Abstract
The paper presents technology and results of the computational experiment on investigation of thermal radiation in the combustion chamber of a model rocket engine. Dependence of optical properties, radiation characteristics and emission characteristics on the main determining factors and parameters is analyzed.
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Original Russian Text © V.A. Kuz’min, E.I. Maratkanova, I.A. Zagrai, R.V. Rukavishnikova, 2016, published in Izvestiya VUZ, Aviatsionnaya Tekhnika, 2016, No. 1, pp. 92–97.
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Kuz’min, V.A., Maratkanova, E.I., Zagrai, I.A. et al. Simulation of thermal radiation emitted by heterogeneous combustion products in the combustion chamber of a model engine. Russ. Aeronaut. 59, 100–106 (2016). https://doi.org/10.3103/S1068799816010165
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DOI: https://doi.org/10.3103/S1068799816010165