Study on the Thermophysical Properties of Hybrid Nanofluid Based on Aircraft De/Anti-Icing Fluid at Low Temperatures

Subject Areas : meso/micro/nano fabrication

Nasim Nayebpashaee ¹

1 - Department of Metallurgy and Mechanical Engineering,Technology and Engineering Research Center, Standard Research Institute (SRI), Karaj, Iran

Received: 2022-05-26 Accepted : 2022-09-17 Published : 2023-06-01

Keywords: Aircraft De/Anti-Icing Fluid, Concentration Effect, Hybrid Nanofluids, Dynamic Viscosity, Low Temperatures, Thermal conductivity,

Abstract :

This work involves an experimental study of the thermophysical properties of hybrid nanofluids of TiO2 and graphene in a binary mixture of water and ethylene glycol. Hybrid nanofluid samples with different volume fractions (0.05-2.5%) were prepared by dispersing equal volumes of TiO2 and graphene nanoparticles in a binary mixture of water and ethylene glycol in the ratio of 50-50% by volume. The thermal conductivity, surface tension, and dynamic viscosity of the hybrid nanofluids were measured at temperatures ranging from 253 K to 303 K. The experimental results showed that the low concentration samples exhibited shear thinning non-Newtonian behavior, while the high concentration samples exhibited shear thickening non-Newtonian behavior. The measurements showed that the thermal conductivity of the nanofluids increases by up to 41.93% with increasing nanoparticle concentration and temperature. The surface tension improves by 43.61%, 39.77%, and 51.98% at concentrations of 2.5%, 2%, and 2% by volume at temperatures of 258.15 K, 268.15 K, and 283.15 K, respectively. In terms of aircraft deicing fluid performance, the addition of TiO2 and graphene nanoparticles at less than 0.5% by volume contributes to the improvement of aircraft deicing fluid performance.

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