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Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:  Yuan CK(苑朝凯);  Meng FZ(孟凡钊);  Liu, Xu;  Liu YF(刘云峰);  Lian H(连欢);  Liu, Yingzheng;  Peng, Di
Adobe PDF(3477Kb)  |  Favorite  |  View/Download：52/5  |  Submit date：2023/07/17
Temperature-sensitive paint  Heat flux  Conjugate gradient method  Air-breathing hypersonic vehicle  Inverse heat conduction problem  
Numerical study of periodic flame flashback in a cavity-based scramjet combustor 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 45108
Authors:  Guo SZ(郭升祖);  Zhang X(张旭);  Liu QL(刘起立);  Yue LJ(岳连捷)
Adobe PDF(5835Kb)  |  Favorite  |  View/Download：80/7  |  Submit date：2023/06/15
Optimal design of E-type coaxial thermocouples for transient heat measurements in shock tunnels 期刊论文
APPLIED THERMAL ENGINEERING, 2023, 卷号: 218, 页码: 11
Authors:  Qi L(齐力);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Adobe PDF(5274Kb)  |  Favorite  |  View/Download：198/7  |  Submit date：2022/11/21
Coaxial thermocouples  Lateral heat conduction  Maximum temperature point  Optimal design  Numerical simulation  
Investigation of radial heat conduction with 1D self-consistent model in helicon plasmas 期刊论文
PLASMA SCIENCE & TECHNOLOGY, 2023, 卷号: 25, 期号: 1, 页码: 15
Authors:  Tian, Bin;  Merino, Mario;  Wan, Jie;  Hu Y(胡远);  Cao, Yong
Adobe PDF(1638Kb)  |  Favorite  |  View/Download：114/6  |  Submit date：2022/12/20
helicon discharge  heat conduction  model coupling  plasma transport  
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  Favorite  |  View/Download：407/77  |  Submit date：2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels