Shen Junwei, Wang Hongbo, Zhang Cheng, Zhang Yuning, Zhang Yuning
Key Laboratory of Power Station Energy Transfer Conversion and System (Ministry of Education), School of Energy Power and Mechanical Engineering, North China Electric Power University, Beijing 102206, China.
Key Laboratory of Power Station Energy Transfer Conversion and System (Ministry of Education), School of Energy Power and Mechanical Engineering, North China Electric Power University, Beijing 102206, China.
Ultrason Sonochem. 2025 Jan;112:107174. doi: 10.1016/j.ultsonch.2024.107174. Epub 2024 Nov 24.
The present paper investigates the bubble collapse dynamics near hydrofoils within a confined space. Experiments involving high-speed photography reveal in detail the typical bubble morphological evolution near different hydrofoils between two glass plates (namely the confined space), and the partitioning of the thickness-related and camber-related parameters is analyzed quantitatively. Based on conformal transformation, the liquid velocity field and Kelvin impulse are used to analyze the bubble collapse characteristics qualitatively and quantitatively, including the bubble interface motion, cross-sectional roundness, and collapse jet. The main conclusions are summarized as follows. (1) The bubble morphological evolution near the hydrofoils can be categorized into five typical collapse shapes, and their partition ranges are significantly affected by the thickness-related and camber-related parameters. (2) The thickness-related hydrofoil parameter positively correlated with the bubble interface motion and cross-sectional roundness, while the camber-related parameter is inversely correlated with them. (3) High-velocity regions between the bubble and the hydrofoil head and tail endpoints explain the bubble interface depressions observed in the experiments.
本文研究了受限空间内水翼附近的气泡坍塌动力学。涉及高速摄影的实验详细揭示了两块玻璃板(即受限空间)之间不同水翼附近典型的气泡形态演变,并对与厚度相关和与弯度相关的参数划分进行了定量分析。基于共形变换,利用液体速度场和开尔文冲量对气泡坍塌特性进行定性和定量分析,包括气泡界面运动、横截面圆度和坍塌射流。主要结论总结如下:(1)水翼附近的气泡形态演变可分为五种典型的坍塌形状,其划分范围受与厚度相关和与弯度相关的参数显著影响。(2)与厚度相关的水翼参数与气泡界面运动和横截面圆度呈正相关,而与弯度相关的参数与它们呈负相关。(3)气泡与水翼头部和尾部端点之间的高速区域解释了实验中观察到的气泡界面凹陷现象。