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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
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
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High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430
Authors:  Jiang YZ;  Wen CY;  Zhang DL(张德良)
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Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors:  Peng J(彭俊);  Luo ZT(罗长童);  Han ZJ(韩子健);  Hu ZM(胡宗民);  Han GL(韩桂来);  Jiang ZL(姜宗林)
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Shock-shock interaction  Machine learning  Hypersonic flow  Impinging jet  Genetic programming  Triple point  
Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
Authors:  Zhang W;  Wang S;  Wang Q;  Ju SJ(鞠胜军);  Yan C
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Aerodynamic thermal  Opposing jets  Parametric sensitivity analysis  Uncertainty quantification  Analysis of Variance  Non-Intrusive Polynomial Chaos  
Synthesis and characterization of light-weight porous ceramics used in the transpiration cooling 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 177, 页码: 438-445
Authors:  Zhang, Bo;  Huang, Jie;  Li, Weijie;  Huang, Haiming;  Zhao, Huanyu;  Peng JL(彭锦龙)
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Carbon fiber-reinforced silicon carbide porous ceramics  Permeability  Oxyacetylene flame test  Transpiration cooling  
Nonprobabilistic uncertain model updating and optimization design of thermal protection system 期刊论文
APPLIED THERMAL ENGINEERING, 2020, 卷号: 180, 页码: 14
Authors:  Jiang WT;  Wang XJ;  Wang RX(王睿星);  Shi QH;  Zhu JJ
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Thermal protection system  Nonprobabilistic optimization  Sensitivity analysis  Uncertainty analysis  Model updating  
Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10
Authors:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
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Optimization design  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Coaxial Thermocouples for Heat Transfer Measurements in Long-Duration High Enthalpy Flows 期刊论文
SENSORS, 2020, 卷号: 20, 期号: 18, 页码: 18
Authors:  Zhang SZ(张仕忠);  Wang Q(汪球);  Li JP(李进平);  Zhang XY(张晓源);  Chen H(陈宏)
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heat transfer measurement  coaxial thermocouple  long-duration  semi-infinite  high enthalpy  
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)
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hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310
Authors:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
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Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet