会议专题

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

2011 International Conference on Electronic & Mechanical Engineering and Information Technology(EMEIT 2011)(2011年机电工程与信息技术国际会议)

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)