Results of numerical simulation and experimental investigation of the working process of a vortex igniter-stabilizer are presented. It is shown that a high-temperature pulsating swirling jet provides reliable ignition of a fuel and its stable combustion at a main-flow velocity of up to 2.5 M.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 89, No. 5, pp. 1339–1346, September–October, 2016.
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Piralishvili, S.A., Markovich, D.M., Lobasov, A.S. et al. Simulation of the Working Process of a Supersonic Combustor with a Vortex Igniter-Stabilizer. J Eng Phys Thermophy 89, 1325–1332 (2016). https://doi.org/10.1007/s10891-016-1495-4
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DOI: https://doi.org/10.1007/s10891-016-1495-4