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Analysis of Gas Dynamics and Combustion in a Small Reverse-Flow Combustion Chamber

  • Aircraft and Rocket Engine Theory
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Abstract

This paper presents the calculation results by a reactor model, numerical simulation in ANSYS Fluent CFD software, and the results of studying the flow structure and the burn-up fuel in the reverse-flow combustion chamber. These results are intended to create a methodology for further refinement of a combustion process in a combustion chamber.

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References

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Authors and Affiliations

  1. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, Kazan, 420111, Russia

    W. M. Yousef, V. A. Sychenkov, N. V. Davydov & Yu. B. Aleksandrov

Authors
  1. W. M. Yousef
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  2. V. A. Sychenkov
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  3. N. V. Davydov
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  4. Yu. B. Aleksandrov
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Corresponding author

Correspondence to W. M. Yousef.

Additional information

Original Russian Text © W.M. Yousef, V.A. Sychenkov, N.V. Davydov, Yu.B. Aleksandrov, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 3, pp. 133–138.

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Yousef, W.M., Sychenkov, V.A., Davydov, N.V. et al. Analysis of Gas Dynamics and Combustion in a Small Reverse-Flow Combustion Chamber. Russ. Aeronaut. 61, 460–466 (2018). https://doi.org/10.3103/S1068799818030212

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  • DOI: https://doi.org/10.3103/S1068799818030212

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