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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
作者:  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)  |  收藏  |  浏览/下载：44/1  |  提交时间：2023/07/17
Temperature-sensitive paint  Heat flux  Conjugate gradient method  Air-breathing hypersonic vehicle  Inverse heat conduction problem  
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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  收藏  |  浏览/下载：365/69  |  提交时间：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  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载：322/169  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
作者:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
浏览  |  Adobe PDF(2082Kb)  |  收藏  |  浏览/下载：421/189  |  提交时间：2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
基于实验设计方法的高超声速飞机前缘型线优化分析 期刊论文
力学学报, 2016, 卷号: 48, 期号: 2, 页码: 290-299
作者:  胡守超;  崔凯;  李广利;  肖尧;  司徒明
浏览  |  Adobe PDF(1239Kb)  |  收藏  |  浏览/下载：340/63  |  提交时间：2016/12/16
Hypersonic Airplane  Air-breathing Vehicle  Shape Optimization  Parameterization  Uniform Design  
Experimental Demonstration Of A New Concept Of Drag Reduction And Thermal Protection For Hypersonic Vehicles 期刊论文
Acta Mechanica Sinica, 2009, 卷号: 25, 期号: 3, 页码: 417-419
作者:  Jiang ZL(姜宗林);  Liu YF(刘云峰);  Han GL(韩桂来);  Zhao W(赵威);  Jiang ZL
Adobe PDF(226Kb)  |  收藏  |  浏览/下载：884/207  |  提交时间：2009/08/03
Hypersonic Vehicle  Shock-reconstruction  Drag Reduction  Thermal Protection  Spike And Lateral Jets  
Research Progress On Thermal Protection Materials And Structures Of Hypersonic Vehicles 期刊论文
Applied Mathematics and Mechanics (English Edition), 2008, 页码: 51-60
作者:  Yang YZ(杨亚政);  Yang JL;  Fang DN;  Yang, YZ (reprint author), Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Technol, Beijing 100083, Peoples R China.
Adobe PDF(601Kb)  |  收藏  |  浏览/下载：917/359  |  提交时间：2009/08/03
Hypersonic Vehicle  High-temperature  Thermal Protection  High-temperature Ceramics  Carbon/carbon Composites  Oxidation Behavior  Creep-behavior  Carbon  Microstructure  Diboride  Kinetics