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Numerical Study of Aerodynamic Performance of Airfoils at Low Angles of Attack by Active Flow Control of Trailing Edge Vortices

机译：后缘涡流主动控制在低迎角翼型气动性能数值研究

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《AIAA Aerospace Sciences Meeting and Exhibit》|2006年|P.1-20|共20页
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J. Vadillo; R. Agarwal;
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中图分类航空;
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2. Numerical study of the aerodynamic performance of blunt trailing-edge airfoil considering the sensitive roughness height [J] . Zhang Xu, Wang Gege, Zhang Mengjie, International journal of hydrogen energy . 2017,第29期

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3. Aerodynamic Flow Control of an Airfoil with Small Trailing-Edge Strips [J] . Deman Tang, Earl H. Dowell Journal of Aircraft . 2006,第6期

机译：带有小后缘条的翼型的气动流动控制
4. Numerical Study of Aerodynamic Performance of Airfoils at Low Angles of Attack by Active Flow Control of Trailing Edge Vortices [C] . American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting and Exhibit . 2006

机译：落后边缘涡流激活流动控制下攻击下翼型空气动力学性能的数值研究
5. Numerical investigations of flow characteristics and aerodynamic parameters of an airfoil with a trailing edge rotary cylinder. [D] . Chan, Preston C. T. 2016

机译：后缘旋转气缸翼型流动特性和空气动力学参数的数值研究。
6. Flow visualization over a thick blunt trailing-edge airfoil with base cavity at low Reynolds numbers using PIV technique [O] . Gholamhossein Taherian, Mahdi Nili-Ahmadabadi, Mohammad Hassan Karimi, -1

机译：使用PIV技术以低雷诺数在具有基本空腔的厚钝尾缘翼型上进行流动可视化
7. Parametric Study of Aerodynamic Performance of an Airfoil with Active Circulation Control using Leading Edge Embedded Cross-Flow Fan [O] . M A Qayyum Q. Mazumder, Vladimir V. Golubev, Snorri Gudmundsson 2019

机译：采用主动循环控制的翼型空气动力性能的参数研究使用前缘嵌入式横流风扇
8. Effect of Trailing Vortices on the Production of Lift on an Airfoil Undergoing a Constant Rate of Change of Angle of Attack [R] . Tupper, K. W. 1983

机译：尾随涡对迎面角度恒定变化率的翼型升力产生的影响

Numerical Study of Aerodynamic Performance of Airfoils at Low Angles of Attack by Active Flow Control of Trailing Edge Vortices

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