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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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State Key... [10]
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岳连捷 [10]
卢洪波 [8]
张新宇 [8]
肖雅彬 [5]
陈立红 [4]
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Role of wall temperature on shock train in a rectangular isolator
会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:
Lu HB
;
Wang D
;
Chen X
;
Yue LJ(岳连捷)
;
Ji, Feng (yuelj@imech.ac.cn)
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Submit date:2017/05/05
Aero
Heating
Dual Mechanisms
On Flow
Shock Train
Specific Heat Ratio
Total Pressure
Total Temperatures
Wall Temperatures
Aerothermal characteristics of bleed slot in hypersonic flows
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:
Yue LJ(岳连捷)
;
Lu HB
;
Xu X
;
Chang XY
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Boundary Layer Control
Boundary Layer Heat Flow
Shock Wave Interactions
Separated Flows
高超声速进气道快速破膜开启的流动特性
期刊论文
航空学报, 2015, 卷号: 36, 期号: 6, 页码: 1795-1804
Authors:
徐骁
;
岳连捷
;
卢洪波
;
肖雅彬
;
张新宇
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Submit date:2015/12/25
高超声速进气道
破膜开启
非定常效应
激波边界层相互作用
分离流
局部收缩比一致的变截面高超声速内转式进气道
专利
发明专利. 局部收缩比一致的变截面高超声速内转式进气道, 专利号: ZL201210157992.X, 申请日期: 2012-05-21, 授权日期: 2014-06-13
Inventors:
肖雅彬
;
岳连捷
;
卢洪波
;
陈立红
;
张新宇
Adobe PDF(457Kb)
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Submit date:2014/06/13
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods
期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Yue LJ(岳连捷)
Adobe PDF(1133Kb)
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Submit date:2014/04/15
Hypersonic Inlet
Cowl-lip Bluntness
Flow Characteristics
Shock Pattern
Shock Interference
Interaction of isentropic compression waves with a bow shock
期刊论文
AIAA JOURNAL, 2013, 卷号: 51, 期号: 10, 页码: 2474-2484
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
;
Zhang XY(张新宇)
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2014/01/17
高超声速进气道唇缘钝化流动的数值研究
会议论文
第四届高超声速科技学术会议, 中国海南三亚, 2011
Authors:
卢洪波
;
岳连捷
;
肖雅彬
;
张新宇
Adobe PDF(62Kb)
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Submit date:2012/04/01
高超声速进气道
钝化唇缘
激波相干
气动热
超燃冲压发动机
高超声速进气道唇缘钝化流动的波系配置及热负荷特性研究
会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:
卢洪波
;
岳连捷
;
肖雅彬
;
陈立红
;
张新宇
Adobe PDF(766Kb)
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Submit date:2014/01/23
高超声速进气道
钝化唇缘
激波相干
气动热
扩张方式对隔离段流场特性的影响
会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors:
裘鑫
;
岳连捷
;
卢洪波
;
陈立红
;
张新宇
Adobe PDF(778Kb)
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Submit date:2010/11/25
隔离段激波串非对称及震荡特性实验研究
会议论文
第八届全国实验流体力学学术会议, 中国广东广州, 2010-12-26
Authors:
岳连捷
;
卢洪波
;
裘新
;
陈立红
;
张新宇
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Submit date:2014/04/02
超然冲压发动机隔离段激波串非对称性震荡特性