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超燃冲压发动机燃烧效率测量方法简介
引用本文:潘余,王振国,刘卫东.超燃冲压发动机燃烧效率测量方法简介[J].实验流体力学,2007,21(2):68-73.
作者姓名:潘余  王振国  刘卫东
作者单位:湖南长沙国防科大航天与材料工程学院,长沙,410073
基金项目:国家高技术研究发展计划(863计划)
摘    要:在进行超燃冲压发动机燃烧室性能评估时,燃烧效率是一个非常重要的指标.然而由于燃烧室内高温、高速等复杂条件的影响,很难对燃烧效率进行直接的确定.对常见的气体采样法、红外线法、体积热量法、推力测量法和冲量函数法等基于试验测量的超燃冲压发动机燃烧效率确定方法进行了详细介绍,并对各自的特点进行了对比分析,供进行燃烧效率测量试验参考.

关 键 词:燃烧效率  超燃冲压发动机  超声速燃烧  试验数据分析  燃烧室性能
文章编号:1672-9897(2007)02-0068-06
修稿时间:2006-03-232006-12-30

Introduction of scramjet combustion efficiencies measurement methods
PAN Yu,WANG Zhen-guo,LIU Wei-dong.Introduction of scramjet combustion efficiencies measurement methods[J].Experiments and Measur in Fluid Mechanics,2007,21(2):68-73.
Authors:PAN Yu  WANG Zhen-guo  LIU Wei-dong
Institution:Aeronautic and Material Institute of National Defense Technology University, Changsha 410073, China
Abstract:The combustion efficiency was a critical parameter for scramjet combustor performance evaluation.But restricted by the high speed and temperature of the complex combustor internal flow,it was very difficult to gain the combustion efficiencies directly.The most frequently used methods of gaining the scramjet combustion efficiency,such as,gas sampling method,infrared measurement method,bulk calorimeter method,force based measurement and impulse function method etc.,were clearly introduced and curtly compared,which can provide instructions and references for related field researchers.
Keywords:combustion efficiency  scramjet  supersonic combustion  post-test analysis  combustor performance
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