Local vibrations and lift performance of low Reynolds number airfoil

机译：低雷诺数翼型的局部振动和升力性能

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TariqAmin Khan; Wei Li; Jiazhong Zhang; Tom I-P. Shih;
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1. Local vibrations and lift performance of low Reynolds number airfoil [J] . TariqAmin Khan, Wei Li, Jiazhong Zhang, Propulsion and Power Research . 2017,第2期

机译：低雷诺数翼型的局部振动和升力性能
2. Aerodynamic Performance of a Very High Lift Low Pressure Turbine Airfoil (T106C) at Low Reynolds and High Mach Number With Effect of Free Stream Turbulence Intensity [J] . Jan Michalek, Michelangelo Monaldi, Tony Arts Journal of turbomachinery . 2012,第6期

机译：低雷诺数和高马赫数的高升程低压涡轮机翼型（T106C）的气动性能受自由流湍流强度的影响
3. Effects of local oscillation of airfoil surface on lift enhancement at low Reynolds number [J] . Kang Wei, Lei Pengfei, Zhang Jiazhong, Journal of Fluids and Structures . 2015,第Null期

机译：低雷诺数时机翼表面局部振荡对升力的影响
4. AERODYNAMIC PERFORMANCE OF A VERY HIGH LIFT LOW PRESSURETURBINE AIRFOIL (T106C) AT LOW REYNOLDS AND HIGH MACH NUMBER WITHEFFECT OF FREE STREAM TURBULENCE INTENSITY [C] . Jan Michalek, Michelangelo Monaldi, Tony Arts ASME turbo expo . 2011

机译：在低雷诺数和高马赫数下，非常高升程低压涡轮机翼型（T106C）的气动性能，具有自由流湍流强度
5. The Use of Separation Induced Laminar to Turbulent Flow Transition to Improve the Performance and Robustness of Low Reynolds Numbers Airfoils and Wings [D] . Di Luca, Matteo. 2021

机译：使用分离诱导的层流到湍流过渡，提高低雷诺数翼型和翼的性能和鲁棒性
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. Numerical Simulation of the Wake Structure and Thrust/Lift Generation of a Pitching Airfoil at Low Reynolds number via an Immersed Boundary Method [O] . Ali Akbar Hosseinjani, Ali Ashrafizadeh 2015

机译：通过浸没边界法在低雷诺数下倾斜翼型的唤醒结构的数值模拟及俯仰翼型
8. Design and test of a natural laminar flow/large Reynolds number airfoil with a high design cruise lift coefficient [R] . Kolesar, C. E. 1987

机译：设计和测试具有高设计巡航升力系数的自然层流/大雷诺数翼型

Local vibrations and lift performance of low Reynolds number airfoil

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