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Russian Aeronautics

, Volume 61, Issue 1, pp 78–83 | Cite as

A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis

  • V. N. Rybakov
  • V. S. Kuz’michev
  • A. Yu. Tkachenko
  • I. N. Krupenich
Aircraft and Rocket Engine Theory
  • 6 Downloads

Abstract

This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system.

Keywords

method optimization parameters working process gas turbine engine engine family engine core unification 

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Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • V. N. Rybakov
    • 1
  • V. S. Kuz’michev
    • 1
  • A. Yu. Tkachenko
    • 1
  • I. N. Krupenich
    • 1
  1. 1.Korolev Samara National Research UniversitySamaraRussia

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