Fig. 32From: Numerical Simulation of Supercooled Droplets Deformation, Impingement and Freezing for In-Flight IcingComparison of experimental and numerical results (a) We = 2.64 (Li and Zhang 2019), (b) We = 10 (Chen et al. 2011), (c) We = 51.6 (Abolghasemibizaki and Mohammadi 2018)Back to chapter page