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Gas ejector with isobaric mixing chamber

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Abstract

A method is proposed for calculating a gas ejector with a tapering isobaric mixing chamber. The efficiency of ejectors with isobaric and cylindrical mixing chambers is compared.

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References

  1. Vasil’ev, Yu.N., Theory of a Supersonic Gas Ejector with a Cylindrical Mixing Chamber, Lopatochnye mashiny i struinye apparaty (Propeller Machines and Jet Equipment), Moscow: Mashinostroenie, 1967, issue 2, pp. 171–225.

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  2. Abramovich, G.N., Prikladnaya gazovaya dinamika (Applied Gas Dynamics), Moscow: Nauka, 1976.

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  3. Aleksandrov, V.Yu. and Klimovskii, K.K., Theory of Supersonic Gas Ejectors, Teploenergetika, 2009, no. 8, pp. 31–33.

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Authors and Affiliations

  1. Baranov Central Institute of Aviation Motors, Moscow, Russia

    V. Yu. Aleksandrov & K. K. Klimovskii

Authors
  1. V. Yu. Aleksandrov
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  2. K. K. Klimovskii
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Additional information

Original Russian Text © V.Yu. Aleksandrov, K.K. Klimovskii, 2010, published in Vestnik Mashinostroeniya, 2010, No. 10, pp. 11–15.

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Aleksandrov, V.Y., Klimovskii, K.K. Gas ejector with isobaric mixing chamber. Russ. Engin. Res. 30, 976–979 (2010). https://doi.org/10.3103/S1068798X10100023

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  • DOI: https://doi.org/10.3103/S1068798X10100023

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