Wall-Droplet Interaction Modeling and Comparative Study on Deformation Models for the Improvement of Icing Analysis Under SLD Conditions

被引:3
作者
Bae, Jinkyu [1 ]
Yee, Kwanjung [1 ]
机构
[1] Seoul Natl Univ, Dept Mech & Aerosp Engn, Seoul, South Korea
关键词
Aircraft Icing; SLD; MVD; Droplet-Wall Interaction; Deformation;
D O I
10.5139/JKSAS.2020.48.4.255
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Under SLD conditions, due to the large size of droplets, physical phenomena such as wall-droplet interaction and deformation have a significant effect on the icing process. Accordingly, many studies have been conducted in order to computationally simulate SLD effects. As one of the efforts, post-processing method have been proposed to describe wall-droplet interaction effect, which modified collection efficiency using Wright model. However, since the model doesn't properly consider the wall condition, it still overestimated collection efficiency and impingement limit. To solve this problem, impingement areas were divided into 3 different regions, and the post-processing method was introduced with the new wall-droplet interaction model developed based on Bai and Gosman rebound model. In order to consider the effect of deformation, the most suitable model was selected by comparing the deformation models used in the various icing codes. As a result, the modified post-processing method showed improved accuracy in predicting the impingement limits and collection efficiency by further estimating mass flux loss due to rebound, and it was observed that the result was the closest to the experimental data when the deformation effect was included by using Wiegand model.
引用
收藏
页码:255 / 267
页数:13
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