An Experimental Database for the Analysis of Bursting of a Laminar Separation Bubble

IF 1.3 Q2 ENGINEERING, AEROSPACE International Journal of Turbomachinery, Propulsion and Power Pub Date : 2024-01-10 DOI:10.3390/ijtpp9010003
M. Dellacasagrande, D. Lengani, D. Simoni, M. Ubaldi
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Abstract

The bursting phenomenon consists in the switch of a laminar separation bubble from a short to a long configuration. In the former case, reduced effects on profile pressure distribution are typically observed with respect to the attached condition. On the contrary, long bubbles provoke significant variations in the loading coefficient upstream of the separation position, with increased risk of stall of the lifting surfaces. The present work presents an experimental database describing separated boundary layers evolving under different Reynolds numbers, adverse pressure gradients and free-stream turbulence levels. Overall, more than 80 flow conditions were tested concerning short and long bubbles for the characterization of separated flows under turbine-like conditions. Measurements were performed on a flat plate geometry using a fast-response Particle Image Velocimetry (PIV) system. For each flow case, two sets of 6000 flow records were acquired with an acquisition frequency equal to 300 and 1000 Hz. Based on existing criteria for the identification of the bursting phenomenon, the flow cases were clustered in terms of short and long bubble states. Additionally, the kind of instability (i.e., convective or absolute) developing into the separated boundary layer was identified based on flow statistics. The present data captures the existing link between the bursting of a laminar separation bubble and the onset of the absolute instability of the separated shear layer, with stationary vortices forming in the dead air region.
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分析层流分离气泡破裂的实验数据库
爆裂现象包括层流分离气泡从短结构转换为长结构。在前一种情况下,与附着状态相比,对剖面压力分布的影响通常较小。相反,长气泡会导致分离位置上游的加载系数发生显著变化,从而增加升力面失速的风险。本研究提供了一个实验数据库,描述了分离边界层在不同雷诺数、不利压力梯度和自由流湍流水平下的演变情况。总体而言,共测试了 80 多种流动条件,涉及短气泡和长气泡,用于描述涡轮条件下分离流动的特征。测量是在平板上使用快速反应粒子图像测速仪(PIV)系统进行的。针对每种流动情况,分别以 300 赫兹和 1000 赫兹的采集频率采集了两组共 6000 条流动记录。根据现有的爆裂现象识别标准,按照短气泡状态和长气泡状态对流动案例进行了分组。此外,还根据流动统计数据确定了进入分离边界层的不稳定类型(即对流或绝对不稳定)。本数据捕捉到了层流分离气泡破裂与分离剪切层绝对不稳定性开始之间的现有联系,并在死气区形成了静止涡流。
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来源期刊
CiteScore
2.30
自引率
21.40%
发文量
29
审稿时长
11 weeks
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