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高超声速吸气发动机燃气模拟装置
Authors
俞鸿儒
单希壮
+5 more
吴松
李斌
李进平
董志成
陈宏
Publication date
1 January 2008
Publisher
中国力学学会
Abstract
本文阐述了用于提高冲压发动机在高马赫数飞行条件下的推力,而发展的简单可靠的催化复合效应实验研究所需要高温燃气的产生方法;进行了理论分析与数值计算:成功研制了一座能产生高温空气与气态燃料燃烧产物的高温燃气激波风洞实验装置,并得到了压力为20大气压,温度为3200K,定常实验时间约为17ms且状态参数稳定的实验结果
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Institute Of Mechanics,Chinese Academy of Sciences
See this paper in CORE
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oai:dspace.imech.ac.cn:311007/...
Last time updated on 12/02/2018
Institute Of Mechanics,Chinese Academy of Sciences
See this paper in CORE
Go to the repository landing page
Download from data provider
oai:dspace.imech.ac.cn:311007/...
Last time updated on 12/02/2018