High-speed measurement of thickness of a water film formed by a jet obliquely impinging onto a plate using an LED-induced fluorescence method

被引:5
|
作者
Zhang, Hongzhou [1 ,2 ]
Huang, Yong [1 ,2 ]
Yuan, Weiwei [1 ,2 ]
Li, Lu [1 ,2 ]
机构
[1] Beihang Univ, Collaborat Innovat Ctr Adv Aeroengine, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengine Aerothermody, Beijing 100191, Peoples R China
关键词
Film thickness; LED-induced fluorescence; Liquid films; High-speed measurement; Plate impingement jet; LASER-INDUCED FLUORESCENCE; LIQUID-FILM; PLIF MEASUREMENTS; HYDRAULIC JUMPS; HEAT-TRANSFER; FLOW; IMPINGEMENT; PREDICTION; MODEL;
D O I
10.1016/j.cja.2023.07.0391000-9361
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A transient thickness distribution measured with a high temporal resolution is elemental for exploring the flow characteristics and mechanism of a liquid film formed by an impinging jet. Therefore, this paper develops a high-speed Light-Emitting Diode-Induced Fluorescence (LEDIF) system based on the brightness measured directly above the liquid film. An Ultraviolet (UV) LED lamp is used to provide sufficient and continuous excitation light. Then, a system performance analysis proves that the system can continuously measure the global film thickness at a high acquisition frequency of 5000 Hz when the dye concentration is 200 mg/L. The influence of the irregularity of the excitation intensity, including the spatial non-uniformity, temporal instability, and long-term instability, on the measurement uncertainty is analyzed in detail. The analysis indicates that the system has an acceptable uncertainty of 10%. Compared with theoretical results, experimental results verify that the LEDIF system can accurately measure the global thickness of a liquid film formed by a water jet obliquely impinging onto a plate. An experimental investigation of the radial section of the raised zone demonstrates that the radial section changes from a sewing needle to an oval when the azimuth angle increases from 10 degrees to 90 degrees. Meanwhile, the dynamic contact angle exponentially decreases from 41.4 degrees to 30.1 degrees. A dynamic analysis of surface waves shows that the measured wave velocity decreases from 12 m/s to 1 m/s and the dominant frequency decreases from 1000 Hz to 10 Hz along the flow direction. (c) 2023 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).
引用
收藏
页码:185 / 201
页数:17
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