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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... [23]
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2007 [23]
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高超声速进气道起动特性数值研究
期刊论文
宇航学报, 2007, 卷号: 28, 期号: 6, 页码: 1482-1487
Authors:
丁海河
;
王发民
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Submit date:2010/05/03
进气道
起动特性
边界层抽吸
流动相似律在气流式倾角传感器中的应用
期刊论文
电子科技大学学报, 2007, 卷号: 36, 期号: 5, 页码: 931-934
Authors:
郑永红
;
彭世
;
黄小丽
;
靳映霞
Adobe PDF(215Kb)
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View/Download:449/134
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Submit date:2010/05/03
气流式
自然对流
相似
温度场
高超声速飞行器-进气道一体化热流数值计算
期刊论文
航空动力学报, 2007, 卷号: 22, 期号: 8, 页码: 1297-1302
Authors:
丁海河
;
王发民
Adobe PDF(403Kb)
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Submit date:2010/05/03
航空、航天推进系统
气动热
超燃冲压发动机
转捩
Cfd(计算流体动力学)
超声速燃烧室凹腔火焰稳定器的数值模拟
期刊论文
推进技术, 2007, 卷号: 28, 期号: 2, 页码: 135-140
Authors:
陈方
;
陈立红
;
张新宇
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Submit date:2010/05/03
超音速燃烧
凹体
燃烧性能
氢
数值仿真
三角翼受迫俯仰滚转耦合运动的气动特性研究
期刊论文
空气动力学学报, 2007, 卷号: 25, 期号: 1, 页码: 65-69
Authors:
郭迪龙
;
杨国伟
;
康宏琳
;
王发民
Adobe PDF(239Kb)
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Submit date:2010/05/03
三角翼
气动特性
受迫俯仰滚转耦合运动
涡结构
磁性纳米颗粒对微槽道液体流动的混合增强作用
期刊论文
实验流体力学, 2007, 卷号: 21, 期号: 1, 页码: 54-58
Authors:
王化峰
;
程万
;
李战华
Adobe PDF(571Kb)
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Submit date:2010/05/03
微流体
微芯片
混合增强
纳米颗粒
磁驱动
高超声速乘波飞行器气动特性研究(英文)
期刊论文
宇航学报, 2007, 期号: 1, 页码: 203-208
Authors:
张杰
;
王发民
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Submit date:2010/05/03
高超声速乘波体
计算流体力学
风洞试验
粘性阻力分析
参考温度法
Numerical Investigation On Detonation Cell Evolution In A Channel With Area-Changing Cross Section
期刊论文
Science In China Series G-Physics Mechanics & Astronomy, 2007, 页码: 797-808
Authors:
Deng B(邓博)
;
Hu ZM(胡宗民)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Deng, B (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temperature Gas Dynam, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Detonation Cells
Transverse Waves
Detailed Chemical Reaction Model
Numerical Simulation
Shock
高焓风洞流场测量的数值重建和非平衡效应的数值分析
学位论文
博士论文,北京: 中国科学院研究生院, 2007
Authors:
曾明
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View/Download:982/48
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Submit date:2009/04/13
Determination of the Maximum Effective Burning Velocity of Dust-Air Mixtures in Constant Volume Combustion
期刊论文
JOURNAL OF LOSS PREVENTION IN THE PROCESS INDUSTRIES, 2007, 卷号: 20, 期号: 4-6, 页码: 462-469
Authors:
Pu Y K
;
Jia F
;
Wang SF(王双峰)
;
Skjold T
;
Pu, YK (reprint author), Chinese Acad Sci, Inst Mech, Natl Micrograv Lab, Beijing 100080, Peoples R China.
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Submit date:2016/01/11
Dust Explosion
Constant Volume Combustion
Maximum Effective Burning Velocity