在不同的攻击角度下,气翼机的双面流动力学:具有倍数噪声的随机模型
Edouard Boujo1, Ivan Kharsansky Atallah2, Luc R Pastur3
1École Polytechnique Fédérale de Lausanne, Laboratory of Fluid Mechanics and Instabilities, CH-1015 Lausanne, Switzerland.
Physical review. E
|October 21, 2025
概括
我们开发了一种新的气翼机动力学模型,捕捉了附着和分离流之间的切换. 这个模型准确地预测了S形的升空曲线和流动分支,并改变了攻击角度.
科学领域:
- 流体动力学 流体动力学
- 空气动力学 在空气动力学.
- 非线性动力学是一种非线性动力学.
背景情况:
- 气翼停机动力学是复杂的,涉及连接和分离的流量状态之间的过渡.
- 了解这些可比化动态对于预测气形表表现至关重要.
- 现有的模型可能无法完全捕捉到停机的间歇性质.
研究的目的:
- 为了建模空气的间歇性可比式停机动力学.
- 开发一个一维的朗格温方程,以捕捉依赖状态的随机强迫.
- 调查攻击角度的决定性潜在变化如何影响流动行为.
主要方法:
- 提出了一个具有状态依赖的随机强迫的单维朗格温方程.
- 包含一个随着攻击角度不断变化的确定性潜力.
- 使用流量统计和动态识别了模型参数.
主要成果:
- 该模型成功地复制了特有的S形升降曲线.
- 该模型准确地捕捉了间歇性可比式停机动力学.
- 该模型预测了随着攻击角度的变化而发生的流动分支的性质.
结论:
- 拟议的兰杰文方程为模拟气形状的模型提供了一个强大的框架.
- 该模型提供了对可比式流转换的潜在机制的洞察.
- 这种方法可以帮助设计和分析在机条件附近运行的气形状.
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