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Fizika Goreniya i Vzryva, 2008, Volume 44, Issue 6, Pages 12–17 (Mi fgv1441)  
Diagnostics of acoustic properties of the combustion zone by means of periodic changes in the nozzle throat area

Ya. A. Lisochkin

Russian Research Center "Applied Chemistry", St. Petersburg, 197198, Russia
Abstract: A mathematical model is proposed, which allows calculating the amplitude of forced pressure oscillations in the combustor of a liquid-propellant rocket engine, caused by periodic changes in the nozzle throat area, with allowance for acoustic properties of the combustion zone. Results calculated for some particular cases are given.
Keywords: high-frequency combustion, forced oscillations.
Received: 14.11.2007
Accepted: 01.03.2008
English version:
Combustion, Explosion and Shock Waves, 2008, Volume 44, Issue 6, Pages 627–631
DOI: https://doi.org/10.1007/s10573-008-0096-8
Bibliographic databases:
Document Type: Article
UDC: 629.7.036.5
Language: Russian
Citation: Ya. A. Lisochkin, “Diagnostics of acoustic properties of the combustion zone by means of periodic changes in the nozzle throat area”, Fizika Goreniya i Vzryva, 44:6 (2008), 12–17; Combustion, Explosion and Shock Waves, 44:6 (2008), 627–631
Citation in format AMSBIB
\Bibitem{Lis08}
\by Ya.~A.~Lisochkin
\paper Diagnostics of acoustic properties of the combustion zone by means of periodic changes in the nozzle throat area
\jour Fizika Goreniya i Vzryva
\yr 2008
\vol 44
\issue 6
\pages 12--17
\mathnet{http://mi.mathnet.ru/fgv1441}
\elib{https://elibrary.ru/item.asp?id=11846388}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2008
\vol 44
\issue 6
\pages 627--631
\crossref{https://doi.org/10.1007/s10573-008-0096-8}
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