IMECH-IR  > 高温气体动力学国家重点实验室
高焓激波风洞自由流参数测量的数值重建
Alternative TitleNumerical rebuilding of free stream measurement in the high enthalpy shock tunnel
曾明; 林贞彬; 郭大华; 柳军; 瞿章华
Source Publication空气动力学学报
2009-06-15
Volume27Issue:3Pages:358-362
ISSN0258-1825
Abstract高焓风洞中参数测量本身受到高温非平衡效应影响,单纯依靠实验测量不足以确定详细的风洞自由流参数.本文以JF-10高焓激波风洞为背景,通过喷管-试验段-测量仪模型非平衡流场的连贯计算,开展自由流参数测量的数值重建.在比较分析测量仪模型绕流场的计算结果和实验测量值的基础上,结合喷管流场的数值模拟结果,共同确定高焓风洞的详细自由流参数.
Keyword高焓激波风洞 高超声速喷管 数值重建 非平衡流
Indexed ByCSCD
Language中文
Funding Organization国家自然科学基金资助项目(10672170,10502056)
CSCD IDCSCD:3530796
Citation statistics
Cited Times:3[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/33229
Collection高温气体动力学国家重点实验室
Corresponding Author曾明
Recommended Citation
GB/T 7714
曾明,林贞彬,郭大华,等. 高焓激波风洞自由流参数测量的数值重建[J]. 空气动力学学报,2009,27,3,:358-362.
APA 曾明,林贞彬,郭大华,柳军,&瞿章华.(2009).高焓激波风洞自由流参数测量的数值重建.空气动力学学报,27(3),358-362.
MLA 曾明,et al."高焓激波风洞自由流参数测量的数值重建".空气动力学学报 27.3(2009):358-362.
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