A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
- Авторлар: Kolodyazhnyi D.Y.1, Nagornyi V.S.1, Sipatov A.M.2, Modorskii V.Y.3
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Мекемелер:
- Peter the Great Saint-Petersburg State Polytechnic University
- AO Aviadvigatel’
- Perm National Research Polytechnical University
- Шығарылым: Том 60, № 1 (2017)
- Беттер: 97-102
- Бөлім: 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
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
D. Kolodyazhnyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: nagorny.vladim@yandex.ru
Ресей, Politekhnicheskaya 29, Saint Petersburg, 195251
V. Nagornyi
Peter the Great Saint-Petersburg State Polytechnic University
Хат алмасуға жауапты Автор.
Email: nagorny.vladim@yandex.ru
Ресей, Politekhnicheskaya 29, Saint Petersburg, 195251
A. Sipatov
AO Aviadvigatel’
Email: nagorny.vladim@yandex.ru
Ресей, pr. Komsomol’skii 93, Perm, 614990
V. Modorskii
Perm National Research Polytechnical University
Email: nagorny.vladim@yandex.ru
Ресей, pr. Komsomol’skii 29, Perm, 614990
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