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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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钝锥高超声速边界层来流感受性数值研究
期刊论文
中国科学. G辑, 物理学,力学,天文学, 2008, 卷号: 38, 期号: 9, 页码: 1246-1254
Authors:
张玉东
;
傅德薰
;
马延文
;
李新亮
Adobe PDF(1531Kb)
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Submit date:2010/05/03
感受性
激波装配法
迎风紧致格式
直接数值模拟
钝锥
三面压缩式高超声速进气道流动结构研究
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 2, 页码: 64-67
Authors:
肖雅彬
;
岳连捷
;
龚鹏
;
王世芬
;
陈立红
;
张新宇
Adobe PDF(413Kb)
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Submit date:2010/05/03
超声速进气道
流动结构
油滴显示
数值模拟
高超声速飞行器前体/冲压发动机一体化气动热实验研究
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 2, 页码: 10-14
Authors:
雷麦芳
;
丁海河
;
王发民
Adobe PDF(459Kb)
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Submit date:2010/05/03
超燃冲压发动机
气动加热
风洞实验
热流分布
Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
期刊论文
SHOCK WAVES, 2008, 卷号: 18, 期号: 1, 页码: 41-51
Authors:
Hu ZM(胡宗民)
;
Myong R S
;
Wang C(王春)
;
Cho T H
;
Jiang ZL(姜宗林)
Adobe PDF(954Kb)
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Submit date:2020/08/26
Shock
Shock Interaction
Oscillation
Hypersonic
Double-wedge
Numerical Study
带中心支板侧压进气道流场特性研究
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 1, 页码: 31-35
Authors:
龚鹏
;
岳连捷
;
肖雅斌
;
王世芬
;
张新宇
Adobe PDF(621Kb)
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Submit date:2010/05/03
超燃冲压发动机
高超声速进气道
侧压式进气道
支板
可压缩尖锥边界层湍流的直接数值模拟
期刊论文
中国科学. G辑, 物理学,力学,天文学, 2008, 卷号: 38, 期号: 1, 页码: 89-101
Authors:
李新亮
;
傅德薰
;
马延文
Adobe PDF(5254Kb)
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Submit date:2010/05/03
尖锥
边界层湍流
直接数值模拟
湍动能
Receptivity To Free-Stream Disturbance Waves For Hypersonic Flow Over A Blunt Cone
期刊论文
Science In China Series G-Physics Mechanics & Astronomy, 2008, 页码: 1682-1690
Authors:
Zhang YD(张玉东)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Li XL(李新亮)
;
Zhang, YD (reprint author), China Acad Aerosp Aerodynam, Beijing 100074, Peoples R China.
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Submit date:2009/08/03
Receptivity
SPT方法在纳米粒子布朗运动观测中的应用
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 1, 页码: 84-87,100
Authors:
王绪伟
;
李战华
Adobe PDF(247Kb)
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Submit date:2009/12/30
布朗运动
单粒子追踪法
纳米粒子
扩散系数
Dns Of Compressible Turbulent Boundary Layer Around A Sharp Cone
期刊论文
Science In China Series G-Physics Mechanics & Astronomy, 2008, 页码: 699-714
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100080, Peoples R China.
Adobe PDF(806Kb)
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Submit date:2009/08/03
Direct Numerical Simulation
Direct Numerical Simulation Of Hypersonic Boundary-Layer Transition Over A Blunt Cone
期刊论文
AIAA Journal, 2008, 页码: 2899-2913
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Lab Nonlinear Mech, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Hyperbolic Conservation-laws