A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
- Autores: Kolodyazhnyi D.Y.1, Nagornyi V.S.1, Sipatov A.M.2, Modorskii V.Y.3
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Afiliações:
- Peter the Great Saint-Petersburg State Polytechnic University
- AO Aviadvigatel’
- Perm National Research Polytechnical University
- Edição: Volume 60, Nº 1 (2017)
- Páginas: 97-102
- Seção: 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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Resumo
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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Sobre autores
D. Kolodyazhnyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: nagorny.vladim@yandex.ru
Rússia, Politekhnicheskaya 29, Saint Petersburg, 195251
V. Nagornyi
Peter the Great Saint-Petersburg State Polytechnic University
Autor responsável pela correspondência
Email: nagorny.vladim@yandex.ru
Rússia, Politekhnicheskaya 29, Saint Petersburg, 195251
A. Sipatov
AO Aviadvigatel’
Email: nagorny.vladim@yandex.ru
Rússia, pr. Komsomol’skii 93, Perm, 614990
V. Modorskii
Perm National Research Polytechnical University
Email: nagorny.vladim@yandex.ru
Rússia, pr. Komsomol’skii 29, Perm, 614990
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