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Russian Aeronautics

, Volume 61, Issue 3, pp 441–444 | Cite as

Influence Analysis of the Second Bypass Air Bleed Parameters on the Engine Performance

  • A. B. Agul’nik
  • I. V. Kravchenko
  • A. A. Gorbunov
  • A. A. Novoselova
  • A. P. Sklyarova
Aircraft and Rocket Engine Theory
  • 4 Downloads

Abstract

This paper considers double bypass aircraft engine with controlled air bleed to the second bypass duct. Its performance is evaluated by mathematical modeling techniques. The second bypass air bleed amount is determined to provide the best engine efficiency at various operating modes.

Keywords

double bypass aircraft engine mathematical modeling controlled air bleed throttle performance 

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Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • A. B. Agul’nik
    • 1
  • I. V. Kravchenko
    • 1
  • A. A. Gorbunov
    • 1
  • A. A. Novoselova
    • 1
  • A. P. Sklyarova
    • 1
  1. 1.Moscow Aviation Institute (National Research University)MoscowRussia

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