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| DSMC碰撞模型参数对高超声速化学反应流的影响 会议论文 第十二届全国流体力学学术会议, 中国陕西西安, 2022-11-19 作者: 赵文盛; 胡远; 李锦; 耿湘人; 杨超; 孙泉华 Adobe PDF(176Kb)  |  收藏  |  浏览/下载:155/34  |  提交时间:2023/04/14 DSMC 碰撞模型参数 高超声速化学反应流 |
| 太极一号射频离子微推力器地面测试与评估 会议论文 第十六届中国电推进学术研讨会, 北京,中国, 12月25-27日 作者: 贺建武; 马隆飞; 杨超; 薛森文; 段俐; 康琦 收藏  |  浏览/下载:117/0  |  提交时间:2021/02/01 |
| DSMC simulation of gas heat transfer between coaxial cylinders 会议论文 31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018 作者: Song H(宋航); Yang C(杨超); Sun QH(孙泉华) Adobe PDF(647Kb)  |  收藏  |  浏览/下载:146/55  |  提交时间:2020/11/20 |
| A microscopic study of one-dimensional H2-O2 detonation using DSMC method 会议论文 31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018 作者: Yang C(杨超); Huang HJ(黄河激); Sun QH(孙泉华) Adobe PDF(936Kb)  |  收藏  |  浏览/下载:159/65  |  提交时间:2020/11/20 |
| 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 作者: Cui K(崔凯); Wang XP; Hu SC; Gao TY; Yang GW(杨国伟) Adobe PDF(797Kb)  |  收藏  |  浏览/下载:1208/352  |  提交时间: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 作者: 胡守超; 崔凯; 李广利; 屈志朋; 杨国伟 浏览  |  Adobe PDF(64Kb)  |  收藏  |  浏览/下载:457/172  |  提交时间: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 作者: 胡守超; 崔凯; 李广利; 屈志朋; 杨国伟 Adobe PDF(1737Kb)  |  收藏  |  浏览/下载:501/130  |  提交时间: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 作者: Cui K(崔凯); Hu SC(胡守超); Gao TY(高太元); Wang XP(王秀平); Yang GW(杨国伟) 浏览  |  Adobe PDF(199Kb)  |  收藏  |  浏览/下载:470/73  |  提交时间:2014/04/02 Vehicle Leading 0algorithm Genetic Hypersonic Optimization Aerothermal Based Method Design Attack Novel Around Angle Evaluated Greatly About Fluid Result Differ |
| 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 作者: 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)  |  收藏  |  浏览/下载:783/188  |  提交时间: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 作者: 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)  |  收藏  |  浏览/下载:605/141  |  提交时间:2013/02/26 China Railways High-speed (Crh) Nose Shape Computational Fluid Mechanics Optimization |