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    Deep Learning–Based Method for Efficient Airfoil Rime Icing Prediction

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006::page 04025081-1
    Author:
    Xu, Zhao-Ke
    ,
    Dai, Hao
    ,
    Zhang, Hai-Jun
    DOI: 10.1061/JAEEEZ.ASENG-6214
    Publisher: American Society of Civil Engineers
    Abstract: AbstractThe input feature parameters of current machine learning and deep learning–based wing icing prediction models primarily consist of flight states and atmospheric conditions, and the output data are ice shapes. This dependency necessitates many ...
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      Deep Learning–Based Method for Efficient Airfoil Rime Icing Prediction

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4314137
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    contributor authorXu, Zhao-Ke
    contributor authorDai, Hao
    contributor authorZhang, Hai-Jun
    date accessioned2026-08-20T21:13:18Z
    date available2026-08-20T21:13:18Z
    date copyright2025/08/05
    date issued2025
    identifier otherJAEEEZ.ASENG-6214.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314137
    description abstractAbstractThe input feature parameters of current machine learning and deep learning–based wing icing prediction models primarily consist of flight states and atmospheric conditions, and the output data are ice shapes. This dependency necessitates many ...
    publisherAmerican Society of Civil Engineers
    titleDeep Learning–Based Method for Efficient Airfoil Rime Icing Prediction
    typeJournal Article
    journal volume38
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-6214
    journal fristpage04025081-1
    journal lastpage04025081-11
    page11
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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