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A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  Favorite  |  View/Download：182/50  |  Submit date：2022/07/04
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
Adobe PDF(4040Kb)  |  Favorite  |  View/Download：315/169  |  Submit date：2021/11/30
Effects of Statistical Characteristics for Deep-Sea Sediments on Lateral Buckling of HPHT Pipelines 会议论文
The 14th ISOPE PACOMS Symposium, Dalian, China, 2020-11-22
Authors:  Shi YM(师玉敏);  Gao FP(高福平);  Liu JT;  ; Zhu YS
Favorite  |  View/Download：102/0  |  Submit date：2021/01/28
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)
Adobe PDF(1569Kb)  |  Favorite  |  View/Download：230/68  |  Submit date：2021/06/11
concentration  hybrid rocket motor  nozzle exit  temperature  Tunable diode laser absorption spectroscopy (TDLAS)  water vapor  
A robust aerodynamic optimization design for airfoil based on interval uncertainty analysis method 会议论文
ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019, San Francisco, CA, United states, July 28, 2019 - August 1, 2019
Authors:  Song X(宋鑫);  Zheng GN(郑冠男);  Yang GW(杨国伟)
Favorite  |  View/Download：129/0  |  Submit date：2020/11/20
Adaptive MOPSO  DFFD  Geometric uncertainty  Interval analysis  Kriging model  Robust design optimization  
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)  |  Favorite  |  View/Download：199/73  |  Submit date：2020/11/20
Aerothermal condition  Cooling effectiveness  Cooling performance  Thermal sensitivity  Turbine vane  
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)
Adobe PDF(4139Kb)  |  Favorite  |  View/Download：304/68  |  Submit date：2019/04/19
MOLECULAR DYNAMICS SIMULATIONS ON THE TENSILE DEFORMATION AND FAILURE OF A POLYETHYLENE/COPPER INTERFACE 会议论文
ASME International Design Engineering Technical Conferences (IDETC) / Computers and Information in Engineering Conference (CIE), Quebec City, CANADA, AUG 26-29, 2018
Authors:  Liao LJ(廖丽涓);  Meng CY(孟昶宇);  Huang CG(黄晨光)
Adobe PDF(1821Kb)  |  Favorite  |  View/Download：291/103  |  Submit date：2019/04/19
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)  |  Favorite  |  View/Download：480/232  |  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)
View  |  Adobe PDF(1249Kb)  |  Favorite  |  View/Download：333/101  |  Submit date：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow