Numerical Simulation of the Collection Efficiency on Aircraft Ground Icing
In this paper, a numerical approach to calculate the droplet collection efficiency on airfoil was presented. Two-dimensional wind field simulations have been performed based on the Reynolds Averaged Navier-Stocks (RANS) equations. The droplet trajectories are calculated by Lagrangian method. Particular attention is paid to the study of collection efficiency of droplets with different diameters and velocities for a NACA0012 airfoil.
aircraft ground icing collection efficiency wind field numerical simulation
Xu Dan-dan Xing Zhi-wei Wang Li-wen
School of Mechanical Engineering Tianjin Univerisity Tianjin, China Aeronautical Automation College Civil Aviation University of China Tianjin, China School of Mechanical Engineering Tianjin Univerisity Aeronautical Automation College Civil Aviation
国际会议
哈尔滨
英文
2408-2411
2011-08-12(万方平台首次上网日期,不代表论文的发表时间)