Modeling of Ice Accretion over Aircraft Wings Using a Compressible OpenFOAM Solver

<div>Cross-sectional distributions of vorticity magnitude at different downstream locations for the clean (a) and iced (b) wing. 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International Journal of Aerospace Engineering

fig13

Figure 13

Figure 13: Modeling of Ice Accretion over Aircraft Wings Using a Compressible OpenFOAM Solver 