Results 11 to 20 of about 16,699 (209)
Energies, 2020 Theoretical modeling and the sliding mode control (SMC) of an active trailing-edge flap of a wind turbine blade based on the adaptive reaching law are investigated.
Tingrui Liu +3 more
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Combined Pitch and Trailing Edge Flap Control for Load Mitigation of Wind Turbines
Energies, 2018 Using active control methods for load mitigation in wind turbines could greatly reduce the cost of per kilowatt hour of wind power. In this work, the combined pitch and trailing edge flap control (CPFC) for load mitigation of wind turbines is ...
Keshan He +3 more
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Alleviation of Dynamic Stall Moments by Morphing Flap
Hangkong gongcheng jinzhan, 2021 Active deflection of trailing edge control surface can reduce the adverse effect of airfoil dynamic stall on aerodynamic characteristics.This study set out to investigate the performance of morphing flap on dynamic stall alleviation.
OUYANG Yan +3 more
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Shanghai Jiaotong Daxue xuebao, 2022 Low power efficiency is a critical factor that restricts marketization development of the vertical axis wind turbine (VAWT). The proposal of the trailing edge flap can change flow structure on blade surface, so as to improve the aerodynamic performance ...
DAI Mengyi, ZHANG Zhihao, TU Jiahuang, HAN Zhaolong, ZHOU Dai, ZHU Hongbo
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Journal of Marine Science and Engineering, 2020 As a result of the large-scale trend of offshore wind turbines, wind shear and turbulent wind conditions cause significant fluctuations of the wind turbine’s torque and thrust, which significantly affect the service life of the wind turbine gearbox
Xin Cai +3 more
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Applied Sciences, 2022 In this paper, the dynamic balance of a rigid variable speed rotor is tested and analyzed. The vibration acceleration is measured by vibration analyzer instrumentations.
Liang Li, Ming Chen, Fang Wang, Anan Xu
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3D Turbulent Boundary Layer Separation Control by Multi-Discharge Plasma Actuator
Aerospace, 2023 In a subsonic wind tunnel, a three-dimensional separation of a developed turbulent boundary layer was simulated on a swept wing flap model. A multi-discharge plasma actuator operating on the basis of dielectric barrier discharge was used to overcome the ...
Sergey Chernyshev +4 more
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Active Management of Flap-Edge Trailing Vortices [PDF]
4th Flow Control Conference, 2008 The vortex hazard produced by large airliners and increasingly larger airliners entering service, combined with projected rapid increases in the demand for air transportation, is expected to act as a major impediment to increased air traffic capacity.
David Greenblatt +4 more
openaire +1 more source
Авіаційно-космічна техніка та технологія, 2023 The subject of study in this article is the effect of mechanization of the trailing edge of the wing, located along 95% of the wing console, on the lift coefficient, drag coefficient, and aerodynamic quality of the wing during takeoff operation for a ...
Leonid Zavorotynskyi, Dmytro Konotop
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Design and Aerodynamic Authority Analysis of ContinuousTrailing-edge Flap for Helicopter Blade
Hangkong gongcheng jinzhan, 2018 Continuous trailing-edge flap has many advantages over conventional discrete flap in helicopter rotor vibration reduction applications, such as light weight, compact structure and stable airflow. Macro fiber composite is chosen as the actuating material.
Li Yun +3 more
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