用于遥控车辆(rov)的带有后缘襟翼的仿生襟翼箔

N. P. Mannam, Sanju Kumar N T, Prasanth Kumar Duba, P. Rajalakshmi
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引用次数: 0

摘要

水生游泳生物的高效推进机制可以为开发新的推进方法提供灵感,其性能超过目前asv, auv和rov的推进器和螺旋桨。生态推进的优势与较小的尾流相结合,将有利于船舶的稳定性和操纵性。因此,我们需要提高我们对鱼或海豚游泳流体动力学及其流固相互作用的认识,以开发新的推进方法的基准设计。近年来,用于推进的扑翼翼推进器引起了人们的极大兴趣。auv、asv和rov都可以从这项技术中受益匪浅。在海豚游泳运动学中,扑翼推进器是必不可少的组成部分。本研究旨在更好地了解受起伏运动和俯仰运动影响的扑翼的流体力学和流固相互作用。本文利用二维粒子图像测速(PIV)等流动可视化技术,对尾翼型仿生扑翼推进器进行了实验研究。本文给出了时间平均涡量曲线和瞬时速度曲线。带后缘襟翼的襟翼浸入5 ~ 10cm /s均匀流速的自由流中。当前运行的雷诺数范围为500 ~ 4300。斯特罗哈尔数的范围是0.2到0.3。本文还采用二维数值模拟的方法研究了无尾缘襟翼的扑翼效果。通过模拟尾流结构及其演变,研究了带或不带尾缘襟翼的扑翼旋涡脱落机理,从而确定了推力和推进效率。提出并详细讨论了这两种箔片的涡脱落机理。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Bioinspired Flapping Foil With Trailing Edge Flap For Remotely Operated Vehicles (ROVs)
Highly efficient propulsive mechanisms of aquatic swimming creatures could serve as inspiration for developing new propulsion methods where it exceeds the performance of present-day thrusters and propellers for ASVs, AUVs, and ROVs. The advantages of eco-friendly propulsion combined with a lesser wake could be advantageous for marine vehicles' stability and maneuvering. As a result, we need to improve our knowledge of fish or dolphin swimming hydrodynamics and their fluid-structure interaction to develop benchmark designs for new propulsion methods. Flapping foil thrusters for propulsion has sparked much interest in recent years. AUVs, ASVs, and ROVs vehicles could greatly benefit from this technology. In dolphin swimming kinematics, the flapping foil thruster is an essential component. This research aims to understand better the hydrodynamics and fluid-structure interaction of flapping foils subjected to heaving and pitching motions. In the present study, the bio-inspired flapping foil thrusters fitted with trailing edge flaps are studied experimentally using flow visualization techniques such as 2D particle image velocimetry (PIV). The time average vorticity contours and instantaneous velocity contours are presented in this study. The flapping foils with trailing edge flaps are immersed in a free stream of uniform flow speed varying from 5 to 10 cm/s. The operating Reynold number (Re) range is 500 to 4300. The Strouhal number range is 0.2 to 0.3. This study also investigated the effect of flapping foil without trailing edge flaps using 2D numerical simulations. By simulating the wake structure and its evolution, the present study aims to understand the vortex shedding mechanisms of flapping foil with or without trailing edge flaps, determining thrust and propulsive efficiency. The vortex shedding mechanisms for both the foils are presented and discussed in detail.
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