| 一种新运行方式脉冲燃烧风洞研制及初步应用 |
| |
| 引用本文： | 刘伟雄,谭宇,毛雄兵,乐嘉陵.一种新运行方式脉冲燃烧风洞研制及初步应用[J].实验流体力学,2007,21(4):59-64. |
| |
| 作者姓名： | 刘伟雄 谭宇 毛雄兵 乐嘉陵 |
| |
| 作者单位： | 西北工业大学,陕西,西安,710072;中国空气动力研究与发展中心,四川,绵阳,621000 |
| |
| 摘 要： | 介绍了一座喷管口径为600mm、利用氢与富氧空气混合燃烧产生高焓试验气流的脉冲风洞.风洞首次采用了活塞挤压为加热器供应燃料和路德维希管供应富氧空气的工作方式,实现了风洞试验过程中需多少燃料就供多少燃料,消除了采用路德维希管供燃料存在的弊端.自主研制的大通径快速阀取代了膜片,提高了设备运行效率.风洞在吸气式高超声速技术研究中得到了成功应用.
|
| 关 键 词： | 风洞 脉冲燃烧 活塞挤压 快速阀 吸气式高超声速技术 |
| 文章编号： | 1672-9897(2007)04-0059-06 |
| 修稿时间： | 2007年12月10 |
The development and preliminary application of a pulse combustion wind tunnel with new running way |
| |
| LIU Wei-xiong,TAN Yu,MAO Xiong-bing,LE Jia-ling.The development and preliminary application of a pulse combustion wind tunnel with new running way[J].Experiments and Measur in Fluid Mechanics,2007,21(4):59-64. |
| |
| Authors: | LIU Wei-xiong TAN Yu MAO Xiong-bing LE Jia-ling |
| |
| Abstract: | A pulse wind tunnel with nozzle diameter of 600mm is presented in this paper,which uses combustion of hydrogen and rich oxygen to reproduce high enthalpy testing gas.A new running way of utilizing a piston compressor to supply fuel and a Ludwieg tube to supply rich oxygen to the heater is adopted firstly in the wind tunnel,which makes it possible to add exactly needed fuel into the heater in a run and eliminates the disadvantages of supplying fuel with a Ludwieg tube.The running efficiency is enhanced by replacing the diaphragm with a self-developed quick-acting valve.The wind tunnel has been applied successfully to the air-breathing hypersonics researches. |
| |
| Keywords: | wind tunnel pulse combustion piston compressor quick-acting valve air-breathing hypersonics |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《实验流体力学》浏览原始摘要信息 |
| 点击此处可从《实验流体力学》下载免费的PDF全文 |
|
