电邮这篇文章 A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
- 作者: Kolodyazhnyi D.Y.1, Nagornyi V.S.1, Sipatov A.M.2, Modorskii V.Y.3
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隶属关系:
- Peter the Great Saint-Petersburg State Polytechnic University
- AO Aviadvigatel’
- Perm National Research Polytechnical University
- 期: 卷 60, 编号 1 (2017)
- 页面: 97-102
- 栏目: 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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详细
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.
作者简介
D. Kolodyazhnyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: nagorny.vladim@yandex.ru
俄罗斯联邦, Politekhnicheskaya 29, Saint Petersburg, 195251
V. Nagornyi
Peter the Great Saint-Petersburg State Polytechnic University
编辑信件的主要联系方式.
Email: nagorny.vladim@yandex.ru
俄罗斯联邦, Politekhnicheskaya 29, Saint Petersburg, 195251
A. Sipatov
AO Aviadvigatel’
Email: nagorny.vladim@yandex.ru
俄罗斯联邦, pr. Komsomol’skii 93, Perm, 614990
V. Modorskii
Perm National Research Polytechnical University
Email: nagorny.vladim@yandex.ru
俄罗斯联邦, pr. Komsomol’skii 29, Perm, 614990
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