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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(19... [4]
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张新宇 [14]
陈立红 [14]
岳连捷 [8]
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Creator:张新宇
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Quasi-One-Dimensional Multimodes Analysis for Dual-Mode Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2014, 卷号: 30, 期号: 6, 页码: 1559-1567
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Tian, L (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2014/12/18
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Tong YG(仝颖刚)
;
Shen Y(沈岩)
;
Chen J(陈健)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Yu, XL (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:2013/07/30
Scramjet
Kerosene Fuel
Plasma Torch
Ignition
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:
Xiao YB(肖雅彬)
;
Yue LJ(岳连捷)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Xiao YB(肖雅彬)
Adobe PDF(1674Kb)
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Submit date:2014/02/24
Three-Dimensional heat transfer analysis and optimized design of actively cooled strut for scramjet applications
会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:
Zhong FQ(仲峰泉)
;
Chen TY(陈同银)
;
Fan XJ(范学军)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Zhong FQ(仲峰泉)
Adobe PDF(2023Kb)
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Submit date:2014/02/24
局部收缩比处处一致的变截面高超声速内转式进气道设计方法
会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:
肖雅彬
;
岳连捷
;
高占彪
;
陈立红
;
张新宇
Adobe PDF(2046Kb)
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Submit date:2014/01/23
优化NURBS内转式进气道设计与流场研究
会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:
肖雅彬
;
岳连捷
;
陈立红
;
张新宇
Adobe PDF(1354Kb)
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Submit date:2014/01/23
高超声速
进气道
内转式
边界层抽吸
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
Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Gu HB(顾洪斌)
;
Li Z(李智)
;
Li F(李飞)
;
Chen LH(陈立红)
;
Gu SL(顾声龙)
;
Zhang XY(张新宇)
;
Gu HB(顾洪斌)
Adobe PDF(242Kb)
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Submit date:2014/02/24
高超声速流线追踪进气道基准流场设计
会议论文
第二届高超声速科技学术会议, 中国安徽黄山, 2009-11-02
Authors:
岳连捷
;
肖雅彬
;
陈立红
;
张新宇
Adobe PDF(734Kb)
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Submit date:2010/11/25
高超声速
流线追踪进气道
基准流场
溢流槽道位置对二元高超声速进气道性能研究
会议论文
第二届高超声速科技学术会议, 安徽·黄山
Authors:
张晓嘉
;
岳连捷
;
陈立红
;
张新宇
Adobe PDF(5127Kb)
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Submit date:2010/11/25