论文标题

变形和浮力的推进性能

Propulsive performance of morphing and heaving foil

论文作者

Singh, Pragalbh Dev, Neogi, Ishan, Shah, Vardhan Niral, Joshi, Vaibhav

论文摘要

在鸟类和昆虫的柔性翅膀,水生哺乳动物和鱼类的身体和鳍的柔性翅膀中观察到的生物运动,包括它们变形翅膀/鳍的能力。变形能力在鱼类上游游泳的能力中具有重要意义,而无需花费过多的能量,而鸟类则长时间滑行。将机翼或鳍片简化为箔纸,变形是指箔纸平稳地改变其弯腰的能力,而无需在箔表面上急转弯。这允许精确控制流动分离和涡流脱落。与传统的尾随边缘延伸或襟翼相比,在潜艇和船舶中使用的舵和电梯中使用,变形箔可以更好地控制推力和升力特性。这项研究旨在理解箔的变形以及正弦剧烈运动对推力产生的重要性。使用二维变分稳定的彼得罗夫 - 盖尔金移动网格框架,用于对不可压缩的低雷诺数进行建模,遍布整个箔片。变形运动的特征在于变形的程度,以与初始凹痕的偏差角度测量,以及在铝箔上的启动点,其和弦长度的百分比。研究了箔形变和重锻运动对推进性能的影响。变形的程度从-30度和30度变化,起始点的范围从15%到和弦的50%不等。该研究的雷诺和曲路数量分别为1100和0.2。当前工作的结果可以为增强生物模仿的工程设计铺平道路,并为设计条件提供最佳推力性能的见解。

Biological locomotion, observed in the flexible wings of birds and insects, bodies and fins of aquatic mammals and fishes, consists of their ability to morph the wings/fins. The morphing capability holds significance in the abilities of fishes to swim upstream without spending too much energy and that of birds to glide for extended periods of time. Simplifying the wing or fins to a foil, morphing refers to the ability of the foil to change its camber smoothly, without sharp bends on the foil surface. This allows precise control over flow separation and vortex shedding. Compared to conventional trailing-edge extensions or flaps, used in rudders and elevators in submarines and ships, morphing foils provide better control of thrust and lift characteristics. This study aims at understanding the importance of the morphing of foil combined with a sinusoidal heaving motion on thrust generation. A two-dimensional variational stabilized Petrov-Galerkin moving mesh framework is utilized for modelling the incompressible low Reynolds number flow across the flapping foil. The morphing motion is characterized by the extent of morphing, measured as an angle of deviation from the initial camber, and the point of initiation of morphing on the foil as a percentage of its chord length. The effect of the foil morphing and the heaving motion on the propulsive performance are investigated. The extent of morphing is varied from -30 deg and 30 deg, and the point of initiation ranges from 15% to 50% of the chord. The Reynolds and Strouhal numbers for the study are 1100 and 0.2, respectively. The results from the current work can pave the way for enhanced engineering designs in bio-mimetics and give insights on design conditions for optimal thrust performance.

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