CFD Model for Aircraft Ground Deicing: Verification and Validation of an Extended Enthalpy-Porosity Technique in Particulate Two Phase Flows
Researchers have focused in the last five years on modelling the aircraft ground deicing process using CFD (computational fluid dynamics) in order to reduce its costs and pollution. As preliminary efforts, those studies did not model the ice melting nor the diffusion between deicing fluids and water...
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| Published in: | Fluids (Basel) Vol. 6; no. 6; p. 210 |
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| Main Authors: | , |
| Format: | Journal Article |
| Language: | English |
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Basel
MDPI AG
01.06.2021
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| ISSN: | 2311-5521, 2311-5521 |
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| Abstract | Researchers have focused in the last five years on modelling the aircraft ground deicing process using CFD (computational fluid dynamics) in order to reduce its costs and pollution. As preliminary efforts, those studies did not model the ice melting nor the diffusion between deicing fluids and water resulting from the melting process. This paper proposes a CFD method to simulate this process filling these gaps. A particulate two-phase flow approach is used to model the spray impact on ice near the contaminated surface. Ice melting is modelled using an extended version of the enthalpy-porosity technique. The water resulting from the melting process is diffused into the deicing fluid forming a single-phase film. This paper presents a new model of the process. The model is verified and validated through three steps. (i) verification of the species transport. (ii) validation of the transient temperature field of a mixture. (iii) validation of the convective heat transfer of an impinging spray. The permeability coefficient of the enthalpy-porosity technique is then calibrated. The proposed model proved to be a suitable candidate for a parametric study of the aircraft ground deicing process. On the validation test cases, the precision of heat transfer prediction exceeds 88%. The model has the ability of predicting the deicing time and the deicing fluid quantities needed to decontaminate a surface. |
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| AbstractList | Researchers have focused in the last five years on modelling the aircraft ground deicing process using CFD (computational fluid dynamics) in order to reduce its costs and pollution. As preliminary efforts, those studies did not model the ice melting nor the diffusion between deicing fluids and water resulting from the melting process. This paper proposes a CFD method to simulate this process filling these gaps. A particulate two-phase flow approach is used to model the spray impact on ice near the contaminated surface. Ice melting is modelled using an extended version of the enthalpy-porosity technique. The water resulting from the melting process is diffused into the deicing fluid forming a single-phase film. This paper presents a new model of the process. The model is verified and validated through three steps. (i) verification of the species transport. (ii) validation of the transient temperature field of a mixture. (iii) validation of the convective heat transfer of an impinging spray. The permeability coefficient of the enthalpy-porosity technique is then calibrated. The proposed model proved to be a suitable candidate for a parametric study of the aircraft ground deicing process. On the validation test cases, the precision of heat transfer prediction exceeds 88%. The model has the ability of predicting the deicing time and the deicing fluid quantities needed to decontaminate a surface. |
| Author | Ernez, Sami Morency, François |
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| Cites_doi | 10.1016/S0035-3159(99)80013-0 10.1016/j.ijheatmasstransfer.2006.05.007 10.1016/j.jcp.2007.01.019 10.2514/1.T5428 10.2514/1.5594 10.1080/713838171 10.1016/0017-9310(87)90317-6 10.1016/j.proeng.2015.01.349 10.1007/978-3-319-99693-6 10.2514/2.2613 10.3390/en12224360 10.1177/1687814016646976 10.1016/j.ijheatmasstransfer.2010.04.025 10.1007/s00231-013-1131-1 10.1002/aic.690250513 10.3390/w12092581 10.1016/j.expthermflusci.2010.02.010 10.1016/j.ijheatmasstransfer.2007.08.010 10.1016/S0301-9322(96)90004-X 10.1007/978-3-642-20598-9 10.1108/HFF-09-2018-0534 10.2514/6.1993-170 |
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| SubjectTerms | Aerodynamics Aircraft aircraft ground deicing Computational fluid dynamics Convective heat transfer Decontamination Deicers Deicing Enthalpy Fluid dynamics Heat transfer Hydrodynamics Ice melting impinging jet Mathematical models Melting Methods Multiphase flow Numerical analysis particulate two-phase flows Permeability coefficient Porosity Predictions Solidification Solids species diffusion Temperature distribution Two phase flow Verification |
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| Title | CFD Model for Aircraft Ground Deicing: Verification and Validation of an Extended Enthalpy-Porosity Technique in Particulate Two Phase Flows |
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