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Numerical procedure for the simulation of an electro-thermal anti-icing system

Antonio Carozza (Department of Fluid Mechanics, CIRA, Capua, Italy)
Francesco Petrosino (Department of Fluid Mechanics, CIRA, Capua, Italy)
Giuseppe Mingione (Department of Fluid Mechanics, CIRA, Capua, Italy)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 29 April 2022

Issue publication date: 4 August 2022

248

Abstract

Purpose

This study aims to couple two codes, one able to perform icing simulations and another one capable to simulate the performance of an electrothermal anti-icing system in an integrated fashion.

Design/methodology/approach

The classical tool chain of icing simulation (aerodynamics, water catch and impact, mass and energy surface balance) is coupled to the thermal analysis through the surface substrate and the ice thickness. In the present approach, the ice protection simulation is not decoupled from the ice accretion simulation, but a single computational workflow is considered.

Findings

A fast approach to simulate advanced anti-icing systems is found in this study.

Originality/value

This study shows the validation of present procedure against literature data, both experimental and numerical.

Keywords

Citation

Carozza, A., Petrosino, F. and Mingione, G. (2022), "Numerical procedure for the simulation of an electro-thermal anti-icing system", Aircraft Engineering and Aerospace Technology, Vol. 94 No. 8, pp. 1433-1448. https://doi.org/10.1108/AEAT-07-2021-0222

Publisher

:

Emerald Publishing Limited

Copyright © 2022, Emerald Publishing Limited

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