Abstract:
At the present time, contacting and noncontacting (in particular, optical) diagnostic methods are used for the investigation of condensed combustion products of space system rocket (SSR) engines. All methods have their own merits and shortcomings. We note that in the history of investigating the high-temperature SSR combustion products, an overwhelming majority of the available results from the measurement of dispersed phase characteristics have been obtained using the contacting diagnostic methods.
Citation:
N. N. Ivanov, A. N. Ivanov, “Instruments and apparatus for contacting diagnostics and their application in the investigation of high-temperature two-phase flows”, Fizika Goreniya i Vzryva, 27:6 (1991), 87–101; Combustion, Explosion and Shock Waves, 27:6 (1991), 729–741
\Bibitem{IvaIva91}
\by N.~N.~Ivanov, A.~N.~Ivanov
\paper Instruments and apparatus for contacting diagnostics and their application in the investigation of high-temperature two-phase flows
\jour Fizika Goreniya i Vzryva
\yr 1991
\vol 27
\issue 6
\pages 87--101
\mathnet{http://mi.mathnet.ru/fgv3465}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 1991
\vol 27
\issue 6
\pages 729--741
\crossref{https://doi.org/10.1007/BF00814519}
Linking options:
https://www.mathnet.ru/eng/fgv3465
https://www.mathnet.ru/eng/fgv/v27/i6/p87
This publication is cited in the following 3 articles:
V. A. Arkhipov, A. A. Glazunov, N. N. Zolotorev, E. A. Kozlov, A. G. Korotkikh, V. T. Kuznetsov, V. I. Trushlyakov, “Analyzing the possibility of burning the launcher nose fairing elements”, Combustion, Explosion and Shock Waves, 59:5 (2023), 553–562
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