Showing 621 - 640 results of 2,060 for search '"Airfoil"', query time: 0.28s Refine Results
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    Investigation of Flow Field Around a Naca Airfoil with OpenFoam and Fluent CFD Software by Zeynel Abidin Fıratoğlu, Yusuf İlhan, Hakkı Keskin, Yusuf Işıker

    Published 2021-01-01
    “…As the flow area, an airfoil with Naca 2415 section manufactured by Harran-Ravens team was selected for Teknofest competition. …”
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    Dynamic stall control over a rotor airfoil based on AC DBD plasma actuation by Guangyin Zhao, Yong Huang, Yongdong Yang, Guoqiang Li, Hesen Yang

    Published 2021-03-01
    “…Abstract At present, the control capability of dielectric barrier discharge (DBD) plasma actuation covers the flow velocity range of helicopter’s retreating blades, so it is necessary to extend it to the dynamic stall control of rotor airfoils. A DBD plasma actuator was adopted to control the dynamic stall of an oscillating CRA309 airfoil in this paper. …”
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    Numerical Investigation of the Turbulent Wake-Boundary Interaction in a Translational Cascade of Airfoils and Flat Plate by Xiaodong Ruan, Xu Zhang, Pengfei Wang, Jiaming Wang, Zhongbin Xu

    Published 2020-08-01
    “…In this paper, the correlation-based transition model is used to study the RSI phenomenon between a translational cascade of airfoils and a flat plat. A comparison was made between computational results and experimental results. …”
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  8. 628

    Numerical investigation of Electrohydrodynamic effect on Lift and Drag Forces on an airfoil in low Reynolds air flow by Mostafa Ashna

    Published 2014-12-01
    “…In this paper, the effect of electric field on two-dimensional low Reynolds air flow around an airfoil and variation of the forces acting on the airfoil is numerically investigated. …”
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  9. 629

    Aerodynamic Efficiency Improvement on a NACA-8412 Airfoil via Active Flow Control Implementation by Nil Couto, Josep M. Bergada

    Published 2022-04-01
    “…The aim is to enhance the airfoil efficiency and to maximize its lift. The boundary layer separation point was modified using Synthetic Jet Actuators (SJA), and the airfoil optimization was carried on by systematically changing the pulsating frequency, momentum coefficient and jet inclination angle. …”
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    Experimental Research of Symmetrical Airfoil Piezoelectric Energy Harvester Excited by Vortex-Induced Flutter Coupling by Xia Li, Xiaoxiao Wang, Haigang Tian, Chengming Wang, Benxue Liu

    Published 2022-12-01
    “…In order to solve the problem of self-energy supply of vehicle-mounted micro-sensors, bridge detection and some other low-power electronic devices in their working state, a vortex-induced flutter composite nonlinear piezoelectric energy harvester (VFPEH) with symmetrical airfoils on both sides of a cylindrical bluff body is designed. …”
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  13. 633

    Application of hyper-parameters adaptive MOEA/D-DE algorithm in aerodynamic stealth optimization of airfoil by WANG Peijun, XIA Lu, LUAN Weida, CHEN Huiqiang

    Published 2023-06-01
    “…The optimization results of airfoil aerodynamic stealth show that MOEA/D-DEAH algorithm has better optimization results than other algo-rithms.…”
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    An Implementation of Self-Organizing Maps for Airfoil Design Exploration via Multi-Objective Optimization Technique by SungKi Jung, Won Choi, Luiz S. Martins-Filho, Fernando Madeira

    Published 2016-04-01
    “…In this study, for the multiple-conflicting objectives that need to be simultaneously fulfilled, the real-coded Adaptive Range Multi-Objective Genetic Algorithm code, which represents the global and stochastic multi-objective evolutionary algorithm, was developed for an airfoil shape design. Furthermore, the PARSEC method reflecting geometrical properties of airfoil is adopted to generate airfoil shapes. …”
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    Experimental study on airfoil flow separation control via an air-supplement plasma synthetic jet by Ru-Bing Liu, Wen-Tao Wei, Hai-Peng Wan, Qi Lin, Fei Li, Kun Tang

    Published 2022-10-01
    “…To explore the flow control effect and mechanism of the air-supplement actuator, via particle image velocimetry experiments in a low-speed wind tunnel, the flow field and boundary layer characteristics of a two-dimensional airfoil surface under different actuation states were compared for different attack angles and jet orifices. …”
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