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Numerical well test model for caved carbonate reservoirs and its application in Tarim Basin, China 期刊论文
JOURNAL OF PETROLEUM SCIENCE AND ENGINEERING, 2018, 卷号: 161, 页码: 611-624
Authors:  Wan YZ;  Liu YW(刘曰武);  Chen FF;  Wu NY;  Hu GW
View  |  Adobe PDF(3967Kb)  |  Favorite  |  View/Download：403/90  |  Submit date：2018/03/05
Caved Carbonate Reservoir  Type Curves  Numerical Well Test  Finite Element Method  
三维后体/尾喷管一体化构型优化设计及性能分析 期刊论文
科学通报, 2012, 卷号: 57, 期号: 4, 页码: 239-247
Authors:  高太元;  崔凯;  王秀平;  胡守超;  杨国伟;  任亮
Adobe PDF(2922Kb)  |  Favorite  |  View/Download：1023/225  |  Submit date：2013/01/16
高超声速  后体/尾喷管一体化  单壁扩张喷管  优化设计  计算流体动力学  
Shape Optimization of High-Speed Train with the Speed of 500kph 会议论文
The 1st International Workshop on High-Speed and Intercity Railways, Beijing, 2012
Authors:  Cui K(崔凯);  Wang XP;  Hu SC;  Gao TY;  Yang GW(杨国伟)
Adobe PDF(797Kb)  |  Favorite  |  View/Download：1315/390  |  Submit date：2012/09/26
High Speed Train  Head Shape  Optimization  Rbf  Genetic Algorithm  Computational Fluid Dynamics  
双旁侧进气高超声速飞机气动布局初步设计与评估 会议论文
高超声速研讨会暨第五届全国高超声速科学技术会议, 中国广西桂林, 2012-11-12
Authors:  胡守超;  崔凯;  李广利;  屈志朋;  杨国伟
View  |  Adobe PDF(64Kb)  |  Favorite  |  View/Download：518/201  |  Submit date：2014/04/02
高超声速飞机  气动布局  进气  飞行攻角  乘波体  数值结果  升阻比  高容积率  层流模型  参数化设计  气动性能  整机  设计方案  构型  数值模拟方法  前缘  拼式  性能评估  前体  Cfd  
双旁侧进气高超声速飞机气动布局与评估 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:  胡守超;  崔凯;  李广利;  屈志朋;  杨国伟
Adobe PDF(1737Kb)  |  Favorite  |  View/Download：597/160  |  Submit date：2014/01/23
高超声速  双旁侧进气  气动布局  计算流体动力学(Cfd)  
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：534/85  |  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  
Aerodynamic optimization and evaluation for the three-dimensional afterbody/nozzle integrated configuration of hypersonic vehicles 期刊论文
Chinese Science Bulletin, 2012, 卷号: 57, 期号: 8, 页码: 849-857
Authors:  Gao TY(高太元);  Cui K(崔凯);  Wang XP(王秀平);  Hu SC(胡守超);  Yang GW(杨国伟);  Ren L;  [email protected]
Adobe PDF(985Kb)  |  Favorite  |  View/Download：1341/353  |  Submit date：2012/09/26
Hypersonic Afterbody/Nozzle Integrated Configuration Single Expanding Ramp Nozzle Optimization Computational Fluid Dynamics  
Leading edge aerothermal inverse design of hyersonic vehicle based on homotopy optimization method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
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);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(53Kb)  |  Favorite  |  View/Download：913/200  |  Submit date：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy  
Primary study of aerodynamic performance evaluation and optimization of the high-speed train 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Wang XP(王秀平);  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Yang GW(杨国伟);  Wang, XP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(349Kb)  |  Favorite  |  View/Download：689/158  |  Submit date：2013/02/26
China Railways High-speed (Crh)  Nose Shape  Computational Fluid Mechanics  Optimization  
Optimization of the upper surface of hypersonic vehicle based on CFD analysis 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Gao TY(高太元);  Cui K(崔凯);  Hu SC(胡守超);  Wang XP(王秀平);  Yang GW(杨国伟);  Gao, TY (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(305Kb)  |  Favorite  |  View/Download：779/204  |  Submit date：2013/02/26
Hypersonic  Shape Optimization  Sequential Quadratic Programming (Sqp)