首页 | 本学科首页   官方微博 | 高级检索  
     

定容燃烧弹实验系统及C7燃料火焰速度测量
引用本文:郑东,钟北京. 定容燃烧弹实验系统及C7燃料火焰速度测量[J]. 航空动力学报, 2017, 32(10): 2364-2370. DOI: 10.13224/j.cnki.jasp.2017.10.008
作者姓名:郑东  钟北京
作者单位:1.清华大学 航天航空学院,北京 100084
基金项目:国家自然科学基金(91441113)
摘    要:设计并搭建了适用于测量高温、高压条件下层流火焰传播速度的定容燃烧弹实验系统。详细介绍了定容燃烧弹实验系统的主要子系统的构成和功能,并阐述实验数据处理方法。测量初始温度为400K、压力为0.1MPa和0.3MPa,C7燃料(甲苯、甲基环己烷、正庚烷)/空气层流火焰传播速度,并与现有文献结果进行了对比。结果表明:该定容燃烧弹实验系统具有较高的可靠性,不仅能够准确测量较高初始温度、不同初始压力条件下燃料/空气的层流火焰传播速度,而且能够拓宽测量火焰传播速度当量比的范围。 

关 键 词:层流火焰传播速度   定容燃烧弹   纹影法   球形火焰   马克斯坦长度
收稿时间:2016-02-22

Experimental system of constant volume combustion bomb and measurement of C7 fuels flame speeds
ZHENG Dong,ZHONG Beijing. Experimental system of constant volume combustion bomb and measurement of C7 fuels flame speeds[J]. Journal of Aerospace Power, 2017, 32(10): 2364-2370. DOI: 10.13224/j.cnki.jasp.2017.10.008
Authors:ZHENG Dong  ZHONG Beijing
Abstract:The experimental system of constant volume combustion bomb for measuring laminar flame speed under the conditions of high temperature and pressure was designed and built.The composition and function of main sub-systems,and the data processing method were introduced in detail.Moreover,at 400 K temperature and 0.1,0.3 MPa pressures the laminar flame speeds of C7 Fuels including toluene/methylcyclohexane/n-heptane were measured,and compared with existing literature results.Results indicate that the experimental system has high reliability.Using this experimental system,laminar flame speeds can be accurately measured at high temperatures and elevated pressures,meanwhile the range of equivalence ratios can be extended.
Keywords:laminar flame propagation speed   constant volume combustion bomb   schlieren method   spherical flame   Markstein length
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号