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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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岳连捷 [4]
张新宇 [3]
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卢洪波 [2]
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Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
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View/Download:376/134
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
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
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
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View/Download:548/186
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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