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压力对液滴参数激光诱导荧光测量的影响研究

INVESTIGATION ON THE EFFECT OF PRESSURE ON LASER-INDUCED FLUORESCENCE MEASUREMENTS OF LIQUID DROPLET PARAMETERS

  • 摘要: 高超声速飞行器飞行时面临复杂的气象环境, 随着飞行速度的提升, 大气环境中的冰晶粒子对飞行器表面的冲击影响呈指数级增长, 造成飞行器表面侵蚀破坏、飞行性能改变, 进而影响飞行稳定性. 液滴是冰晶粒子的重要存在形态, 深入探究高速气流与液滴的相互作用过程, 能够揭示气液两相耦合作用背后的复杂流动规律, 而通过实验手段精准表征液滴温度、直径等液相关键参数, 更是开展高空低压条件下气液相互作用过程研究的前提与基础. 本研究旨在利用双色激光诱导荧光技术, 建立低压环境下液滴温度和直径的同步测量方法, 为高空低压条件下气/液相互作用研究提供可靠的测量技术支撑. 实验选用温度敏感型Rhodamine B(RhB)和温度相对不敏感型SulfoRhodamine 101(SRh101)两种染料构建单染料和双染料测量体系, 系统研究了染料浓度、激光脉冲能量以及环境压力对荧光光谱响应特性和温度标定关系的影响规律. 通过优化选取两个不同荧光光谱波带建立了单染料与混合染料两种条件下荧光强度比与温度间的定量关系. 此外, 开展了不同温度条件下液滴的二维成像测量实验, 通过图像处理技术获得了液滴二维温度空间分布和直径变化, 系统分析了实验测量偏差及其影响因素. 实验结果表明2c LIF技术可有效应用于低压环境下液滴参数测量.

     

    Abstract: Hypersonic vehicles inevitably encounter extremely intricate and highly variable meteorological conditions during flight. As flight speed increases, the impact of suspended ice crystal particles on the vehicle’s surface structure grows exponentially. T causing severe erosion to thermal protection and structural surfaces, altering aerodynamic performance, and undermining flight stability and maneuverability. Droplets represent one of the most significant and widely distributed forms of ice crystal particles existing in high-altitude atmospheres. In-depth investigation of the dynamic interaction process between high-speed gas flows and micro-droplets can reveal complex flow patterns and underlying physical mechanisms that govern gas-liquid coupling phenomena. Moreover, the accurate and reliable experimental characterization of key droplet parameters—such as transient temperature and spatial diameter distributions—serves as an indispensable prerequisite and fundamental foundation for studying gas-liquid interaction behaviors under high-altitude, low-pressure environmental conditions. This study develops a novel simultaneous measurement method that is specifically designed to characterize critical liquid-phase parameters, particularly droplet temperature and diameter in low-pressure environments, by utilizing the two-color laser-induced fluorescence (2c LIF) technique, thereby providing robust and reliable measurement support for advanced gas-liquid interaction research under high-altitude, low-pressure conditions. Temperature-sensitive Rhodamine B (RhB) and relatively temperature-insensitive SulfoRhodamine 101 (SRh101) fluorescent dyes are carefully and deliberately employed to construct both single-dye and mixed-dye measurement systems with optimized configurations. A thorough and systematic investigation is conducted to evaluate the quantitative influence of key experimental factors, including dye concentration, laser pulse energy, and ambient pressure, on the calibration relationship and fluorescence spectral characteristics of the system. Quantitative linear and nonlinear relationships between the fluorescence intensity ratios and the corresponding droplet temperature are precisely established for each dye configuration by selecting two distinct and non-overlapping spectral bands. Furthermore, high-resolution two-dimensional imaging of micro-droplets under varying temperature conditions is carried out, with advanced image processing techniques applied to extract the detailed spatial distributions of droplet diameter and temperature. Experimental measurement deviations and their primary influencing factors are comprehensively and systematically analyzed. The final experimental findings clearly suggest that the 2c LIF technique enables effectively and accurately facilitates the non-intrusive measurement of multi-parameter droplet characteristics in low-pressure environments.

     

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