一定空化数范围内叶顶涡的结构

H. Higuchi, R. Arndt, V. Arakeri, J. Killen
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引用次数: 1

摘要

对椭圆翼的叶尖涡卷起过程进行了实验研究。空化现象为旋涡卷起机理的可视化提供了一种很好的方法。用激光多普勒测速仪首次获得了非空化涡的速度分布。讨论了速度分布的测量不对称性和涡核内压力分布的计算结果。在空化充分发展的情况下,对涡旋轨迹进行了分析,并与理论进行了比较。空腔芯半径随着压力的减小而增大,直至形成扭曲的带状结构。讨论了这些结构的芯厚和波长。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Structure of Tip Vortices Over a Range of Cavitation Number
The tip vortex roll-up process from an elliptic wing was experimentally investigated. Cavitation provided an excellent method for visualizing the mechanism of vortex roll-up. The velocity profiles of the non-cavitating vortex were first obtained with a laser Doppler velocimeter. The measured asymmetry of the velocity profile and the computed pressure distribution in the vortex core are discussed. In the case of fully developed cavitation, the vortex trajectory was analyzed and compared with theory. The cavity core radius increased with reduced pressure until the developed cavity forms a twisted ribbon structure. The core thickness and the wave length of these structures are also discussed.
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