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超声速反向混合实验及其压力温度测量
Temperature and pressure measurements in the supersonic counter flow mixing
【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。
【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.
【关键词】 裂解;
氢氧燃烧;
激波;
超声速混合;
【Key words】 pyrolysis; oxyhydrogen combustion; shock waves; supersonic mixing;
【Key words】 pyrolysis; oxyhydrogen combustion; shock waves; supersonic mixing;
【基金】 国家自然科学基金(19632002)
- 【文献出处】 流体力学实验与测量 ,Experiments and Measurements In Fluid Mechanics , 编辑部邮箱 ,2003年03期
- 【分类号】TQ221
- 【被引频次】4
- 【下载频次】76