Anti-icing fluid performance on substrates with different thermal conductivity and roughness

The performance of aircraft anti-icing fluids reduces unusually on aviation composites. It is unclear whether this is due to low substrate thermal conductivity or hydrophobicity. Therefore, we considered experimentally the performance of Newtonian and non-Newtonian aircraft anti-icing fluids on substrates with thermal conductivities from 0.17 to 252 W/m.K. It was found that the decrease of substrate thermal conductivity promotes the freezing of Newtonian and low viscous Non-Newtonian fluids compared to the thicker Non-Newtonian one. The thermal conductivity effect can be explained by the competition of two heat transfer processes: heat accumulation and the transfer of latent heat. Thus, Newtonian and low viscous Non-Newtonian aircraft anti-icing fluids must be defined on aviation composites together with substrate thermal conductivity, wettability, and roughness.

Automated summary

The performance of aircraft anti-icing fluids on aviation composites is affected by substrate thermal conductivity and hydrophobicity. Decreased substrate thermal conductivity promotes easier freezing of Newtonian and low viscous non-Newtonian fluids. Therefore, the choice of aircraft anti-icing fluids for aviation composites should consider substrate thermal conductivity, wettability, and roughness.