Russian Aeronautics

, Volume 61, Issue 1, pp 64–70 | Cite as

Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios

  • R. R. Khaliulin
  • V. A. SychenkovEmail author
  • V. I. Panchenko
Aircraft and Rocket Engine Design and Development


This paper presents the results of an investigation of ejectors with the low entrainment ratio. A technique for calculating the ejectors with a curvilinear axis has been developed. Comparative studies of the performance characteristics of ejectors with the rectilinear axis of the mixing chamber and the curvilinear initial section of the mixing chamber are carried out.


ejector low entrainment ratio calculation technique ejector characteristic ejector with rectilinear axis curvilinear initial section of mixing chamber 


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Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • R. R. Khaliulin
    • 1
  • V. A. Sychenkov
    • 1
    Email author
  • V. I. Panchenko
    • 1
  1. 1.Tupolev Kazan National Research Technical UniversityKazan TatarstanRussia

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