IMECH-IR  > 力学所知识产出(1956-2008)
高焓风洞中钝体近尾流红外辐射测试技术
Alternative TitleExperimental technique on infrared radiation in wake of blunt cone in high-enthalpy tunnel
杭建; 林贞彬; 郭大华; 林建民; 曾明; 黄德; 葛学真
Source Publication实验流体力学
2005
Volume19Issue:4Pages:69-73
ISSN1672-9897
Abstract介绍在JF-10氢氧爆轰驱动高焓激波风洞中开展再人流场红外辐射测量的实验技术。风洞试验状态的驻室总压为19.6MPa,驻室总温为7920K。实验以球头钝锥体为试验模型,测量其近尾流红外辐射能量通量的横向分布。测量采用插入式锑化铟多元红外成像系统,波段范围为2.27-6.0μm。试验数据呈现明显的规律性。试验结果表明:利用这一测量技术能够提供高焓条件下有较高空间分辨率的、较为准确的红外实验数据。
Keyword氢氧爆轰驱动激波风洞 再入流场 红外辐射 钝体 尾流
Subject Area力学
Indexed ByCSCD
Language中文
CSCD IDCSCD:2168525
Citation statistics
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/15611
Collection力学所知识产出(1956-2008)
Recommended Citation
GB/T 7714
杭建,林贞彬,郭大华,等. 高焓风洞中钝体近尾流红外辐射测试技术[J]. 实验流体力学,2005,19,4,:69-73.
APA 杭建.,林贞彬.,郭大华.,林建民.,曾明.,...&葛学真.(2005).高焓风洞中钝体近尾流红外辐射测试技术.实验流体力学,19(4),69-73.
MLA 杭建,et al."高焓风洞中钝体近尾流红外辐射测试技术".实验流体力学 19.4(2005):69-73.
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