液滴膨化和微爆炸模式的临界条件

D. Antonov, P. Strizhak
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引用次数: 0

摘要

复合液滴中的微爆炸效应可以改善燃烧室二次雾化过程的整体特性,提高燃料燃烧的完整性,减少点火延迟,减少人为排放。本工作的目的是对微爆炸模式的临界条件和微爆炸模式进行实验和理论研究。通过改变气体介质温度(473 ~ 1523 K)和大气压力([2]),对复合材料液滴中的微爆炸效应进行了实验研究。研究了气体介质温度、固体颗粒和气泡浓度对液滴破碎时间延迟的影响。采用幻影Miro高速慢动作摄像机,帧率为2000 fps,分辨率为512 × 768像素,记录了液滴的加热、蒸发和破裂特性。在Phantom Camera Control软件中对实验视频片段进行处理,分析它们进入加热区之前的初始液滴大小,并估计它们之间的距离。测量这些参数的系统误差分别不超过0.025和0.05 mm。采用聚©聚/微爆炸[3]模型,研究了聚©聚/微爆炸复合水/燃料滴的建模问题。最新的模型[3]是基于复合液滴一维传热方程的解析解,假设一个球形水子液滴正好位于球形燃料液滴的中心。得到了该方程在液滴表面具有Robin边界条件的解析解,并将其实现为数值代码,用于计算的每个时间步。利用Abramzon和Sirignano模型,考虑了热膨胀和蒸发的影响。所开发的数学装置可以帮助开发与液体和泥浆燃料点火和燃烧有关的高温气体蒸气降技术。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
CRITICAL CONDITIONS OF DROPLET PUFFING AND MICROEXPLOSION MODES
Microexplosion e¨ects in composite droplets make it possible to improve integral characteristics of secondary atomization processes in the combustion chamber, to increase completeness of fuel combustion, to reduce ignition time delay, and to diminish anthropogenic emissions [1]. The purpose of this work is experimental and theoretical research of critical conditions of pu©ng and microexplosion modes. The experimental research of microexplosion e¨ects in composite droplets was carried out by varying the temperature of the gaseous medium (473 1523 K) and atmospheric pressure [2]. The in§uence of the gaseous medium temperature and solid particles and gas bubbles concentrations on the time delay of droplets fragmentation were investigated. The droplet heating, evaporation, and breakup characteristics were recorded using a Phantom Miro high-speed slow-motion video camera with a frame rate of 2000 fps at 512 × 768-pixel resolution. The experimental video fragments were processed in the Phantom Camera Control software to analyze the initial droplet size before they enter the heating zone and to estimate the distance between them. The systematic errors in the measurement of these parameters did not exceed 0.025 and 0.05 mm, respectively. The problem of modeling pu©ng/microexplosion of composite water/fuel droplets was examined with using model for pu©ng/ microexplosions [3]. The most recent model [3] is based on the analytical solution to the one-dimensional heat transfer equation in a composite droplet assuming that a spherical water subdroplet is placed exactly in the center of a spherical fuel droplet. The analytical solution to this equation with the Robin boundary condition at the droplet surface was obtained, implemented into the numerical code, and used at each time step of the calculations. The e¨ects of thermal swelling and evaporation, using the Abramzon and Sirignano model, are considered. The developed mathematical apparatus can be helpful in developing high-temperature gas vapor drop technologies associated with ignition and combustion of liquid and slurry fuels.
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