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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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Coupling noise analysis of force and temperature on Taiji-1 interferometer
会议论文
1st Optics Frontier Conference 2021, Hangzhou, 24 April 2021 到 26 April 2021
Authors:
Wang J(王娟)
;
Deng XQ(邓小芹)
;
Yang R(杨然)
;
Luo ZR(罗子人)
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Submit date:2021/11/30
Force noise
Interferometry
Noise coupling
Taiji-1
Temperature noise
Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser
会议论文
2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020
Authors:
Fang SH(方思晗)
;
Wang ZZ(王泽众)
;
Li RJ(李仁杰)
;
Zhang ZL(张泽林)
;
Lin X(林鑫)
;
Li F(李飞)
;
Yu XL(余西龙)
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Submit date:2021/06/11
concentration
hybrid rocket motor
nozzle exit
temperature
Tunable diode laser absorption spectroscopy (TDLAS)
water vapor
Oxidation of Ammonia and NO Formation during NH3/CO Post-combustion
会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:
Wei XL(魏小林)
;
Zhang YF(张玉锋)
;
Zhao J(赵京)
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Submit date:2019/11/20
Chemical mechanism
Entrained Flow Reactor
Hydrocarbon fuel
Hydrogen carriers
Ignition energies
NO and CO emissions
Post
combustion
Temperature increase
A molecular dynamics simulation on the oxidation of core-shell aluminum nanoparticles in oxygen and water environments
会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:
Chu QZ
;
Liao LJ(廖丽涓)
;
Shi BL
;
Luo KH
;
Wang NF
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Submit date:2019/11/20
Aluminum nanoparticles
Concentration distributions
Heat and mass transfer process
Heat transfer efficiency
Molecular dynamics simulations
Oxidation mechanisms
Particle temperature
Structure evolution
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(xfan@imech.ac.cn)
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Submit date:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
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Submit date:2018/01/16
Combustion
Diesel Engines
Hydrogen
Large Eddy Simulation
Spacecraft
Stabilization
Supersonic Aircraft
Temperature Measurement
Wall Flow
The effects of air vitiation on the supersonic turbulent channel flow using direct numerical simulation
会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:
Chen XP
;
Li XP(李晓鹏)
;
Dou HS
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Submit date:2017/05/05
Mass Fraction
Mean Velocities
Nondimensional
Reynolds Analogy
Static Temperature
Statistical Characteristics
Temperature Correlation
Turbulent Channel Flows
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
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
Adobe PDF(1195Kb)
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Submit date:2016/07/01
Adiabatic Flame Temperature
Combustion
Directed Graphs
Flow Separation
Heat Flux
Kerosene
Large Eddy Simulation
Musculoskeletal System
Real Time Systems
Sensitivity Analysis
Spacecraft
Transients
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Ma SG(马素刚)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Zhong, Fengquan (fzhong@imech.ac.cn)
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Submit date:2017/05/05
Combustion Pro
Cess
Directed Relation Graph
Dynamic Evolution
Fuel Injection Velocities
Kinetic Mechanism
Reduced Mechanisms
Temperature Profiles
Temporal And Spatial Evolutions