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Experimental Study on Effect of Wavelength and Amplitude of Wavy Ground on a NACA 0012 Airfoil

机译:NACA 0012机翼波浪形的波长和振幅影响的实验研究。

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摘要

The effect of wavelength and amplitude of a sinusoidal wavy ground on the aerodynamics and flowfield of a NACA 0012 airfoil at low Reynolds numbers was investigated experimentally. The results show that, regardless of wave length and amplitude, the periodic variation in the sectional lift and pitching moment persisted, and that the smaller wavy ground distance the larger lift and pitching moment became. The pitching moment also had an opposite trend to the lift. The maximum and minimum lift always occurred at wave peak and valley, respectively. The maximum and minimum lift and pitching moment increased drastically with increasing wave amplitude while depended weakly on the wave length. However, the change in the drag force over the wavy ground was found to be nonmonotonic. (c) 2019 American Society of Civil Engineers.
机译:实验研究了正弦波状波的波长和振幅对低雷诺数的NACA 0012翼型的空气动力学和流场的影响。结果表明,无论波长和振幅如何,截面升力和俯仰力矩的周期性变化都持续存在,并且波浪形地面距离越小,升力和俯仰力矩就越大。俯仰力矩也与升力有相反的趋势。最大和最小升力总是分别出现在波浪的波峰和波谷处。最大和最小升力和俯仰力矩随着波幅的增加而急剧增加,而对波长的依赖性很小。但是,发现波浪形地面上的阻力变化是非单调的。 (c)2019美国土木工程师学会。

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  • 来源
    《Journal of aerospace engineering》 |2019年第5期|04019064.1-04019064.8|共8页
  • 作者

    Tremblay-Dionne V.; Lee T.;

  • 作者单位

    McGill Univ, Dept Mech Engn, 817 Sherbrooke St W, Montreal, PQ H3A 2K6, Canada;

    McGill Univ, Dept Mech Engn, 817 Sherbrooke St W, Montreal, PQ H3A 2K6, Canada;

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