Investigation of the Splashing Phenomenon of Large Droplets for Aviation Safety

2015-01-2100

06/15/2015

Event
SAE 2015 International Conference on Icing of Aircraft, Engines, and Structures
Authors Abstract
Content
In this paper we numerically investigated the impact of large droplets on smooth solid surfaces to understand the splashing mechanism involved in ice accretion due to supercooled large droplets. A Navier-Stokes solver was used to describe the flow field, the moment-of-fluid (MOF) method was used to capture the droplet interface evolution, and the adaptive mesh refinement technique was employed to refine the mesh near the region of interest. We investigated the effect of air on splashing mechanism and confirmed that a low pressure can suppress the droplet splashing. The size distribution of splashed secondary droplets was studied and showed good agreement with experimental results. The effect of surface curvature on the splashing phenomenon was highlighted. Finally, the droplet impact on a NACA 23012 airfoil was studied and the water collection efficiency was investigated.
Meta TagsDetails
DOI
https://doi.org/10.4271/2015-01-2100
Pages
11
Citation
Lian, Y., and Guo, Y., "Investigation of the Splashing Phenomenon of Large Droplets for Aviation Safety," SAE Technical Paper 2015-01-2100, 2015, https://doi.org/10.4271/2015-01-2100.
Additional Details
Publisher
Published
Jun 15, 2015
Product Code
2015-01-2100
Content Type
Technical Paper
Language
English