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高速列车过隧道、明线会车及隧道会车工况下的动力响应研究 会议论文
第21届全国结构工程学术会议, 中国辽宁沈阳, 2012-10-12
Authors:  赖姜;  曾晓辉;  孙振旭;  杨国伟
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高速列车  明线会车  过隧道  隧道会车  动力学响应  
An new approach for acceleration of train model with compressed air 会议论文
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
Authors:  Yang QS(杨乾锁);  Song JH;  Yang GW(杨国伟);  Yang QS(杨乾锁)
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Moving Train Model Experiments  Airgun  Compressed Air  Friction Deceleration  
Investigation of aerodynamic performance of high-speed train by detached eddy simulation 会议论文
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
Authors:  Zheng HW(郑洪伟);  Yang GW(杨国伟);  Zheng HW(郑洪伟)
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High Speed Train  Detached Eddy Simulation  Aerodynamic Performance  
Comparisons of high order hybrid schemes using a parameter-free discontinuity detector 会议论文
42nd AIAA Fluid Dynamics Conference and Exhibit 2012, New Orleans, LA, United states, JUN 25-28, 2012
Authors:  Shen YQ(申义庆);  Zha GC;  Yang GW(杨国伟);  Gao Z(高智);  Shen YQ(申义庆)
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A numerical study on aerodynamic noise sources of high-speed train 会议论文
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
Authors:  Yang Y(杨焱);  Yang GW(杨国伟);  Yang Y(杨焱)
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High-speed Train  Aerodynamic Noise  Noise Source Generation  Cfd  Caa  
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
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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
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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)
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Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ