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Simulation of the test stand gas-liquid ejector operation

  • Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
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Abstract

Based on the data of numerical simulation of the test stand gas-liquid ejector operation, the fields of gasodynamic flow parameters in the gas flue channel are determined. The test stand operation in real time and processes of interaction between the flow of combustion products and neutralizing liquid are also analyzed.

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References

  1. Zabelin, L.V., Gafiyatullin, R.V., Ponik, A.N., and Meleshko, V.Yu., Osnovy promyshlennoi tekhnologii utilizatsii krupnogabaritnykh tverdotoplivnykh zaryadov (Fundamentals of Industrial Technology of Reclamation of Large-Sized Solid-Propellant Grains), Moscow: OOO Nedra-Biznesstsentr, 2004.

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Authors and Affiliations

  1. Perm’ State Technical University, Perm’, Russia

    V. Ya. Modorskii & A. V. Kozlova

Authors
  1. V. Ya. Modorskii
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  2. A. V. Kozlova
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Additional information

Original Russian Text © V.Ya. Modorskii, A.V. Kozlova, 2008, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2008, No. 1, pp. 29–32.

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Modorskii, V.Y., Kozlova, A.V. Simulation of the test stand gas-liquid ejector operation. Russ. Aeronaut. 51, 34–39 (2008). https://doi.org/10.3103/S1068799808010066

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  • DOI: https://doi.org/10.3103/S1068799808010066

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