2021
DOI: 10.1016/j.icheatmasstransfer.2021.105698
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Anti-icing fluids interaction with surfaces: Ice protection and wettability change

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Cited by 12 publications
(5 citation statements)
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“…The SH coating was exposed to icing/deicing cycling (IWT), rain erosion, and accelerated aging test, and the results were compared with those from tests performed on SH TiO 2 /stearic acid and commercial hydrophobic fluoropolymer. The IWT test conditions were T = −10 • C with air speed of 43 m/s and LWC of 0.5 g/m 3 . At the end of the study, it was possible to affirm that the prepared SH coating was resistant to UV exposure, and could resist up to 6000 water droplets impact at 165 m/s and especially started to degrade after 170 icing/deicing cycles resulting in the coating with the best performance.…”
Section: Shs Tested In Flight Conditionsmentioning
confidence: 99%
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“…The SH coating was exposed to icing/deicing cycling (IWT), rain erosion, and accelerated aging test, and the results were compared with those from tests performed on SH TiO 2 /stearic acid and commercial hydrophobic fluoropolymer. The IWT test conditions were T = −10 • C with air speed of 43 m/s and LWC of 0.5 g/m 3 . At the end of the study, it was possible to affirm that the prepared SH coating was resistant to UV exposure, and could resist up to 6000 water droplets impact at 165 m/s and especially started to degrade after 170 icing/deicing cycles resulting in the coating with the best performance.…”
Section: Shs Tested In Flight Conditionsmentioning
confidence: 99%
“…The authors found no direct correlation between the CA and the endurance time and even when a positive result was observed, it was possible that the surface affected the fluid flow off establishing possible negative effects on aerodynamics. A later study setting out to explore this problem is more accurately described in [3]. In this paper, as opposed to [2], the authors provided detailed information about commercial anti-ice fluids (density, viscosity and surface tension) and employed surfaces (Sa, advancing and receding CA).…”
Section: Deicing Fluidsmentioning
confidence: 99%
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“…Chemical fluid, mechanical, thermal, hybrid, and other ice protection methods are widely used in commercial aircraft. The chemical fluid ice protection method removes ice deposits and forms a protective film on airplane surfaces (Grishaev et al, 2021). This method protects aircraft surfaces from icing by lowering the freezing temperature of supercooled water below the ambient temperature by mixing a chemical fluid with supercooled water that has been impinged.…”
Section: Ice Protection Systemsmentioning
confidence: 99%
“…These can be classified into three main groups, namely, anti-icing (to avoid the formation of ice by applying surface engineering methods), de-icing (to remove ice once it is accreted on a surface), and combined anti-icing and de-icing. De-icing relies on various physical principles, including the application of low-temperature freezing liquids, [1] the use of the Joule effect, [2,3] solar actuation and photothermal effects, [4][5][6] the de-icing activation with plasmas, [7] the implementation of plasmonic nanoparticles, [8] the application of bulk or guided ultrasonic sound waves in the kHz range generated by external piezoelectric devices, [9,10] or, as reported very recently, the use of surface acoustic waves (SAWs) with suitable substrates coated with a piezoelectric thin film. [11] In this article, we go a step forward and disclose a series of basic ice-substrate interactions upon activation with bulk acoustic waves (AWs) generated in excited piezoelectric substrates.…”
Section: Introductionmentioning
confidence: 99%