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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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Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
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Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp 会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
Authors:  Tong FL(童福林);  Li XL(李新亮);  Duan, Yanhui;  Yu ZP(于长平);  Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Concave Surface Curvature  Adverse Pressure-gradient  Large-eddy Simulation  Reynolds-number  Near-wall  Flows  Separation  Vortices  Models  
Large-eddy simulation of turbulent preferential concentration and collision of bidisperse heavy particles in isotropic turbulence 会议论文
1st International Workshop on Computational Particle Technology, Suzhou, PEOPLES R CHINA, MAR, 2016
Authors:  Chen JC(陈进财);  Jin GD(晋国栋);  Jin, GD (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
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Direct Numerical Simulations  Space-time Correlations  Inertial Particles  Approximate Deconvolution  Cloud Droplets  Fluidized-bed  Flow  Model  Motion  Particle-laden Turbulence  Large-eddy Simulation  Subgrid Scale Motion  Bidisperse Particles  Preferential Concentration  Collision Rate Attenuation