Anodizing/spraying process | F-SiO2, PDMS/ Aluminum plate | 26.3 kPa vs 821.9 kPa at -20oC | 276.2 s vs 4.8 s at -15oC | 30 icing / deicing cycles, 12.4 ms droplet dynamic bounce time | [52] |
Laser etching /hydrothermal/chemical modification | FAS-17 modifies the TiO2 / Ti6Al4V Titanium alloy plate | 70 kPa vs 700 kPa at -10oC | 765 s vs 13.2 s at -10oC | 17 ms droplet dynamic bounce time | [42] |
Template method | CF, PEEK, FAS-17/ Aluminum plate | 30.5 kPa vs 413 kPa at -20oC | 514 s vs 54 s at -20oC | Simple preparation and high mechanical durability | [53] |
Two-step spraying method | PU, DE@HD-POS/ Aluminum plate | 50.8 kPa vs 819 kPa at -10oC | 315 s vs 52 s at -15oC | 13.25 ms droplet dynamic bounce time | [54] |
Chemical etching / modification | AgNO3, stearic acid/ Tinplate | | 621s vs 295 s at -15oC | 10 icing / deicing cycles | [55] |
One-step spraying method | F-SiO2, FSC/ Tinplate | 27 kPa vs 1600 kPa at -20oC | 1765 s vs 170 s at -20oC | 20 icing / deicing cycles, high peeling resistance, wear resistance and durability | [56] |
Phase separation method | SAN, SiO2/ ASA resin | | 5040 s vs 540 s at -10oC | Good self-cleaning performance | [57] |
One step impregnation method | PVDF, SiO2/ Aluminum plate | Reduced 40% at -20oC | 273 s vs 65 s at -20oC | 18 icing / deicing cycles | [58] |
Layer upon layer self-assembly method | TMES-SiO2/ Aerospace composite board | 53.6 kPa vs 335.3 kPa at -15oC | 195 s vs 77 s at -15oC | High mechanical durability and wear resistance | [59] |