Impingement Characteristics Investigation of Supercooled Large Droplets Based on Eulerian Method

This numerical simulation investigates the two‑phase flow under the condition of supercooled large droplets impinging on the aircraft surface. Based on Eulerian framework， a method for calculating supercooled water droplet impingement characteristics is established. Then， considering the deformation...

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Principais autores:	YE Zekun, SHEN Xiaobin, ZHAO Jingyu, LIN Guiping
Formato:	Artigo
Idioma:	Inglês
Publicado em:	Editorial Office of Transactions of Nanjing University of Aeronautics and Astronautics 2025-04-01
coleção:	Transactions of Nanjing University of Aeronautics and Astronautics
Assuntos:	aircraft icing droplet impingement characteristics supercooled large droplet （sld） eulerian method numerical simulation
Acesso em linha:	https://tnuaa.nuaa.edu.cn/njhkhten/article/abstract/202502004?st=article_issue
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