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جستجوی مقالات
شنبه 22 آذر 1404
Energy Equipment and Systems
، جلد ۸، شماره ۳، صفحات ۲۹۷-۳۰۶
عنوان فارسی
چکیده فارسی مقاله
کلیدواژههای فارسی مقاله
عنوان انگلیسی
Simulation of an airfoil with a deformable flap applicable in wind turbine structural load reduction
چکیده انگلیسی مقاله
Flow over an airfoil equipped with Deformable Trailing Edge Flap (DTEF) has been numerically
studied in a two-dimensional steady-state condition with various angles of attack. The airfoil is NACA 64-418, and the flap angle is defined by changing camber
-
line geometry at 10% chord length from the trailing edge. It has been shown that the direction of the flap deflection has significant impacts on aerodynamic behaviors, which provides an extra means to adjust wind turbine structural loads. Simulations have been conducted with aerodynamic-aeroelastic FAST code in the form of an open-loop control scheme to determine the DTEF's performance in a wind turbine. The wind turbine behavior has been plotted and compared for various flap angles. The load-variation ranges of the wind turbine have been identified, which help determine their sensitivity to flap changes. Finally, an open-loop control circuit is aimed at reducing the amplitude of oscillations of the blade root flapwise bending moment.
کلیدواژههای انگلیسی مقاله
Trailing-Edge Flap,Aerodynamics,Wind Turbine,Smart Rotor
نویسندگان مقاله
Majid Ebrahimi |
School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran
Farzad A. Shirazi |
School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran
Kobra Gharali |
School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran
نشانی اینترنتی
https://www.energyequipsys.com/article_45681_9841045521463b00de2e769b4d7147b5.pdf
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en
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