Отправить статью по E-mail A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
- Авторы: Kolodyazhnyi D.Y.1, Nagornyi V.S.1, Sipatov A.M.2, Modorskii V.Y.3
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Учреждения:
- Peter the Great Saint-Petersburg State Polytechnic University
- AO Aviadvigatel’
- Perm National Research Polytechnical University
- Выпуск: Том 60, № 1 (2017)
- Страницы: 97-102
- Раздел: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230010
- DOI: https://doi.org/10.3103/S1068799817010147
- ID: 230010
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Аннотация
A technique for calculating the two-phase flows in the pneumatic injector of the aircraft engine is developed based on solving the model problem, namely, on verification of the two-phase flow model by means of solving the problem of liquid column disintegration under the effect of an incident airflow. We determine the turbulence models that satisfactorily describe the biphase flow processes.
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Об авторах
D. Kolodyazhnyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: nagorny.vladim@yandex.ru
Россия, Politekhnicheskaya 29, Saint Petersburg, 195251
V. Nagornyi
Peter the Great Saint-Petersburg State Polytechnic University
Автор, ответственный за переписку.
Email: nagorny.vladim@yandex.ru
Россия, Politekhnicheskaya 29, Saint Petersburg, 195251
A. Sipatov
AO Aviadvigatel’
Email: nagorny.vladim@yandex.ru
Россия, pr. Komsomol’skii 93, Perm, 614990
V. Modorskii
Perm National Research Polytechnical University
Email: nagorny.vladim@yandex.ru
Россия, pr. Komsomol’skii 29, Perm, 614990
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