开发基于OpenFOAM的3D欧利尔/拉格兰吉飞机冰模拟解决方案
Han Han1, Zifei Yin1, Yijun Ning2
1School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China.
Entropy (Basel, Switzerland)
|July 8, 2023
概括
一个新的3D结冰模拟代码准确地预测了气翼上的冰形状. 它使用混合网格和双滴滴跟踪方法,以提高飞机结冰研究的准确性.
科学领域:
- 航空航天工程 航空航天工程
- 计算流体动力学 (CFD) 是一种计算流体动力学.
- 冰积累物理 冰积累物理
背景情况:
- 飞机的结冰会造成严重的安全风险.
- 精确模拟冰积累对于飞机设计和安全至关重要.
- 现有的方法与复杂的几何形状和各种水滴大小作斗争.
研究的目的:
- 开发和验证一个新的3D冰化模拟代码.
- 为了提高预测冰积累在气形和翅膀上的预测准确度.
- 为超冷大滴 (SLD) 集成先进的滴滴跟踪.
主要方法:
- 在OpenFOAM框架内开发了一个3D结冰模拟代码.
- 在复杂的几何形状中采用混合的卡特西安/机身配套网格策略.
- 实施了欧勒尔和拉格朗的滴滴跟踪方法,用于不同的滴滴大小.
- 使用雷诺兹平均纳维埃-斯托克斯 (RANS) 方程和迈尔斯冰积累模型.
主要成果:
- 模拟代码证明了在预测冰形状方面的可行性和准确性.
- 通过使用欧勒尔和拉格朗日方法对二维几何的3D模拟进行验证.
- 成功模拟了M6翼上的冰积累,展示了完整的3D功能.
结论:
- 开发的3D冰化模拟代码是预测冰积累的可行工具.
- 混合网格和双滴滴跟踪方法提高了模拟准确度.
- 该代码为进一步研究飞机冰封提供了一个强大的平台.
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