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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./通讯作者:Peng, D (corresponding author), Shanghai Jiao Tong Univ, Gas Turbine Res Inst, Sch Mech Engn, Shanghai 200240, Peoples R China.
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:165/56  |  Submit date: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./通讯作者:Wang YP(汪运鹏)(1,2)
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:754/148  |  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  
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./通讯作者:HU, Zongmin
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download:462/240  |  Submit date: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./通讯作者:Wang, Xiaojun
Authors:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
View  |  Adobe PDF(2082Kb)  |  Favorite  |  View/Download:571/240  |  Submit date: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
Authors:  胡守超;  崔凯;  李广利;  肖尧;  司徒明
View  |  Adobe PDF(1239Kb)  |  Favorite  |  View/Download:655/218  |  Submit date:2016/12/16
Hypersonic Airplane  Air-breathing Vehicle  Shape Optimization  Parameterization  Uniform Design  
Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟)
View  |  Adobe PDF(199Kb)  |  Favorite  |  View/Download:723/194  |  Submit date:2014/04/02
Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ  
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
Authors:  Jiang ZL(姜宗林);  Liu YF(刘云峰);  Han GL(韩桂来);  Zhao W(赵威);  Jiang ZL
Adobe PDF(226Kb)  |  Favorite  |  View/Download:984/243  |  Submit date: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
Authors:  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)  |  Favorite  |  View/Download:1027/414  |  Submit date:2009/08/03
Hypersonic Vehicle  High-temperature  Thermal Protection  High-temperature Ceramics  Carbon/carbon Composites  Oxidation Behavior  Creep-behavior  Carbon  Microstructure  Diboride  Kinetics