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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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Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model
会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
Authors:
Yao W(姚卫)
;
Chen L(陈留)
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Submit date:2021/06/11
Heat release and temperature diagnostics for swirling flames using chemiluminescence and absorption tomography
会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:
Lin X(林鑫)
;
Wang KL(王宽亮)
;
Li F(李飞)
;
Yu XL(余西龙)
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Adobe PDF(495Kb)
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View/Download:240/58
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Submit date:2019/11/06
Dynamics character of swirling flame investigated by OH and CH2O planar laser-induced fluorescence
会议论文
5th International Symposium on Laser Interaction with Matter (LIMIS), Changsha, PEOPLES R CHINA, NOV 11-13, 2018
Authors:
Yan H(严浩)
;
Zhang SH(张少华)
;
Yu XL(余西龙)
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Submit date:2019/11/20
laser
induced fluorescence
swirling flame
OH
CH2O
proper orthogonal decomposition
Optical Diagnostics of Swirling Flame by Simultaneous Planar Laser-induced Fluorescence and High-speed Chemiluminescence Imaging of OH Radical
会议论文
PhotonIcs and Electromagnetics Research Symposium - Spring (PIERS-Spring), Rome, ITALY, JUN 17-20, 2019
Authors:
Yan H(严浩)
;
Zhang SH(张少华)
;
Wang FY(王方仪)
;
Yu XL(余西龙)
Adobe PDF(1166Kb)
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Submit date:2022/11/24
AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL
会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
;
Teng HH(滕宏辉)
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View/Download:290/62
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Submit date:2019/04/19
Experimental Studies of Film Cooling in Supersonic Combustors
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Fan C(樊川)
;
Wang J(王晶)
;
Fan XJ(范学军)
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Submit date:2018/01/16
Combustion
Combustors
Coolants
Kerosene
Spacecraft
Supersonic Aerodynamics
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Wang Q(汪球)
;
Li JW
;
Lu P
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
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  |  
Adobe PDF(679Kb)
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Submit date:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis
Performance of a detonation driven shock tunnel
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li JW
;
Wang Q(汪球)
;
Zhao W(赵伟)
;
Lu P
;
Tan YX
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Adobe PDF(468Kb)
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Submit date:2018/01/16
Detonation
Gas Dynamics
Hypersonic Flow
Shock Tubes
Supersonic Aerodynamics
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:
Wang YP
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, YP (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:2016/06/28
Plasma Assisted Low Temperature Combustion
会议论文
22nd International Symposium on Plasma Chemistry (ISPC 22), Antwerp, BELGIUM, JUL 05-10, 2015
Authors:
Ju YG
;
Lefkowitz JK
;
Reuter CB
;
Won SH
;
Yang XL
;
Yang S
;
Sun WT
;
Jiang ZL(姜宗林)
;
Chen Q
;
Ju, YG (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
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Submit date:2017/05/04
Plasma Assisted Combustion
Low Temperature Chemistry
Kinetics
Cool Flames
S-curve Transition
Nonequilibrium Plasma
Saturated-hydrocarbons
Diffusion Flames
Pulsed Discharge
Ignition
Mixtures
Oxidation
Kinetics
Enhancement