IMECH-IR  > 高温气体动力学国家重点实验室
高温低密度激波管
王苏
Classification研制
2016
Abstract用于开展强激波结构、高温平衡和非平衡辐射、气体电离过程与等离子体电磁波传输特性、再入流场的光电特性、高焓驻点传热等方面的研究,主要技术指标: 高压驱动段长1.6m,低压试验段长17m,采用氢氧燃烧驱动运行。激波管初始压力P1=0.1-100Pa,激波运行马赫数Ms=8-23,可以模拟距地面30-80km高度的飞行环境。以空气为工作物质时,入射激波后2区温度T2:2800-6000K,电子密度在1×1010/cm3-2×1013/cm3范围内;反射激波后五区温度T5:4200-12000K,电子密度最高可达1×1015 /cm3。
Contact010-82544018
URL查看原文
Document Type仪器设备
Identifierhttp://dspace.imech.ac.cn/handle/311007/79586
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
王苏. 高温低密度激波管(研制), 2016.
Files in This Item: Download All
File Name/Size DocType Version Access License
s028.jpg(52KB)仪器设备 开放获取MIT LicenseThumbnail
View Download
Related Services
Recommend this item
Bookmark
Usage statistics
Export to Endnote
Google Scholar
Similar articles in Google Scholar
[王苏]'s Articles
Baidu academic
Similar articles in Baidu academic
[王苏]'s Articles
Bing Scholar
Similar articles in Bing Scholar
[王苏]'s Articles
Terms of Use
No data!
Social Bookmark/Share
File name: s028.jpg
Format: JPEG
All comments (0)
No comment.
 

Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.