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High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors:  Yang L;  岳连捷;  张启帆;  张新宇
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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
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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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Investigation of high-order cell-centered finite difference method for aeroacoustics 会议论文
25th AIAA/CEAS Aeroacoustics Conference, 2019, Delft, Netherlands, May 20, 2019 - May 23, 2019
Authors:  Jin Y;  Liao F(廖飞);  Cai JS;  Morris PJ
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A novel method of cooling channel optimization for active-cooled structure using the calculus of variations 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:  Li X(李轩);  Lu Y(陆阳);  Wu K(吴坤);  Fan XJ(范学军)
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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)
View  |  Adobe PDF(1173Kb)  |  Favorite  |  View/Download：481/232  |  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  
Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion 会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
Authors:  Liu CY;  Zhang J(张健)
View  |  Adobe PDF(414Kb)  |  Favorite  |  View/Download：247/92  |  Submit date：2018/11/08
Oxygen  Diluted environments  Monotonic trend  Partial premixing  Stabilization mechanisms  Transition process  Transitional flames  Transitional process  Turbulent combustion  
Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
Authors:  Gan JY;  Shen YQ(申义庆);  Zha GC
View  |  Adobe PDF(555Kb)  |  Favorite  |  View/Download：309/100  |  Submit date：2017/05/05
Central Differencing  Drag Prediction  Finite Difference Scheme  High  Order Scheme  Line Relaxation  Mesh Refinement  Trailing Edges  Turbulent Models  
Experimental Investigation of Dynamic Fracture Behaviors of Polymethyl Methacrylate 会议论文
23rd World Forum on Advanced Polymeric Materials (POLYCHAR), Univ Nebraska Lincoln, Lincoln, NE, MAY 11-15, 2015
Authors:  Gao GY;  Zhou J;  Li Z;  Li, Z (reprint author), Peking Univ, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China.;  Li, Z (reprint author), Peking Univ, Coll Engn, Beijing 100871, Peoples R China.
View  |  Adobe PDF(2033Kb)  |  Favorite  |  View/Download：271/112  |  Submit date：2017/05/12
Crack Interaction  Fracture  Optical Method Of Caustics  Semi-circular Bending  Toughness  Stress Intensity Factor  Semicircular Bend Technique  Crack-propagation  Brittle-fracture  Caustic Analysis  Specimen  Pmma  Parallel  Field  Rock  
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)  |  Favorite  |  View/Download：504/183  |  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