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Comparison of the simulated and LIDAR measured atmospheric density and temperature in lower thermosphere 会议论文
The 29th International Symposium on Rarefied Gas Dynamics, 中国陕西西安, 2014-07-13
作者:  Wan T(万田);  Hu GQ(胡国庆);  Jiang JZ(蒋建政);  Liu HL(刘宏立);  Fan J(樊菁);  Pan YL(潘蔚林);  Qiao S(乔帅)
浏览  |  Adobe PDF(1166Kb)  |  收藏  |  浏览/下载:204/69  |  提交时间:2015/09/10
Comparison of the simulated and LIDAR measured atmospheric density and temperature in transitional flow regime 会议论文
The 29th International Symposium on Rarefied Gas Dynamics, 中国陕西西安, 2014-07-13
作者:  Wan T(万田);  Hu GQ(胡国庆);  Jiang JZ(蒋建政);  Liu HL(刘宏立);  Fan J(樊菁);  Pan YL(潘蔚林);  Qiao S(乔帅)
浏览  |  Adobe PDF(28Kb)  |  收藏  |  浏览/下载:169/72  |  提交时间:2015/09/10
Transitional  Lidar  Regime  Altitude  Empirical  Diurnal  
Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds 会议论文
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russia, September 7, 2014 - September 12, 2014
作者:  Qian W;  Yang GW(杨国伟);  Zheng GN(郑冠男);  Zhang GJ
浏览  |  Adobe PDF(1159Kb)  |  收藏  |  浏览/下载:200/66  |  提交时间:2017/05/27
All-movable Horizontal Tail  Flutter Boundaries  Overload Factors  Structure Dynamics  Transonic Flutter  Transonic Speed  Wind Tunnel Tests  Wind-tunnel Testing  
Fast Dynamic Mesh Method and its Application on Aeroelasticity 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
作者:  Yang GW(杨国伟);  Zheng GN(郑冠男);  Nie XY(聂雪媛)
浏览  |  Adobe PDF(3458Kb)  |  收藏  |  浏览/下载:666/236  |  提交时间:2014/03/11
Dynamic Mesh  Rbf  Reduced-point Option  Aeroelasticity  
Interaction of shock wave with multi-fluids interface using quadrilateral-based adaptive mesh 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2012, 卷号: 23, 期号: 5, 页码: 1250033
作者:  Zheng HW(郑洪伟);  Li XJ(李现今);  Yang GW(杨国伟);  Shu C;  Zheng, HW;  Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(791Kb)  |  收藏  |  浏览/下载:724/173  |  提交时间:2013/01/18
Shock  Multi-fluids  Interface  Unstructured  Adaptive Mesh Refinement  Quadrilateral  Instability Driven  
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
作者:  Zheng HW(郑洪伟);  Yang GW(杨国伟);  Zheng HW(郑洪伟)
Adobe PDF(778Kb)  |  收藏  |  浏览/下载:733/265  |  提交时间:2013/02/06
High Speed Train  Detached Eddy Simulation  Aerodynamic Performance  
基于背景网格的混合网格变形方法 期刊论文
振动工程学报, 2011, 卷号: 24, 期号: 5, 页码: 473-481
作者:  郑冠男;  杨国伟
Adobe PDF(2966Kb)  |  收藏  |  浏览/下载:690/181  |  提交时间:2012/04/01
动网格方法  背景网格  弹簧网络法  代数插值  气动弹性  
基于混合网格Navier-Stokes方程的并行隐式计算方法研究 期刊论文
应用力学学报, 2011, 卷号: 28, 期号: 3, 页码: 211-218
作者:  郑冠男;  邓守春;  韩同来;  杨国伟
Adobe PDF(2129Kb)  |  收藏  |  浏览/下载:839/241  |  提交时间:2012/04/01
混合网格  K-ω两方程湍流模型  Dp-lur隐式方法  Mpi  染色分层通讯  
Convective heat transfer characteristics of China RP-3 aviation kerosene at supercritical pressure 期刊论文
Applied Thermal Engineering, 2011, 卷号: 31, 期号: 14-15, 页码: 2360-2366
作者:  Li XF;  Huai XL;  Cai J;  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Guo ZX;  Huai, XL (reprint author), Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
Adobe PDF(289Kb)  |  收藏  |  浏览/下载:1288/408  |  提交时间:2012/04/01
Supercritical Pressure  Aviation Kerosene  Convective Heat Transfer  Numerical Study  Cracked Kerosene  Tubes  Water  Flows  
基于混合网格NS 方程并行计算的某机全机颤振特性分析 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
作者:  郑冠男;  杨国伟;  钱卫
Adobe PDF(569Kb)  |  收藏  |  浏览/下载:419/138  |  提交时间:2014/01/23
Cfd  Csd  气动弹性  耦合算法  颤振特性  Mpi