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arXiv 2603.02472physics.flu-dyn

层流与湍流极端涡旋风遭遇中的涡旋相似性

Vortical similarities across laminar and turbulent extreme gust encounters

Hiroto Odaka, Barbara Lopez-Doriga, Kunihiko Taira

AI总结:

研究揭示了在极端涡旋风遭遇中,方形机翼上层流与湍流流动的显著相似性,发现大尺度涡旋核心结构在不同雷诺数下具有相似特征,为高雷诺数流动建模提供新见解。

摘要:

本文研究揭示了在极端涡旋风遭遇中,方形机翼上层流与湍流流动的显著相似性。大尺度涡旋核心结构负责显著的瞬时升力变化,在Re=600和10,000时表现出 remarkable 相似性。这些结构的形成归因于机翼表面由强风引起的涡量通量,导致低雷诺数和高雷诺数流动之间共享大尺度拓扑特征。尽管Re=10,000情况下细尺度涡旋结构迅速形成,但湍流流动的尺度分解识别出的大型结构与Re=600时观察到的相似。这些发现表明,层流极端气动流动中的大尺度涡旋特征为高雷诺数流动提供了关键见解,可能降低极端气动流动的建模和控制复杂性。

英文摘要:

This study uncovers a striking similarity between massively separated laminar and turbulent flows that develop over a square wing during extreme vortex gust encounters. The evolving large-scale, vortical core structures responsible for significant transient lift variations exhibit remarkable similarity across Re = 600 and 10,000. The formation of these structures is attributed to a substantial gust-induced vorticity flux produced at the wing surface, resulting in shared large-scale topological features between the low- and high-Reynolds-number flows. Although fine-scale vortical structures quickly emerge in the Re = 10,000 case, the large-scale structures identified by scale decomposition of the turbulent flow resemble those observed at Re = 600. These findings suggest that large-scale vortical features present in laminar extreme aerodynamic flows provide key insights into their higher Reynolds number counterparts, potentially reducing the complexity of flow modeling and control for extreme aerodynamics.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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