基于PIV技术的尾涡探测与涡特性定量评价

F. Albano, F. De Gregorio, A. Ragni
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引用次数: 7

摘要

本文总结了为研究大型商用飞机释放的尾涡的形成、运动和持续而进行的活动。在两个不同的大型拖曳储罐设施中进行了两个不同的实验测试活动,进行了PIV测量。根据第一次调查的经验和科学界的经验,说明了从尾流初始形成阶段到尾流在远尾流区域崩溃的尾流涡特征所采用的解决方案。与采用的技术解决方案、选定的实验设备和改进的测量系统一起,特别注意:数据分析描述、先进PIV算法的重要性和选定的后处理方法,以评估表征涡旋结构的主要震级。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Trailing vortex detection and quantitative evaluation of vortex characteristics by PIV technique
This paper summarises the activities performed in order to investigate the formation, motion and persistence of trailing vortices released by large commercial aircraft. Two different experimental test campaigns were carried out in two different large towing tank facilities performing PIV measurements. The lesson learned by the first investigation and by the experience of the scientific community, the solution adopted in order to characterise the wake vortex by the initial formation phase down to wake collapsing in the far-wake region are illustrated. Together with the adopted technical solution, with the selected experimental facility and with the improved measurement system, a particular care is taken: on the data analysis description, on the importance of advanced PIV algorithms and on the selected postprocessing methods for evaluating the main magnitudes characterising the vortex structures.
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