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Open Access

Modelling and analysis of initial icing roughness with fixed-grid enthalpy method based on DPM-VOF algorithm

Jie LIUaPeng KEb( )
Department of Civil Helicopter Research and Development, China Helicopter Research and Development Institute, Tianjin 300000, China
School of Transportation Science and Engineering, Beihang University, Beijing 100191, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Ice particles could form under the continuous impingement of incoming supercooled droplets in icing conditions, which will change the surface roughness to enhance the further heat and mass transfer during icing process. A fixed-grid porous enthalpy method based on the improved Discrete Phase Model (DPM) and Volume of Fluid (VOF) integrated algorithm is developed to solve the multiphase heat transfer problem to give more detailed demonstration of the formation of initial ice roughness. The algorithms to determine the criterion of transformation from DPM to VOF and the allocation of source items during transformation are improved to the general DPM-VOF algorithm. Two verification cases, namely two glycerine-solution droplets impact and single droplet freeze, are conducted to verify the accuracy and reliability of the enthalpy-DPM-VOF method, where the simulation results match well with experiment phenomena. Ice roughness on a NACA0012 airfoil is precisely captured and the effects on convective heat transfer characteristics are preliminarily revealed. The results illustrate that the enthalpy-DPM-VOF method could successfully capture the characteristics of motion and the phase change process of droplet, as well as balance the calculation accuracy and efficiency.

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Chinese Journal of Aeronautics
Pages 168-178

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Cite this article:
LIU J, KE P. Modelling and analysis of initial icing roughness with fixed-grid enthalpy method based on DPM-VOF algorithm. Chinese Journal of Aeronautics, 2022, 35(7): 168-178. https://doi.org/10.1016/j.cja.2021.07.028

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Received: 10 December 2020
Revised: 21 January 2021
Accepted: 04 March 2021
Published: 23 October 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/).