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The Effect of Steady and Pulsed Air Jet Vortex Generator Blowing on an Airfoil Section Model Undergoing Sinusoidal Pitching

机译：稳定脉冲喷射涡流发电机吹对翼型剖面模型的影响

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Simon Prince; Richard Green; Frank Coton; Yaxing Wang;
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1. The Effect of Steady and Pulsed Air Jet Vortex Generator Blowing on an Airfoil Section Model Undergoing Sinusoidal Pitching [J] . Prince Simon, Green Richard, Coton Frank, Journal of the American Helicopter Society . 2019,第3期

机译：稳定和脉冲空气涡流发生器吹气对正弦变桨的翼型截面模型的影响
2. Separation control on high lift low-pressure turbine airfoils using pulsed vortex generator jets [J] . Ralph J. Volino, Mounir B. Ibrahim Applied thermal engineering: Design, processes, equipment, economics . 2012,第Null期

机译：利用脉冲涡发生器射流控制高升程低压涡轮机翼的分离
3. Separation Control on a Very High Lift Low Pressure Turbine Airfoil Using Pulsed Vortex Generator Jets [J] . Ralph J. Volino, Olga Kartuzova, Mounir B. Ibrahim Journal of turbomachinery . 2011,第4期

机译：使用脉冲涡流发生器喷嘴对超高升程低压涡轮机翼型进行分离控制
4. COMBINED EFFECTS OF WAKES AND PULSED VORTEX GENERATOR JET FLOW CONTROL ON BOUNDARY LAYER SEPARATION ON A VERY HIGH LIFT LOW PRESSURE TURBINE AIRFOIL [C] . Ralph J. Volino ASME turbo expo . 2012

机译：尾流和脉动涡流发生器射流控制对极高升压低压涡轮机翼型边界层分离的综合影响
5. Analytical and computational investigations of airfoils undergoing high-frequency sinusoidal pitch and plunge motions at low Reynolds numbers [D] . McGowan, Gregory Z. 2008

机译：在低雷诺数下进行高频正弦俯仰和跳入运动的机翼的分析和计算研究
6. Dataset on tip vortex formation noise produced by wall-mounted finite airfoils with sinusoidal and porous tip geometries [O] . Tingyi Zhang, Danielle Moreau, Thomas Geyer, 2020

机译：具有正弦形和多孔尖端几何形状的壁装有限翼型产生的尖端涡旋形成噪声数据集
7. Separation Control on High Lift Low-Pressure Turbine Airfoils Using Pulsed Vortex Generator Jets [O] . Ralph J. Volino, Mounir B. Ibrahim 2012

机译：脉冲涡流发生器对高扬程低压涡轮翼型的分离控制
8. Experimental investigation of the effect of vortex generators on the aerodynamic characteristics of a NACA 0021 airfoil undergoing large amplitude pitch oscillations. [R] . M. L. Rueger G. M. Gregorek 1991

机译：涡流发生器对经历大幅度俯仰振荡的NaCa 0021翼型气动特性影响的实验研究。

The Effect of Steady and Pulsed Air Jet Vortex Generator Blowing on an Airfoil Section Model Undergoing Sinusoidal Pitching

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