Dynamic stall control over an airfoil by NS-DBD actuation

The wind tunnel test was conducted with an NACA 0012 airfoil to explore the flow control effects on airfoil dynamic stall by NS-DBD plasma actuation. Firstly, light and deep dynamic stall states were set, based on the static stall characteristics of airfoil at a Reynolds number of 5.8 × 10 5 . Then,...

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Veröffentlicht in:	Chinese physics B 2020-10, Vol.29 (10), p.105203
Hauptverfasser:	Yang, He-Sen, Zhao, Guang-Yin, Liang, Hua, Wei, Biao
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
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