In polar or cold marine environments, icing of inertial separator blades in the air intake systems of ships and offshore platforms can obstruct the blade channels, severely compromising their stable operation. This study investigates the effects of varying inflow conditions and droplet salinity on the icing and aerodynamic characteristics of inertial separator blades by modifying the physical properties of droplets. The results indicate that droplet salinity and inflow conditions significantly affect the blade icing shape, particularly causing the icing region near the second vane to shift markedly downstream as inflow velocity increases. For saline droplets, higher inflow velocity and liquid water content exert a more pronounced effect on the icing characteristics of blades. At the second vane, as salinity increases from 0.00 % to 2.67%, the decay rate of maximum icing thickness reaches 0.131 under the inflow velocity of 7 m/s and liquid water content of 1.0 g/m³, whereas under lower inflow velocity and liquid water content, the decay rates are 0.079 and 0.110, respectively. Under the inflow velocity of 7 m/s and liquid water content of 1.0 g/m³, the total icing area decreases by approximately 22.24 % when salinity increases from 0.00 % to 2.67 %; the reduction is approximately 19.61 % under lower inflow velocity and about 11.62 % under lower liquid water content. With increasing droplet salinity, the total pressure loss induced by blade icing gradually decreases, and higher inflow velocity and liquid water content further amplify this effect.
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