Aerodynamic Analysis of Active Trailing-Edge Flaps and Passive Surface Roughness on NACA 4412 Airfoil

The focus of this study is to understand the effect of the flow control mechanism on NACA 4412 airfoil. Two configuration of flow control method is used in this investigation. The first configuration is, airfoil with only the trailing-edge flap. This is the active flow control method. The trailing-e...

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Veröffentlicht in:	IOP conference series. Materials Science and Engineering 2020-10, Vol.943 (1), p.12036
Hauptverfasser:	Manickam, Thanesh A/L, Roy, Sukanta
Format:	Artikel
Sprache:	eng
Schlagworte:	Active control Airfoils Configuration management Control methods Flow control Flow separation Leading edges Surface roughness Trailing edge flaps Wind turbines
Online-Zugang:	Volltext
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