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Calculation of Parameters for Combustor with the Air–Fuel Mixture Premixing

  • AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT
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Abstract

A technique is presented for calculating the main parameters along the flame tube length in the combustor with combustion of premixed air–fuel mixtures. The calculation in the combustion zone is carried out by numerical solution of the system of equations based on the well-known brutto reaction equation of material balance for a homogeneous reactor.

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Correspondence to A. V. Baklanov.

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Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 2, pp. 95 - 99.

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Sychenkov, V.A., Baklanov, A.V. & Yousef, W.M. Calculation of Parameters for Combustor with the Air–Fuel Mixture Premixing. Russ. Aeronaut. 64, 277–282 (2021). https://doi.org/10.3103/S106879982102015X

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  • DOI: https://doi.org/10.3103/S106879982102015X

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