论文部分内容阅读
The flow around a circular cylinder is numerically simulated based on a dynamic Smagorinsky Large Eddy Simulation(LES)model [1].
Large eddy simulation of high Reynolds number flow around a near wall cylinder
【摘 要】
：
The flow around a circular cylinder is numerically simulated based on a dynamic Smagorinsky Large Eddy Simulation(LES)model [1].
【机 构】
：
SchoolofCivil,EnvironmentalandMiningEngineering,TheUniversityofWesternAustralia,Crawley,WA6009,Austr
【出 处】
：
第14届亚洲显示会议(The 14th Asian Symposium on Visualization)
【发表日期】
：
2017年5期
其他文献
Experimental Investigation of Thermo-Hydraulic Characteristics in a Heat Exchanger Tube with Incline
Heat exchangers is commonly applied in various thermal industries.Improving the thermal performance is an important issue for energy savings and heat exchan
An experimental investigation on the impact and icing processes of a water droplet on curved cold su
The present study experimentally investigated the impact and icing processes of a water droplet on different curved cold surfaces.
Heat exchangers have wide range of applications from industrial fields and engineering devices such as power plant,air conditioning,refrigeration,food proce
Axisymmetric thermocapillary interaction of two drops in a vertical temperature gradient is investigated experimentally on the ground.
An experimental study on the lift/drag forces and visualization on the wing tip vortices of a NACA4412 wing in adjacent to a sine wavy surface is introduced
Drying is the process for removing moisture from product by evaporation.
Boundary layer and miixng layer are common elementary flow in the field of engineering,however,little kown in the kind of confluent flow of boundary/mixing
Heat transfer enhancement techniques have been developed and widely utilized in several engineering applications,such as refrigeration,heat exchanger and fo
Convection exists widely in the nature.The researches of turbulent thermal convection in physics and flow characteristics,which can deepen the understanding
High Speed Schlieren Visualization of Hypersonic Separated Flow Induced by a Perpendicular Blunt Fin
Shock wave/boundary layer interaction,which often accompanied by separation,is a common feature of high speed flow over flight vehicles.Previous research re