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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(1... [10]
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傅德薰 [21]
李新亮 [21]
马延文 [20]
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梁贤 [7]
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Mach 8 的平板可压缩湍流边界层直接数值模拟及分析
期刊论文
中国科学: 物理学 力学 天文学, 2012, 卷号: 42, 期号: 3, 页码: 282-293
Authors:
梁贤
;
李新亮
;
傅德薰
;
马延文
;
E-mail: liangxian@imech.ac.cn
Adobe PDF(2097Kb)
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Submit date:2012/11/19
直接数值模拟
高超声速
壁湍流
可压缩性效应
边界层
基于直接数值模拟的可压缩湍流模型评估与改进
期刊论文
力学学报, 2012, 卷号: 44, 期号: 2, 页码: 222-229
Authors:
李新亮
;
傅德薰
;
马延文
Adobe PDF(14774Kb)
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Submit date:2012/11/19
直接数值模拟
湍流模型
先验评估
【key Words】 Direct Numerical Simulation
Turbulence Model
Assessment
万核级可扩展CFD软件及应用
期刊论文
华中科技大学学报(自然科学版), 2011, 卷号: 39, 期号: S1, 页码: 67-70
Authors:
梁贤
;
李新亮
;
傅德薰
;
马延文
Adobe PDF(234Kb)
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Submit date:2012/04/01
超级计算
加速比
复杂流动
直接数值模拟
湍流
DNS of shock/boundary layer interaction flow in a supersonic compression ramp
会议论文
6th International Conference on Computational Fluid Dynamics, St Petersburg, RUSSIA, JUL 12-16, 2010
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Liang X(梁贤)
;
Li, XL (reprint author), CAS, Inst Mech, LHD, Beijing 100190, Peoples R China
Adobe PDF(966Kb)
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Submit date:2013/02/26
Turbulent-boundary-layer
Direct Numerical-simulation
Mach8 的平板可压缩湍流边界层直接数值模拟
会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:
梁贤
;
李新亮
;
傅德薰
;
马延文
Adobe PDF(882Kb)
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Submit date:2014/01/23
直接数值模拟
高超声速
壁湍流
可压缩
边界层
基于直接数值模拟的超/高超声速湍流模型评估与改进
会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors:
李新亮
;
傅德薰
;
马延文
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Submit date:2010/11/25
Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp
期刊论文
SCIENCE CHINA: Physics, Mechanics & Astronomy, 2010, 卷号: 53, 期号: 9, 页码: 1651-1658
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Liang X(梁贤)
;
Li XL(李新亮)
Adobe PDF(951Kb)
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View/Download:1612/366
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Submit date:2010/10/25
compression Ramp
Shock/turbulent Boundary Layer Interaction
Direct Numerical Simulation
Shock Oscillation
Direct Numerical Simulation of Compressible Turbulent Flows
期刊论文
ACTA MECHANICA SINICA, 2010, 卷号: 26, 期号: 6, 页码: 795-806
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Liang X(梁贤)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Submit date:2016/02/01
Direct Numerical Simulation
Compressible Turbulence
Coherent Structures
Turbulent Boundary-layer Flow
Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack
期刊论文
Physics of Fluids, 2010, 卷号: 22, 期号: 2, 页码: 025105-1-18
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Li XL(李新亮)
Adobe PDF(3867Kb)
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Submit date:2010/03/07
Effects of wall temperature on boundary layer stability over a blunt cone at Mach 7.99
期刊论文
Computers & Fluids, 2010, 卷号: 39, 期号: 2, 页码: 359–371
Authors:
Liang X(梁贤)
;
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
梁贤,李新亮
Adobe PDF(1248Kb)
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View/Download:1211/354
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Submit date:2009/12/28