Отправить статью по E-mail Influence Analysis of the Second Bypass Air Bleed Parameters on the Engine Performance
- Авторы: Agul’nik A.B.1, Kravchenko I.V.1, Gorbunov A.A.1, Novoselova A.A.1, Sklyarova A.P.1
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Выпуск: Том 61, № 3 (2018)
- Страницы: 441-444
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230634
- DOI: https://doi.org/10.3103/S1068799818030182
- ID: 230634
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Аннотация
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.
Об авторах
A. Agul’nik
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: agulnik201@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
I. Kravchenko
Moscow Aviation Institute (National Research University)
Email: agulnik201@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Gorbunov
Moscow Aviation Institute (National Research University)
Email: agulnik201@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Novoselova
Moscow Aviation Institute (National Research University)
Email: agulnik201@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Sklyarova
Moscow Aviation Institute (National Research University)
Email: agulnik201@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
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