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On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
作者:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:249/101  |  提交时间:2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Experimental investigation of liquid film cooling in hypersonic flow 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10
作者:  Yuan CK(苑朝凯);  Li JP(李进平);  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
浏览  |  Adobe PDF(4383Kb)  |  收藏  |  浏览/下载:436/126  |  提交时间:2019/06/10
Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
浏览  |  Adobe PDF(523Kb)  |  收藏  |  浏览/下载:461/52  |  提交时间:2020/01/06
高超声速飞行复现风洞理论与方法 期刊论文
力学学报, 2018, 卷号: 50, 期号: 6, 页码: 1283-1291
作者:  姜宗林;  李进平;  胡宗民;  刘云峰;  俞鸿儒
浏览  |  Adobe PDF(634Kb)  |  收藏  |  浏览/下载:456/72  |  提交时间:2019/01/09
高超声速  激波风洞  复现飞行条件  爆轰驱动  缝合条件  
Theories and technologies for duplicating hypersonic flight conditions for ground testing 期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.;  Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
浏览  |  Adobe PDF(1315Kb)  |  收藏  |  浏览/下载:336/128  |  提交时间:2017/11/29
Development and calibration of detonation-driven high-enthalpy and hypersonic test facilities 图书章节
2016
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
浏览  |  Adobe PDF(883Kb)  |  收藏  |  浏览/下载:219/38  |  提交时间:2018/11/06
Development of the advanced high-enthalpy test facility for hypersonic vehicles 会议论文
The 29th International Symposium on Rarefied Gas Dynamics, 中国陕西西安, 2014-07-13
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
浏览  |  Adobe PDF(67Kb)  |  收藏  |  浏览/下载:240/71  |  提交时间:2015/09/10
Enthalpy  Facility  Challenging  Capable  Aerospace  Promoting  Detonation  Viewing  Facilities  Tunnel  
A chemical shock tube driven by detonation 期刊论文
Shock Waves, 2012, 卷号: 22, 期号: 4, 页码: 351-362
作者:  Li JP(李进平);  Chen H(陈宏);  Yu HR(俞鸿儒);  Li, J;  Chinese Acad Sci, Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(848Kb)  |  收藏  |  浏览/下载:798/266  |  提交时间:2013/01/18
Shock Tube  Detonation Driver  Chemical Kinetics Study  
高超声速激波风洞研究进展 期刊论文
力学进展, 2009, 卷号: 39, 期号: 6, 页码: 766-776
作者:  姜宗林;  俞鸿儒
Adobe PDF(2137Kb)  |  收藏  |  浏览/下载:797/183  |  提交时间:2010/05/03
高焓激波风洞  超高速度流动  轻气体驱动器  自由活塞驱动器  反向爆轰驱动  正向爆轰驱动  双爆轰驱动  气动热力学  近空间飞行器  
Research progress on high-enthalpy and hypersonic flows 会议论文
5th International Conference on Fluid Mechanics, Shanghai, PEOPLES R CHINA, AUG 15-19, 2007
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Lin ZB(林贞彬);  Jiang Z
Adobe PDF(690Kb)  |  收藏  |  浏览/下载:875/238  |  提交时间:2009/07/23
Hypersonic Flows  Detonation Driver  Shock-reflected Tunnels  Shock-expanded Tube  Heat Transfer