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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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力学所知识产出(19... [7]
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刘嘉 [7]
王发民 [7]
姚文秀 [5]
雷麦芳 [4]
刘宏 [2]
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Creator:刘嘉
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高超声速飞行器测热试验研究
期刊论文
流体力学实验与测量, 2004, 卷号: 18, 期号: 1, 页码: 29-32,37
Authors:
刘嘉
;
姚文秀
;
李静美
;
王发民
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Submit date:2010/05/03
高超声速飞行器
热流率
风洞试验
高超声速边界层流动转捩研究
期刊论文
计算物理, 2004, 卷号: 21, 期号: 1, 页码: 61-67
Authors:
刘嘉
;
雷麦芳
;
姚文秀
;
王发民
Adobe PDF(409Kb)
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高超声速流动
稳定性分析
转捩
高超声速飞行器前体压缩性能研究
期刊论文
应用数学和力学, 2004, 卷号: 25, 期号: 1, 页码: 85-92
Authors:
刘嘉
;
姚文秀
;
雷麦芳
;
王发民
Adobe PDF(559Kb)
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高超声速飞行器
一体化设计
压缩性
超音速来流中侧向喷流干扰流场的数值模拟
期刊论文
航空学报, 2004, 卷号: 25, 期号: 2, 页码: 108-112
Authors:
周维
;
刘宏
;
刘嘉
;
王发民
Adobe PDF(318Kb)
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Submit date:2007/06/15
侧向喷流
Forebody Compressibility Research of Hypersonic Vehicle
期刊论文
Applied Mathematics and Mechanics (English Edition), 2004, 卷号: 25, 期号: 1, 页码: 93-101
Authors:
Liu J(刘嘉)
;
Yao WX(姚文秀)
;
Lei MF(雷麦芳)
;
Wang FM(王发民)
;
Wang, FM (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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乘波前体构型设计与压缩性能分析
期刊论文
工程力学, 2003, 卷号: 20, 期号: 6, 页码: 130-134
Authors:
刘嘉
;
王发民
Adobe PDF(192Kb)
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乘波体
相交楔锥
压缩性
一体化设计
钝锥绕流流动稳定性分析与转捩预报
期刊论文
计算物理, 2002, 卷号: 19, 期号: 2, 页码: 115-120
Authors:
刘宏
;
王发民
;
刘嘉
;
姚文秀
;
雷麦芳
Adobe PDF(374Kb)
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Submit date:2010/05/03
钝锥
Rayleigh迭代
稳定性
转捩