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A single-camera synthetic schlieren method for measuring two-dimensional liquid surfaces
会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
Authors:
Xu D(徐多)
;
Li HX
;
Avila M
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Submit date:2021/11/30
Numerical simulation of 30p30n multi-element airfoil using delayed detached-eddy simulation
会议论文
AIAA AVIATION 2020 FORUM, 15 June 2020 through 19 June 2020
Authors:
Jin Y
;
廖飞, Cai JS
Adobe PDF(4611Kb)
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Submit date:2021/06/11
In-situ investigation on fatigue behaviors of Ti-6Al-4V manufactured by selective laser melting
会议论文
19th International Colloquium on Mechanical Fatigue of Metals (ICMFM), Univ Porto, Fac Engn, Porto, PORTUGAL, SEP 05-07, 2018
Authors:
Qian GA(钱桂安)
;
Jian,Zhimo
;
Pan XN(潘向南)
;
Berto,Filippo
Adobe PDF(2875Kb)
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Submit date:2022/11/24
Selective laser melting
In-situ SEM
Ti-6Al-4V
Low cycle fatigue
Crack propagation
Contribution of Cavitation Generation to Shock Wave Sterilization Effects in a Narrow Water Chamber
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:
Wang JZ(王静竹)
;
Abe, A.
;
Koita, T.
;
Sun, M.
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Submit date:2023/03/17
Total internal reflection imaging ellipsometry biosensor: Its principle and applications
会议论文
31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018
Authors:
Wang T(王婷)
;
Ma K(马克)
;
Liu W(刘巍)
;
Jin G(靳刚)
;
Niu Y(牛宇)
Adobe PDF(1508Kb)
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Submit date:2020/11/20
Evanescent Wave
Imaging Ellipsometry
Label-free biosensor
Surface Plasmon Resonance
Total Internal Reflection
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Yao W(姚卫)
;
Li B(李波)
Adobe PDF(1665Kb)
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Submit date:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions
会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
Authors:
Prapamonthon P
;
Yin B(银波)
;
Yang GW(杨国伟)
;
Zhang MH(张莫晗)
Adobe PDF(2782Kb)
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Submit date:2020/11/20
Aerothermal condition
Cooling effectiveness
Cooling performance
Thermal sensitivity
Turbine vane
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)
Adobe PDF(1173Kb)
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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
Development of zone flamelet model for scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(623Kb)
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View/Download:243/79
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Submit date:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
Development of zone flamelet modelfor scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(832Kb)
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View/Download:262/78
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Submit date:2018/11/08
Combustion
Cost benefit analysis
Costs
Mixtures
Ramjet engines
Supersonic aircraft
Computational costs
Equivalence ratios
Local flow conditions
Scramjet combustors
Statistics approaches
Supersonic combustion
Supersonic combustors
Turbulent combustion