Unsteady wall pressure distribution (476 taps) over a 2D airfoil section at chord-based Reynolds number ranging from 0.5 to 3.4 Millions.
收藏DataCite Commons2026-03-27 更新2026-03-28 收录
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https://awit.aeris-data.fr/catalogue-mistery/?uuid=58997972-d17d-479b-8355-bd1b58c9c8f3
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资源简介：
The spanwise organization of the flow over a thick airfoil is investigated using surface pressure measurements for a range of angles of attack around maximum lift and high Reynolds numbers (0.5 to 3.4 Million). With this dataset, it is possible to track global dynamics from local measurements as detailed in https://doi.org/10.48550/arXiv.2602.03844
提供机构：
Aeris
创建时间：
2026-03-10
