基于VOF模型对轮子喷雾和着陆水积累的冰化计算的模拟
Jiaqi Dai1, Lifen Zhang2, Qixi Chen1
1School of Power and Energy, Northwestern Polytechnical University, Xi'an, 710072, China.
Scientific reports
|March 4, 2026
概括
飞机着陆的结冰是由于跑道喷水而引起的安全问题. 数字模拟表明,在潮湿的条件下行驶时最大的冰积累不会威胁起飞和着陆的安全.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 热力学是一种热力学.
背景情况:
- 飞机的着陆是脆弱的冰积累从滑道喷雾水在潮湿的条件下.
- 降落上形成的冰块可能会在起飞和降落期间危及飞机的安全.
研究的目的:
- 为了数值模拟和分析飞机着陆架上的水膜结冰过程.
- 评估极端跑道和天气条件下冰积累对安全的影响.
主要方法:
- 在Fluent软件中开发了一种有限体积模型,用于水积累动态.
- 利用流体体积 (VOF) 模型和网状运动来计算水膜厚度.
- 采用热力学平衡方程来估计冰的积累厚度.
主要成果:
- 分析了诸如空气动力学阻力和重力等外部因素对水膜厚度的影响.
- 基于水膜动态计算的保守冰积累厚度.
- 确定估计的冰积累不会影响飞机的安全.
结论:
- 该研究证实,车轮喷雾和着陆水积累的最大冰积累在驾驶过程中不会对飞机安全构成威胁.
- 数字模拟为分析着陆结冰现象提供了一种资源高效的方法.
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