Effects of smart flap on aerodynamic performance of sinusoidal leading-edge wings at low Reynolds numbers

Sinusoidal leading-edge wings have shown a high performance after the stall region. In this study, the role of smart flaps in the aerodynamics of smooth and sinusoidal leading-edge wings at low Reynolds numbers of 29,000, 40,000 and 58,000 is investigated. Four wings with NACA 634-021 profile are fi...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2021-03, Vol.235 (4), p.439-450
Hauptverfasser:	Mehraban, AA, Djavareshkian, MH, Sayegh, Y, Forouzi Feshalami, B, Azargoon, Y, Zaree, AH, Hassanalian, M
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Angle of attack Drag Fluid flow Leading edges Lift Low Reynolds number Stalling Three dimensional printing Wind tunnel testing Wind tunnels
Online-Zugang:	Volltext
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