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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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崔凯 [4]
杨国伟 [4]
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Aerodynamic optimization and evaluation for the three-dimensional afterbody/nozzle integrated configuration of hypersonic vehicles
期刊论文
Chinese Science Bulletin, 2012, 卷号: 57, 期号: 8, 页码: 849-857
Authors:
Gao TY(高太元)
;
Cui K(崔凯)
;
Wang XP(王秀平)
;
Hu SC(胡守超)
;
Yang GW(杨国伟)
;
Ren L
;
kcui@imech.ac.cn
Adobe PDF(985Kb)
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View/Download:1170/324
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Submit date:2012/09/26
Hypersonic Afterbody/Nozzle Integrated Configuration Single Expanding Ramp Nozzle Optimization Computational Fluid Dynamics
Shape Optimization for Hypersonic Arc-Wing Missiles
期刊论文
Journal of Spacecraft and Rockets, 2010, 卷号: 47, 期号: 4, 页码: 694-700
Authors:
Cui K(崔凯)
;
Yang GW(杨国伟)
Adobe PDF(4987Kb)
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View/Download:1234/239
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Submit date:2010/09/07
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)
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View/Download:850/219
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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)
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View/Download:737/256
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Submit date:2007/06/15