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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:990/216  |  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  
基于CFD分析的弧形翼导弹气动外形优化 期刊论文
中国科学. G辑, 物理学,力学,天文学, 2009, 卷号: 39, 期号: 6, 页码: 865-873
Authors:  崔凯;  杨国伟
Adobe PDF(3468Kb)  |  Favorite  |  View/Download:762/132  |  Submit date:2010/05/03
优化设计  导弹  弧形翼  计算流体力学  可变多面体搜索方法  
Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing 期刊论文
Journal of Aircraft, 2009, 卷号: 46, 期号: 4, 页码: 1444-1450
Authors:  Yang GW(杨国伟);  Chen DW(陈大伟);  Cui K(崔凯);  Yang GW
Adobe PDF(1016Kb)  |  Favorite  |  View/Download:899/203  |  Submit date:2009/08/03
Navier-stokes Solver  Aircraft  
Waverider configurations derived from general conical flowfields 期刊论文
Acta Mechanica Sinica, 2007, 卷号: 23, 期号: 3, 页码: 247-255
Authors:  Cui K(崔凯);  Zhao DX;  Yang GW(杨国伟);  Cui, K (reprint author), Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116023, Peoples R China.
Adobe PDF(649Kb)  |  Favorite  |  View/Download:871/228  |  Submit date:2009/08/03
Waverider  Hypersonic  Computational Fluid Dynamics  Navier-stokes Solver  Design  Cone  
The Effect of Conical Flowfields on the Performance of Waveriders at Mach 6 期刊论文
Chinese Science Bulletin, 2007, 卷号: 52, 期号: 1, 页码: 57-64
Authors:  Cui K(崔凯);  Yang GW(杨国伟);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100080, Peoples R China.
Adobe PDF(655Kb)  |  Favorite  |  View/Download:754/259  |  Submit date:2007/06/15
6马赫锥体流场对乘波体性能的影响及规律 期刊论文
科学通报, 2006, 卷号: 51, 期号: 24, 页码: 2830-2837
Authors:  崔凯;  杨国伟
Adobe PDF(967Kb)  |  Favorite  |  View/Download:883/166  |  Submit date:2010/05/03
高超声速飞行器  乘波体  计算流体力学