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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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姜宗林 [3]
刘云峰 [2]
岳连捷 [2]
张启帆 [2]
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Indexed By:EI
Date Issued:2021
Language:英语
Community:高温气体动力学国家重点实验室
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Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition
期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:
Zhang WS(张文硕)
;
Zhang, Zijian
;
Jiang ZL(姜宗林)
;
Han X(韩信)
;
Liu, Yunfeng
;
Wang, Chun
Adobe PDF(15045Kb)
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View/Download:259/29
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Submit date:2022/01/24
Hysteresis of Shock Train Movement in the Isolator with a Ramp
期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
Authors:
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang P
;
Zhao QJ
Adobe PDF(2961Kb)
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Submit date:2022/02/17
Atomization of misaligned impinging liquid jets
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 15
Authors:
Zhang, Chenwei
;
Zhang ZY(张振宇)
;
Wu K(吴坤)
;
Xia, Xi
;
Fan XJ(范学军)
Adobe PDF(15401Kb)
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Submit date:2022/01/12
AMP Exception
AMP Exception
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy
期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
Authors:
Fang SH(方思晗)
;
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Li RJ(李仁杰)
;
Li, Jing
;
Zhang, Zhedian
;
Liu, Yan
;
Yu XL(余西龙)
Adobe PDF(4367Kb)
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Submit date:2021/08/03
Tunable diode laser absorption spectroscopy
Hybrid rocket motor
Temperature
Partial pressure
Combustion efficiency
Parametric Study on Lateral–Directional Stability of Hypersonic Waverider
期刊论文
AIAA Journal, 2021, 卷号: 59, 期号: 8, 页码: 3025-3042
Authors:
刘文
;
张陈安
;
Wang Xiao-Peng
;
Li Jin-Jie
;
王发民
Adobe PDF(7528Kb)
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Submit date:2021/08/30
High-Throughput Screening of Nitrogen-Coordinated Bimetal Catalysts for Multielectron Reduction of CO2 to CH4 with High Selectivity and Low Limiting Potential
期刊论文
JOURNAL OF PHYSICAL CHEMISTRY C, 2021, 卷号: 125, 期号: 13, 页码: 7155-7165
Authors:
Wang Shuo
;
Li Lei
;
Li Jing
;
Yuan Chengzong
;
Kang Yao
;
Hui Kwan San
;
Zhang Jintao
;
Bin F(宾峰)
;
Fan Xi
;
Chen Fuming
;
Hui Kwun Nam
Adobe PDF(6747Kb)
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Submit date:2021/05/17
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Electric-Field-Driven Ion Emission from the Free Surface of Room Temperature Ionic Liquids
期刊论文
JOURNAL OF PHYSICAL CHEMISTRY LETTERS, 2021, 卷号: 12, 期号: 1, 页码: 211-216
Authors:
Zhang, Fei
;
Jiang XK(蒋玺恺)
;
Chen, Gaofeng
;
He, Yadong
;
Hu, Guoqing
;
Qiao, Rui
Adobe PDF(2456Kb)
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Submit date:2021/03/30
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(8067Kb)
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View/Download:404/71
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation