Abstract
The calculation made on the basis of simple mathematical models are presented for evaluating the temperature and thermal capacity of a plasma plug flame in the GTE afterburner in a wide range of startup conditions.
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Original Russian Text © V.V. MIkhailov, V.V. Lebedev, A.N. Mukhin, 2010, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2010, No. 3, pp. 69–71.
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Mikhailov, V.V., Lebedev, V.V. & Mukhin, A.N. Application of a plasma ignition system to ignite kerosene-air mixture in the GTE afterburner in a wide range of its startup conditions. Russ. Aeronaut. 53, 349–352 (2010). https://doi.org/10.3103/S1068799810030177
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DOI: https://doi.org/10.3103/S1068799810030177