翼尖涡漂移补偿常用涡心检测准则评估

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-05-01 Epub Date: 2025-02-15 DOI:10.1016/j.ast.2025.110069
Zhiyuan Wang , Chong Pan , Zepeng Cheng
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引用次数: 0

摘要

涡旋漂移的特征是涡旋核心位置的低频位移,严重影响了涡旋统计的定量化。为了减轻这种影响,重新定心校正是粒子图像测速(PIV)测量速度场数据集的后处理常用方法。该方法的关键问题之一是如何精确地检测瞬时涡中心。本文对常用的八种涡旋中心检测准则进行了实证评价,旨在寻找最实用的涡旋漂移补偿准则。利用时间分辨立体PIV测量的孤立涡或反旋转涡对近尾迹和中尾迹区域的横流速度场,采用不同的涡心检测准则进行重新定心校正后处理,分为基于速度的局部方法和基于速度梯度的非局部方法。得到的瞬时涡中心和涡动统计,包括平均速度分布和湍流统计,进行了详细的比较。结果表明,伪循环准则是一种基于速度的非局部方法,其性能优于其他所有测试准则。利用伪环流判据将瞬时速度场分解为平均分量、大尺度运动和小尺度湍流波动三分量,可以有效地将旋涡漂移的伪波动从小尺度湍流波动中剥离出来,得到最紧凑的涡廓线,涡核区小尺度湍流动能和雷诺数剪应力最低。这一进展使其成为研究翼尖旋涡不稳定性或与旋涡徘徊运动相关的能量传递特性的理想涡心检测准则。
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Assessment of prevalent vortex-center detection criteria for the compensation of wandering motion of wingtip vortices
Vortex wandering, characterized as low-frequency displacements of vortex core locations, significantly affects the quantification of vortex statistics. To mitigate this impact, re-centering correction is a commonly employed method for post-processing velocity-field datasets being measured by particle image velocimetry (PIV). One of the key problems in this method is how to precisely detect instantaneous vortex centers. In this paper, eight prevalent vortex-center detection criteria are empirically evaluated, with the purpose of finding the most practical criterion for the compensation of vortex wandering. Cross-stream velocity fields in the near-wake and middle-wake regions of either an isolated vortex or a counter-rotating vortex pair, being measured by time-resolved stereoscopic PIV, are post-processed by re-centering correction with various vortex-center detection criteria, which are categorized as local or non-local methods with velocity-based or velocity-gradient-based measures. The yielded instantaneous vortex centers and vortex kinematical statistics, including mean velocity profiles and turbulent statistics, are compared in detail. It is found that the pseudo-circulation criterion, which is a velocity-based non-local method, outperforms all the other tested criteria. Once applying the pseudo-circulation criterion to decompose the instantaneous velocity field into triple components, i.e., mean component, large-scale motion and small-scale turbulent fluctuation, the pseudo-fluctuation from vortex wandering can be effectively peeled off from small-scale turbulent fluctuation, resulting in the most compact vortex profile, as well as the lowest level of small-scale turbulent kinetic energy and Reynolds shear stress in the vortex core region. Such an advance makes it an ideal vortex-center detection criterion to study either wingtip vortex instability or energy transfer characteristics associated with the vortex wandering motion.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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