Numerical Simulation of Unsteady Conjugate Heat Transfer of Electrothermal Deicing Process
A novel 3-D unsteady model of in-flight electrothermal deicing process is presented in this paper to simulate the conjugate mass and heat transfer phenomena of water film runback, phase change, and solid heat conduction. Mathematical models of water film runback and phase change are established and...
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2018/5362541 |
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doaj-ced36cdfc9f6404f85652091f19c881e2020-11-24T22:20:43ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742018-01-01201810.1155/2018/53625415362541Numerical Simulation of Unsteady Conjugate Heat Transfer of Electrothermal Deicing ProcessZuodong Mu0Guiping Lin1Xiaobin Shen2Xueqin Bu3Ying Zhou4Laboratory of Fundamental Science on Ergonomics and Environmental Control, Beihang University, Beijing 100191, ChinaLaboratory of Fundamental Science on Ergonomics and Environmental Control, Beihang University, Beijing 100191, ChinaLaboratory of Fundamental Science on Ergonomics and Environmental Control, Beihang University, Beijing 100191, ChinaLaboratory of Fundamental Science on Ergonomics and Environmental Control, Beihang University, Beijing 100191, ChinaLaboratory of Fundamental Science on Ergonomics and Environmental Control, Beihang University, Beijing 100191, ChinaA novel 3-D unsteady model of in-flight electrothermal deicing process is presented in this paper to simulate the conjugate mass and heat transfer phenomena of water film runback, phase change, and solid heat conduction. Mathematical models of water film runback and phase change are established and solved by means of a loosely coupled method. At the current time step, solid heat conduction, water film runback, and phase change are iteratively solved until the heat boundary condition reaches convergence, then the temperature distribution and ice shape at the moment are obtained, and the calculation of the next time step begins subsequently. A deicing process is numerically simulated using the present model following an icing tunnel experiment, and the results match well with those in the literatures, which validate the present model. Then, an in-flight deicing process is numerically studied to analyze the effect of heating sequence.http://dx.doi.org/10.1155/2018/5362541 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Zuodong Mu Guiping Lin Xiaobin Shen Xueqin Bu Ying Zhou |
spellingShingle |
Zuodong Mu Guiping Lin Xiaobin Shen Xueqin Bu Ying Zhou Numerical Simulation of Unsteady Conjugate Heat Transfer of Electrothermal Deicing Process International Journal of Aerospace Engineering |
author_facet |
Zuodong Mu Guiping Lin Xiaobin Shen Xueqin Bu Ying Zhou |
author_sort |
Zuodong Mu |
title |
Numerical Simulation of Unsteady Conjugate Heat Transfer of Electrothermal Deicing Process |
title_short |
Numerical Simulation of Unsteady Conjugate Heat Transfer of Electrothermal Deicing Process |
title_full |
Numerical Simulation of Unsteady Conjugate Heat Transfer of Electrothermal Deicing Process |
title_fullStr |
Numerical Simulation of Unsteady Conjugate Heat Transfer of Electrothermal Deicing Process |
title_full_unstemmed |
Numerical Simulation of Unsteady Conjugate Heat Transfer of Electrothermal Deicing Process |
title_sort |
numerical simulation of unsteady conjugate heat transfer of electrothermal deicing process |
publisher |
Hindawi Limited |
series |
International Journal of Aerospace Engineering |
issn |
1687-5966 1687-5974 |
publishDate |
2018-01-01 |
description |
A novel 3-D unsteady model of in-flight electrothermal deicing process is presented in this paper to simulate the conjugate mass and heat transfer phenomena of water film runback, phase change, and solid heat conduction. Mathematical models of water film runback and phase change are established and solved by means of a loosely coupled method. At the current time step, solid heat conduction, water film runback, and phase change are iteratively solved until the heat boundary condition reaches convergence, then the temperature distribution and ice shape at the moment are obtained, and the calculation of the next time step begins subsequently. A deicing process is numerically simulated using the present model following an icing tunnel experiment, and the results match well with those in the literatures, which validate the present model. Then, an in-flight deicing process is numerically studied to analyze the effect of heating sequence. |
url |
http://dx.doi.org/10.1155/2018/5362541 |
work_keys_str_mv |
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1725774382007058432 |