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    Aerothermal–Heat Transfer Coupling Calculation Method Based on Whole Ballistic Iteration

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005::page 04025072-1
    Author:
    Qiu, Bo
    ,
    Zhu, Yandan
    ,
    Liu, Xiao
    ,
    Zhang, Haoyuan
    ,
    Yao, Jie
    ,
    Zeng, Lei
    DOI: 10.1061/JAEEEZ.ASENG-6113
    Publisher: American Society of Civil Engineers
    Abstract: AbstractAiming at the coupling problem between the aerothermal environment of an aircraft’s flow field and the thermal response of its structural field, this paper proposes a novel coupling calculation method based on whole ballistic iteration, which ...
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      Aerothermal–Heat Transfer Coupling Calculation Method Based on Whole Ballistic Iteration

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4314125
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    contributor authorQiu, Bo
    contributor authorZhu, Yandan
    contributor authorLiu, Xiao
    contributor authorZhang, Haoyuan
    contributor authorYao, Jie
    contributor authorZeng, Lei
    date accessioned2026-08-20T21:12:57Z
    date available2026-08-20T21:12:57Z
    date copyright2025/07/10
    date issued2025
    identifier otherJAEEEZ.ASENG-6113.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314125
    description abstractAbstractAiming at the coupling problem between the aerothermal environment of an aircraft’s flow field and the thermal response of its structural field, this paper proposes a novel coupling calculation method based on whole ballistic iteration, which ...
    publisherAmerican Society of Civil Engineers
    titleAerothermal–Heat Transfer Coupling Calculation Method Based on Whole Ballistic Iteration
    typeJournal Article
    journal volume38
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-6113
    journal fristpage04025072-1
    journal lastpage04025072-15
    page15
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005
    contenttypeFulltext
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