A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis
- Авторы: Rybakov V.N.1, Kuz’michev V.S.1, Tkachenko A.Y.1, Krupenich I.N.1
-
Учреждения:
- Korolev Samara National Research University
- Выпуск: Том 61, № 1 (2018)
- Страницы: 78-83
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230413
- DOI: https://doi.org/10.3103/S1068799818010129
- ID: 230413
Цитировать
Аннотация
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.
Ключевые слова
Об авторах
V. Rybakov
Korolev Samara National Research University
Автор, ответственный за переписку.
Email: viktor.rybakov@gmail.com
Россия, Moskovskoe sh. 34, Samara, 443086
V. Kuz’michev
Korolev Samara National Research University
Email: viktor.rybakov@gmail.com
Россия, Moskovskoe sh. 34, Samara, 443086
A. Tkachenko
Korolev Samara National Research University
Email: viktor.rybakov@gmail.com
Россия, Moskovskoe sh. 34, Samara, 443086
I. Krupenich
Korolev Samara National Research University
Email: viktor.rybakov@gmail.com
Россия, Moskovskoe sh. 34, Samara, 443086
Дополнительные файлы
