IMECH-IR  > 力学所知识产出(1956-2008)
应用于固体火箭发动机喷管出口羽流温度测量的光学辐射高温计
Alternative TitleAn Optical High Temperature Thermometer for Plume Measurement of Solid Propellant Rocket Motor
余西龙; 郭颜红; 门们; 周建军; 杨乾锁
Source Publication导弹与航天运载技术
2008-04-10
Issue2Pages:53-55
ISSN1004-7182
Abstract利用辐射光谱测量温度的原理,设计并制造了一种新型的非接触式光学辐射高温计.详细介绍该温度计的基本原理和标定方法,并将该温度计应用于火箭发动机喷管出口羽流的温度测量中,初步的实验结果和数值模拟结果相一致.
Keyword红外辐射 温度测量 火箭发动机
Indexed ByCSCD
Language中文
CSCD IDCSCD:3252822
Citation statistics
Cited Times:1[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/41368
Collection力学所知识产出(1956-2008)
Corresponding Author余西龙
Recommended Citation
GB/T 7714
余西龙,郭颜红,门们,等. 应用于固体火箭发动机喷管出口羽流温度测量的光学辐射高温计[J]. 导弹与航天运载技术,2008,2,:53-55.
APA 余西龙,郭颜红,门们,周建军,&杨乾锁.(2008).应用于固体火箭发动机喷管出口羽流温度测量的光学辐射高温计.导弹与航天运载技术(2),53-55.
MLA 余西龙,et al."应用于固体火箭发动机喷管出口羽流温度测量的光学辐射高温计".导弹与航天运载技术 .2(2008):53-55.
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