Vorticity statistics in the near wake of asymmetric prismatic airfoil NACA 64-618 at negative angle of attack –10° at Reynolds numbers 1.6 ⋅ 104 and 1.6 ⋅ 105 in distance 0.0 – 0.4 × chord past trailing edge measured by Particle Image Velocimetry

Open Access

Issue		MATEC Web Conf. Volume 367, 2022 21^st Conference on Power System Engineering


Article Number		00017
Number of page(s)		8
DOI		https://doi.org/10.1051/matecconf/202236700017
Published online		14 October 2022

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