Email this article A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis
- Authors: Rybakov V.N.1, Kuz’michev V.S.1, Tkachenko A.Y.1, Krupenich I.N.1
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Affiliations:
- Korolev Samara National Research University
- Issue: Vol 61, No 1 (2018)
- Pages: 78-83
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230413
- DOI: https://doi.org/10.3103/S1068799818010129
- ID: 230413
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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.
About the authors
V. N. Rybakov
Korolev Samara National Research University
Author for correspondence.
Email: viktor.rybakov@gmail.com
Russian Federation, Moskovskoe sh. 34, Samara, 443086
V. S. Kuz’michev
Korolev Samara National Research University
Email: viktor.rybakov@gmail.com
Russian Federation, Moskovskoe sh. 34, Samara, 443086
A. Yu. Tkachenko
Korolev Samara National Research University
Email: viktor.rybakov@gmail.com
Russian Federation, Moskovskoe sh. 34, Samara, 443086
I. N. Krupenich
Korolev Samara National Research University
Email: viktor.rybakov@gmail.com
Russian Federation, Moskovskoe sh. 34, Samara, 443086
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