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Method of Selecting Active Parameters Using Sensitivity Analysis and Linear Programming 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2023, 页码: 17
作者:  Li YJ(李昱君);  Zhang TC(张泰昌);  Fang, Yunming;  Fan XJ(范学军)
Adobe PDF(3807Kb)  |  收藏  |  浏览/下载：59/0  |  提交时间：2023/11/28
Active parameter  sensitivity analysis  linear programming  selection method  chemical kinetic model  
Study of the effects of hydraulic fractures on gas and water flow in shale gas reservoirs 期刊论文
Energy Sources, Part A: Recovery Utilization and Environmental Effects, 2023, 卷号: 45, 期号: 3, 页码: 9540-9551
作者:  Wan YJ;  Chen ZY;  Shen WJ (沈伟军);  Kuang ZX;  Liu XH;  Guo W;  Hu Y
Adobe PDF(1984Kb)  |  收藏  |  浏览/下载：484/91  |  提交时间：2019/11/15
Shale gas reservoir  hydraulic fracture  sensitivity analysis  gas desorption  water retention  gas production  
Multi-objective robust optimization of a solar power tower plant under uncertainty 期刊论文
ENERGY, 2022, 卷号: 238, 页码: 11
作者:  Luo, Yan;  Wang, Zhiyuan;  Zhu, Jiamin;  Lu, Tao;  Xiao, Gang;  Chu, Fengming;  Wang RX(王睿星)
Adobe PDF(2614Kb)  |  收藏  |  浏览/下载：377/94  |  提交时间：2021/11/01
Solar power tower plant system  Uncertainty propagation  Multi-objective robust optimization  Global sensitivity analysis  Levelized cost of energy  
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
作者:  Zhang W;  Wang S;  Wang Q;  Ju SJ(鞠胜军);  Yan C
Adobe PDF(2859Kb)  |  收藏  |  浏览/下载：249/97  |  提交时间：2021/02/09
Aerodynamic thermal  Opposing jets  Parametric sensitivity analysis  Uncertainty quantification  Analysis of Variance  Non-Intrusive Polynomial Chaos  
Tandem, long-duration, ultra-high-altitude tethered balloon and its system characteristics 期刊论文
ADVANCES IN SPACE RESEARCH, 2020, 卷号: 66, 期号: 10, 页码: 2446-2465
作者:  Zhang DH;  Luo HB;  Cui YX;  Zeng XH(曾晓辉);  Wang S
Adobe PDF(3704Kb)  |  收藏  |  浏览/下载：249/71  |  提交时间：2020/11/30
Tethered balloon  Ultra-high altitude  Static model  Design method  Sensitivity analysis  
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
作者:  Jiang WT;  Wang XJ;  Wang RX(王睿星);  Shi QH;  Zhu JJ
Adobe PDF(6028Kb)  |  收藏  |  浏览/下载：240/67  |  提交时间：2020/11/30
Thermal protection system  Nonprobabilistic optimization  Sensitivity analysis  Uncertainty analysis  Model updating  
Thermal effects of substrate on Marangoni flow in droplet evaporation: Response surface and sensitivity analysis 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2017, 卷号: 113, 页码: 354-365
作者:  Chen X(陈雪);  Wang, Xun;  Chen, Paul G.;  Liu QS(刘秋生);  Liu, QS (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Micrograv, Beijing 100190, Peoples R China.
Adobe PDF(2334Kb)  |  收藏  |  浏览/下载：425/188  |  提交时间：2017/11/29
Droplet Evaporation  Marangoni Flow  Thermal Property  Response Surface  Sensitivity Analysis  
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：434/214  |  提交时间：2018/01/16
Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China.
Adobe PDF(2993Kb)  |  收藏  |  浏览/下载：351/164  |  提交时间：2017/12/18
Detailed Hydrogen Oxidation Mechanism  Dlr  Flame Stabilization  Sensitivity Analysis  Supersonic Combustion  
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
Adobe PDF(1195Kb)  |  收藏  |  浏览/下载：464/170  |  提交时间：2016/07/01
Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients