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A theoretical method for solving shock relations coupled with chemical equilibrium and its applications 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:  Zhang, Zijian;  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Chemical equilibrium  Detonation  Dissociated air  Shock relation  Theoretical solution  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download：301/68  |  Submit date：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
Authors:  Peng, Di;  Liu, Xu;  Jiao, Lingrui;  Li, Ziyan;  Wen, Xin;  Yuan CK(苑朝凯);  Han GL(韩桂来);  Liu YF(刘云峰);  Liu, Yingzheng;  Jiang ZL(姜宗林)
Adobe PDF(3477Kb)  |  Favorite  |  View/Download：288/59  |  Submit date：2021/03/30
Temperature-sensitive paint  Time-resolved measurement  Hypersonic flow  Background radiation  
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
Authors:  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)  |  Favorite  |  View/Download：285/102  |  Submit date：2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:  Yuan CK(苑朝凯);  Zhou K(周凯);  Liu YF(刘云峰);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1468Kb)  |  Favorite  |  View/Download：368/110  |  Submit date：2019/04/11
Spectral measurement  Hypervelocity flow  Radiation  Expansion tunnel  
Theoretical analysis on deflagration-to-detonation transition 期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 8, 页码: 84703
Authors:  Liu YF(刘云峰);  Shen H(沈还);  Zhang DL(张德良);  Jiang ZL(姜宗林)
View  |  Adobe PDF(699Kb)  |  Favorite  |  View/Download：414/87  |  Submit date：2018/10/30
deflagration  detonation  deflagration-to-detonation transition  
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
Authors:  姜宗林;  李进平;  胡宗民;  刘云峰;  俞鸿儒
View  |  Adobe PDF(634Kb)  |  Favorite  |  View/Download：488/77  |  Submit date：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  
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1080Kb)  |  Favorite  |  View/Download：536/135  |  Submit date：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
气相爆轰波胞格尺度与点火延迟时间关系研究 期刊论文
力学学报, 2014, 卷号: 46, 期号: 6, 页码: 977-981
Authors:  张薇;  刘云峰;  姜宗林
View  |  Adobe PDF(1345Kb)  |  Favorite  |  View/Download：764/216  |  Submit date：2015/01/19
爆轰波  胞格  点火延迟时间  化学反应模型  
长试验时间爆轰驱动激波风洞技术研究 期刊论文
力学学报, 2012, 卷号: 44, 期号: 5, 页码: 824-831
Authors:  姜宗林;  李进平;  赵伟;  刘云峰;  俞鸿儒
Adobe PDF(2350Kb)  |  Favorite  |  View/Download：1680/358  |  Submit date：2013/01/16
高超声速飞行  反向爆轰驱动激波风洞  长试验时间  高温气体流动