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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
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：279/101  |  Submit date：2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478
Authors:  Luo ZT(罗长童);  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Li JP(李进平);  Jiang ZL(姜宗林)
Adobe PDF(2227Kb)  |  Favorite  |  View/Download：289/69  |  Submit date：2019/10/21
Aerodynamic force measurement  Dynamic system  Impact response  Cross-validation  System identification  
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
Authors:  Yuan CK(苑朝凯);  Li JP(李进平);  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
Adobe PDF(4383Kb)  |  Favorite  |  View/Download：460/135  |  Submit date：2019/06/10
Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel 期刊论文
JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381
Authors:  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
Adobe PDF(1208Kb)  |  Favorite  |  View/Download：692/140  |  Submit date：2018/10/30
copper calorimeter  high enthalpy shock tunnel  heat transfer  hypersonic  
高超声速条件下溢流液膜厚度测量方法 期刊论文
中国科学. 技术科学, 2018, 卷号: 48, 期号: 6, 页码: 629-638
Authors:  苑朝凯;  李进平;  陈宏;  姜宗林;  俞鸿儒
Adobe PDF(4824Kb)  |  Favorite  |  View/Download：553/102  |  Submit date：2018/10/24
高超声速热防护  主动冷却  液膜厚度  电导法  
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
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  
高超声速溢流冷却实验研究 期刊论文
力学学报, 2018, 卷号: 50, 期号: 1, 页码: 1-8
Authors:  苑朝凯;  李进平;  陈宏;  姜宗林;  俞鸿儒
Adobe PDF(570Kb)  |  Favorite  |  View/Download：420/98  |  Submit date：2018/10/24
高超声速热防护  主动冷却  溢流冷却  液膜  
Shock relations in gases of heterogeneous thermodynamic properties 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭俊);  Li JP(李进平);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1654Kb)  |  Favorite  |  View/Download：381/97  |  Submit date：2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution  
Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points 期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2017, 卷号: 31, 期号: 2, 页码: 318-323
Authors:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(419Kb)  |  Favorite  |  View/Download：448/117  |  Submit date：2017/10/27
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
Authors:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(763Kb)  |  Favorite  |  View/Download：575/237  |  Submit date：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone