长径比对轧制和扭转箔的影响

A. N. Zurman-Nasution, B. Ganapathisubramani, G. Weymouth
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引用次数: 3

摘要

扑翼飞行和游泳由于其内在的科学丰富性和对新型机器人系统的适用性而受到越来越多的研究。条带理论通常应用于扑翼,但这种建模只严格适用于无限展弦比(AR)的极限,在这种情况下,几何和运动是有效均匀的。本文比较了条形理论和三维扑翼的流动特性和受力,在改变扑翼AR时保持了相似的滚动和扭转运动学。我们发现有限AR和展向变化运动学的关键影响是产生一个时间周期的展向流动,它稳定了旋涡结构并增强了翼根的动力学。本文提出了一种类似于普朗特有限翼理论的扑翼展弦比修正方法,为今后将条形理论应用于有限展弦比扑翼的分析和设计奠定了基础。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Effects of aspect ratio on rolling and twisting foils
Flapping flight and swimming are increasingly studied both due to their intrinsic scientific richness and their applicability to novel robotic systems. Strip theory is often applied to flapping wings, but such modeling is only rigorously applicable in the limit of infinite aspect ratio (AR) where the geometry and kinematics are effectively uniform. This work compares the flow features and forces of strip theory and three-dimensional flapping foils, maintaining similitude in the rolling and twisting kinematics while varying the foil AR. We find the key influence of finite AR and spanwise varying kinematics is the generation of a time-periodic spanwise flow which stabilizes the vortex structures and enhances the dynamics at the foil root. An aspect-ratio correction for flapping foils is developed analogous to Prandtl finite wing theory, enabling future use of strip theory in analysis and design of finite aspect ratio flapping foils.
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