Simulating Drag and Lift Coefficient Variation of the MI VAWT1 airfoil with Angle of Attack at Low Reynolds Number

Krishpersad Manohar; Rikhi Ramkissoon

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Simulating Drag and Lift Coefficient Variation of the MI VAWT1 airfoil with Angle of Attack at Low Reynolds Number

机译：在低雷诺数下模拟具有迎角的MI VAWT1机翼的阻力系数和升力系数变化

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Due to the complexity of shear layer development over an airfoil surface, measurements of timeresolved fluctuating surface pressure within the separated flow region are difficulty. Modelling the flow characteristics with computer generated simulations is

机译：由于翼型表面上剪切层发展的复杂性，很难在分离的流动区域内测量时间分辨的波动表面压力。使用计算机生成的模拟对流动特性进行建模是

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《International Journal of Engineering Trends and Technology》 |2016年第2期|共页
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Krishpersad Manohar; Rikhi Ramkissoon;
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1. LIFT AND DRAG COEFFICIENTS BEHAVIOR AT LOW REYNOLDS NUMBER IN AN AIRFOIL WITH MINIFLAPS GURNEY SUBMITTED TO A TURBULENT FLOW. PART 2 [J] . J. COLMAN, J. MARANON DI LEO, J. S. DELNERO Latin American Applied Research . 2010,第1期

机译：在翼型中流过的最小翼型盖尼式翼型中，雷诺数较低时，升降系数的行为。第2部分
2. Lift and drag coefficients behavior at low reynolds number in an airfoil with miniflaps gurney submitted to a turbulent flow: Part 2 [J] . Colman J., Mara?ón Di Leo J., Delnero J. S., Latin American Applied Research . 2010,第1期

机译：小型翼型格尼襟翼处于湍流中的翼型在低雷诺数下的升力和阻力系数特性：第2部分
3. LIFT AND DRAG COEFFICIENTS BEHAVIOUR AT LOW REYNOLDS NUMBER IN AN AIRFOIL WITH GURNEY FLAP SUBMITTED TO A TURBULENT FLOW. PART 1 [J] . J. COLMAN, J. MARANON DI LEO, J. S. DELNERO Latin American Applied Research . 2008,第3期

机译：翼型中带有低雷诺数的起升系数和举升系数行为，且格尼襟翼呈湍流状态。第1部分
4. EXPERIMENTAL ANALYSIS OF A NACA 0021 AIRFOIL UNDER DYNAMIC ANGLE OF ATTACK VARIATION AND LOW REYNOLDS NUMBERS [C] . D. Hoist, B. Church, F. Wegner, ASME turbo expo: turbomachinery technical conference and exposition . 2018

机译：动态变化角度和低雷诺数下的NACA 0021机翼的实验分析
5. Modeling and analysis of NACA 4412 airfoil to increase lift and to optimize the lift-to-drag ratio. [D] . Mustafa, Ali. 2009

机译：对NACA 4412机翼进行建模和分析，以增加升力并优化升阻比。
6. Flexible Flaps Inspired by Avian Feathers Can Enhance Aerodynamic Robustness in low Reynolds Number Airfoils [O] . Yuta Murayama, Toshiyuki Nakata, Hao Liu 2021

机译：灵活的襟翼灵感来自禽羽毛可以增强低雷诺数翼型的空气动力学鲁棒性
7. Experimental Analysis of a NACA 0021 Airfoil Under Dynamic Angle of Attack Variation and Low Reynolds Numbers [O] . D. Holst, B. Church, F. Wegner, 2018

机译：在攻击变化动态角度下Naca 0021翼型的实验分析和低雷诺数
8. Investigation of the variation of lift coefficient with Reynolds number at a moderate angle of attack on a low-drag airfoil [R] . Tetervin, Neal 1942

机译：低阻力翼型中等迎角雷诺数随升力系数变化的研究

Simulating Drag and Lift Coefficient Variation of the MI VAWT1 airfoil with Angle of Attack at Low Reynolds Number

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