010508212040053
Bibliographic databases:
Document Type: Article
UDC: 533.697.4+544.452+519.63
Language: Russian
Citation: V. A. Levin, N. E. Afonina, V. G. Gromov, G. D. Smekhov, A. N. Khmelevskii, V. V. Markov, “Gas dynamics and thrust in the exhaust system of a jet engine with an annular nozzle”, Fizika Goreniya i Vzryva, 48:4 (2012), 38–50; Combustion, Explosion and Shock Waves, 48:4 (2012), 406–417
Citation in format AMSBIB
\Bibitem{LevAfoGro12}
\by V.~A.~Levin, N.~E.~Afonina, V.~G.~Gromov, G.~D.~Smekhov, A.~N.~Khmelevskii, V.~V.~Markov
\paper Gas dynamics and thrust in the exhaust system of a jet engine with an annular nozzle
\jour Fizika Goreniya i Vzryva
\yr 2012
\vol 48
\issue 4
\pages 38--50
\mathnet{http://mi.mathnet.ru/fgv2}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2012
\vol 48
\issue 4
\pages 406--417
\crossref{https://doi.org/10.1134/S0010508212040053}
\isi{https://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcApp=Publons&SrcAuth=Publons_CEL&DestLinkType=FullRecord&DestApp=WOS_CPL&KeyUT=000308042200005}
\scopus{https://www.scopus.com/record/display.url?origin=inward&eid=2-s2.0-84870472489}
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    • This publication is cited in the following 10 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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