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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 ... [6]
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张新宇 [3]
于长平 [2]
余西龙 [2]
李新亮 [2]
李飞 [2]
王知溥 [2]
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2015 [6]
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Date Issued:2015
Community:高温气体动力学国家重点实验室
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Harmonic growth of spherical Rayleigh-Taylor instability in weakly nonlinear regime
期刊论文
PHYSICS OF PLASMAS, 2015, 卷号: 22, 期号: 11, 页码: 112112
Authors:
Liu WH(刘万海)
;
Chen YL
;
Yu ZP(于长平)
;
Li XL(李新亮)
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View/Download:404/103
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Submit date:2016/03/21
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:
Wang ZP(王知溥)
;
Li F(李飞)
;
Gu HS
;
Yu XL(余西龙)
;
Zhang XY(张新宇)
;
Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:531/223
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Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas
双模态发动机的模态鉴别方法
期刊论文
力学学报, 2015, 期号: 3, 页码: 389-397
Authors:
李飞
;
王知溥
;
余西龙
;
顾洪斌
;
陈立红
;
张新宇
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View/Download:423/74
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Submit date:2015/12/25
双模态冲压发动机
模态鉴别
释热分布
H_2O/CO_2污染对RP-3航空煤油着火特性的影响
期刊论文
推进技术, 2015, 卷号: 36, 期号: 3, 页码: 336-344
Authors:
梁金虎
;
王苏
;
张灿
;
张胜涛
;
岳连捷
;
范秉诚
;
张新宇
;
崔季平
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View/Download:230/61
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Submit date:2015/12/25
污染效应
着火延时
煤油
H2o
Co2
激波管
An energy integral method analysis of preferred modes and the spreading rates of supersonic circular jets
会议论文
10th Asia-Pacific Conference on Combustion, ASPACC 2015, Beijing, China, July 19, 2015 - July 22, 2015
Authors:
Yu DH
;
Gu HB(顾洪斌)
;
Zhang P
;
Zhang, Peng (pengzhang.zhang@polyu.edu.hk)
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Submit date:2017/05/05
Axisymmetric Jet
Flow Parameters
Linear Frequency Response
Mixing Enhancement
Periodic Excitations
Supersonic Circular Jet
Supersonic Combustion
Supersonic Jets
壁温对激波-湍流边界层干扰的影响规律研究
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
朱兴坤
;
于长平
;
李新亮
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View/Download:304/111
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Submit date:2016/08/16
湍流边界层
壁温
恢复温度
绝热壁
压缩性效应
直接数值模拟
半经验公式
湍动能
过渡区
理论分析