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Numerical Simulation of Biology-Inspired Beetle Wings at Various Flying Conditions

机译:不同飞行条件下受生物启发的甲虫翅膀的数值模拟

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Comprehensive numerical studies have been carried out on a biology-inspired computational model of Rhinoceros beetle subjected to changes in flow physics during propelling at different angles of attack. Over a pool of choices, Rhinoceros beetle is selected for its superior ability to function in various media. Detailed analyses have been carried out using a three dimensional pressure based SST k-ω turbulence model with the biomimetic structure. Numerical simulations have been carried out using refined polyhedral mesh with different lateral and longitudinal tilts at a free stream velocity of 5 m/s. Different flow property contours are generated and each case is compared with various flying conditions of Beetle to find out the best aerodynamic performance for various practical applications. Endurance is appropriated in this paper, through the estimation of the maximum aerodynamic efficiency for different orientations of the beetle wings. Authors ascertained that for every longitudinal angle of attack, there exists a lateral angle of attack at which aerodynamic efficiency becomes high and beyond which efficiency drops. Authors comprehended that the insects possess an innate ability to fix its wings at this critical efficient angle of attack as it changes its longitudinal angle of attack step by step, when it tries to take off. For landing, however, this phenomenon reverses to identify the angle of attack at which the aerodynamic efficiency becomes low. For a particular longitudinal orientation, detailed breakdown flow-physics research is carried out to single out the most aerodynamically efficient lateral angle of attack and to understand the reason behind that particular orientation's successful performance in aerospace that can be mimicked for a Micro Aerial Vehicle (MAV). This study is a pointer toward for the design optimization of MAY for industrial applications.
机译:在犀牛甲虫的生物学启发计算模型上进行了全面的数值研究,该模型在以不同的攻角推进期间在流动物理学中发生变化。在众多选择中,犀牛甲虫因其在各种培养基中发挥出色的功能而被选中。已经使用具有仿生结构的基于三维压力的SSTk-ω湍流模型进行了详细分析。使用自由侧速度为5 m / s的具有不同横向和纵向倾斜度的精制多面网格进行了数值模拟。生成不同的流动特性轮廓,并将每种情况与甲壳虫的各种飞行条件进行比较,以找到适用于各种实际应用的最佳空气动力学性能。通过估计甲虫翼不同方向的最大空气动力学效率,本文采用了耐力性。作者确定,对于每个纵向迎角,都存在一个横向迎角,在该迎角处,空气动力效率变高,而效率下降。作者认为,昆虫在试图起飞时会逐步改变其纵向攻角,因而具有将其翅膀固定在此临界有效攻角上的天生能力。然而,对于着陆,该现象相反以识别出空气动力学效率变低的迎角。对于特定的纵向方向,进行了详细的击穿流物理学研究,以找出在空气动力学上最有效的横向攻角,并了解该特定方向在航空航天中成功表现的原因,而微型航空器(MAV)可以模仿这种方向)。该研究为工业应用MAY的设计优化指明了方向。

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