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超声速反向混合实验及其压力温度测量
引用本文:邢小月,陈宏,林建民,俞鸿儒.超声速反向混合实验及其压力温度测量[J].实验流体力学,2003,17(3):31-35.
作者姓名:邢小月  陈宏  林建民  俞鸿儒
作者单位:中国科学院力学研究所高温气体动力学研究开放实验室,北京,100080
基金项目:国家自然科学基金(19632002)
摘    要:对超声速反向射流混合加热方案进行实验验证。实验结果表明:控制向燃烧室注入水雾的流量可以方便地调节燃烧室的温度和压力;用双路氢氧进气系统易于实现稳定的点火和燃烧。用热电偶测量混合前后的流场温度分布的初步结果表明,反向射流混合方案基本可行。

关 键 词:裂解  氢氧燃烧  激波  超声速混合
文章编号:1007-3124(2003)03-0031-05
修稿时间:2002年6月24日

Temperature and pressure measurements in the supersonic counter flow mixing
XING Xiao-yue,CHEN Hong,LIN Jian-min,YU Hong-ru.Temperature and pressure measurements in the supersonic counter flow mixing[J].Experiments and Measur in Fluid Mechanics,2003,17(3):31-35.
Authors:XING Xiao-yue  CHEN Hong  LIN Jian-min  YU Hong-ru
Abstract:The heating scheme by supersonic counter flow mixing has been tested. The experimental results show that the temperature and pressure in a combustion chamber can be adjusted conveniently by controlling the rate of water flow sprayed in it and the ignition and stable flame of oxyhydrogen mixture can be easily realized by using double oxygen and hydrogen supply. The temperature distributions of the flow field measured by two-platinum lawrencium thermocouple certify that the heating scheme by counter flow mixing is basically feasible.
Keywords:pyrolysis  oxyhydrogen combustion  shock waves  supersonic mixing
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