Abstract
A mathematical model, which permits the ejector geometry to be optimized, has been designed in the framework of the inverse problem with the use of a non-equilibrium model of the two-phase gas-droplet medium and pressure law. A conventional ejector with a cylindrical chamber and diffuser is compared to the optimum geometry ejector based on numerical studies.
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Original Russian Text© I.A. Lepeshinskii, Yu.V. Zuev, V.A. Reshetnikov, I.V. Antonovskii, 2014, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2014, No. 3, pp. 33–36.
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Lepeshinskii, I.A., Zuev, Y.V., Reshetnikov, V.A. et al. Mixers based on a variable geometry ejector. Russ. Aeronaut. 57, 260–265 (2014). https://doi.org/10.3103/S1068799814030076
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DOI: https://doi.org/10.3103/S1068799814030076