翼板交界湍流非定常的高效吸力控制

IF 3.4 3区 工程技术 Q1 MECHANICS 水动力学研究与进展:英文版 Pub Date : 2017-04-01 DOI:10.1016/S1001-6058(16)60745-X
Jian-hua Liu (刘建华), Chang-you Song (宋长友)
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引用次数: 1

摘要

水下航行体翼身结合部流被认为是水下航行体辐射噪声的一个重要来源,引起了人们的广泛关注。本文采用烟丝流可视化和时间分辨PIV测量技术,对低速风洞中翼板结合部的流动进行了实验研究。为了揭示这种流动的物理行为,对层流翼板连接处进行了烟丝流动可视化。提出了一种新的控制策略,以精确定位流线即将卷起形成涡流的吸入口。从时均流场和瞬时流场两方面讨论了控制效果。
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Efficient suction control of unsteadiness of turbulent wing-plate junction flows

A wing-body junction flow of a navigating underwater vehicle is considered to be a crucial source of the flow radiating acoustic noise, which attracts much research interest. In this paper, wing-plate junction flows are experimentally investigated in a low-speed wind tunnel by smoke-wire flow visualizations and time-resolved PIV measurements. To reveal the physical behavior of such flows, smoke-wire flow visualizations are conducted for a laminar wing-plate junction. A novel control strategy is proposed, to accurately locate the suction openings where the streamline is about to roll up to form a vortex in the turbulent junction flows. The control effect is discussed in perspectives of both the time-averaged and instantaneous flow fields.

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CiteScore
5.90
自引率
0.00%
发文量
1240
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