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基于CFD/CSD耦合的导弹舵面颤振数值研究 会议论文
2018年全国固体力学学术会议, 中国黑龙江哈尔滨, 2018年11月23日至25日
Authors:  姜倩;  郑冠男;  杨国伟
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CFD/CSD耦合  颤振特性  气动弹性  导弹舵面  
基于CFD/CSD耦合含间隙三维全动舵面气动弹性研究 期刊论文
应用力学学报, 2018, 卷号: 35, 期号: 1, 页码: 1-7
Authors:  黄程德;  郑冠男;  杨国伟;  黄杰
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间隙非线性  虚拟质量法  切换点  二分法  极限环振荡  CFD/CSD耦合  
基于任意多面体网格的Navier-Stokes方程并行求解器 期刊论文
科学技术与工程, 2016, 卷号: 16, 期号: 18, 页码: 101-105+139
Authors:  张明锋;  杨国伟;  郑冠男;  刘中玉
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并行求解器  Navier-stokes方程  任意多面体网格  有限体积方法  并行效率  
基于预处理HLLEW格式的全速域数值算法 期刊论文
计算物理, 2016, 卷号: 33, 期号: 3, 页码: 273-282
Authors:  刘中玉;  张明锋;  郑冠男;  杨国伟
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Preconditioning  Flow At All Mach Number  Incompressible Flow  Hllew Scheme  Implicit Time-marching  
An airplane jig shape design method based on high fidelity aeroelastic simulation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 47, 页码: 314-323
Authors:  Yang W;  Wang QF;  Zhou L;  Zheng GN(郑冠男);  Liu W;  Yang, W (reprint author), Commercial Aircraft Corp China Ltd, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China.
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Aeroelasticity  Cfd  Csd  Jig Shape  Structural Mesh  
某全机跨声速颤振模型颤振特性仿真与试验验证 期刊论文
空气动力学学报, 2014, 卷号: 32, 期号: 3, 页码: 364-368
Authors:  钱卫;  杨国伟;  张桂江;  郑冠男
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跨声速颤振  全机结构相似颤振模型  Cfd颤振仿真  跨声速颤振风洞试验  N-s方程  
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
Authors:  Qian W;  Yang GW(杨国伟);  Zheng GN(郑冠男);  Zhang GJ
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All-movable Horizontal Tail  Flutter Boundaries  Overload Factors  Structure Dynamics  Transonic Flutter  Transonic Speed  Wind Tunnel Tests  Wind-tunnel Testing  
基于任意多面体网格的Navier-Stokes方程并行求解器 会议论文
第八届全国流体力学学术会议, 中国甘肃兰州, 2014-09-18
Authors:  张明锋;  郑冠男;  刘中玉;  杨国伟
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并行求解器  Navier-stokes方程  任意多面体网格  有限体积方法  计算效率  
Flutter analyses of complete aircraft based on hybrid grids and parallel computing 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 2, 页码: 398-404
Authors:  Zheng GN(郑冠男);  Yang GW(杨国伟);  Qian W;  Yang, GW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
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Cfd  Csd  Aeroelasticity  Coupled Method  Flutter  Mpi  
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
Authors:  Yang GW(杨国伟);  Zheng GN(郑冠男);  Nie XY(聂雪媛)
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Dynamic Mesh  Rbf  Reduced-point Option  Aeroelasticity