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鼓包诱导斜爆震波的数值研究 期刊论文
推进技术, 2022, 卷号: 43, 期号: 05, 页码: 190-201
Authors:  韩信;  张文硕;  张子健;  刘云峰;  姜宗林
Adobe PDF(3358Kb)  |  Favorite  |  View/Download：247/66  |  Submit date：2022/06/10
斜爆震发动机  鼓包  加速起爆  来流扰动  流动控制  
一维与二维爆轰传播的时空关联特性数值研究 期刊论文
力学学报, 2021, 卷号: 53, 期号: 07, 页码: 2069-2078
Authors:  张文硕;  杨鹏飞;  姜宗林;  刘云峰
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斜爆轰  活塞  时空关联  基元反应模型  
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：295/65  |  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：281/58  |  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：280/102  |  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：361/108  |  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：411/86  |  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：480/75  |  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：532/133  |  Submit date：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
振动激发对高超声速气动力/热影响 期刊论文
力学学报, 2017, 卷号: 49, 期号: 03, 页码: 616-626
Authors:  张子健;  刘云峰;  姜宗林
View  |  Adobe PDF(711Kb)  |  Favorite  |  View/Download：410/86  |  Submit date：2017/12/22
振动激发  气动力/热  边界层  高温气体效应