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超燃冲压发动机电弧加热器试验流场调试
引用本文:刘初平,隆永胜,白菡尘,张绍武,陈德江.超燃冲压发动机电弧加热器试验流场调试[J].实验流体力学,2005,19(4):42-45.
作者姓名:刘初平  隆永胜  白菡尘  张绍武  陈德江
作者单位:1. 国防科技大学航天与材料工程学院,湖南,长沙,410073
2. 中国空气动力研究与发展中心,四川,绵阳,621000
基金项目:国家863-702资助项目(2003AA723072).
摘    要:利用电弧加热器提供超燃冲压发动机地面模拟试验的纯空气流场,需要在前电极与喷管之间由冷气混合室加入冷气以降低电弧加热气体的焓值;为了较为准确地获得流场的总温参数,采用了总温探针对流场总温900-1600K进行了校测,总温的测量值与计算的焓值、流量匹配法计算的总温进行了对比,结果表明:总温越高,测量值与计算值相差越大,在名义总温1600K时达到了450K,笔者分析了产生的原因。

关 键 词:超燃发动机  电弧加热器  流场  流量匹配法
文章编号:1672-9897(2005)04-0042-04
收稿时间:2004-09-16
修稿时间:2005-03-02

A preliminary study of the arc flow field for scramjet research
LIU Chu-ping,LONG Yong-sheng,BAI Han-chen,ZHANG Shao-wu,CHEN De-jiang.A preliminary study of the arc flow field for scramjet research[J].Experiments and Measur in Fluid Mechanics,2005,19(4):42-45.
Authors:LIU Chu-ping  LONG Yong-sheng  BAI Han-chen  ZHANG Shao-wu  CHEN De-jiang
Institution:1. Insititute of Aerospace and Material Engineering, NUDT, Changsha 410073, China; 2. China Aerodynamics Research and Development Center, Mianyang 621000, China
Abstract:The arc air flows with long duration and lower temperature by adding cooling air into the mixing chamber among the front electrode and nozzle is an idea for scramjet research. Temperature measurement probes were used to calibrate the flow field and reasonable results were obtained, though discrepancy between measurements and calculations occurred. The discrepancy became greater up to 450K as the measured temperatures reached 1600K,and the preliminary analysis for the discrepancy is presented in this paper.
Keywords:scramjet  arc heater  flow field
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