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    Aerodynamic Shape Optimization of Forebodies Based on the GEK and Discrete Adjoint Methods

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006::page 04025086-1
    Author:
    Xiao, Yang
    ,
    Zhang, Yufei
    DOI: 10.1061/JAEEEZ.ASENG-5602
    Publisher: American Society of Civil Engineers
    Abstract: AbstractThe aerodynamic shape optimization of air-breathing hypersonic vehicles often involves a high computational load due to the large number of design variables. Additionally, the complex shockwave structures and shockwave-geometry interactions can ...
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      Aerodynamic Shape Optimization of Forebodies Based on the GEK and Discrete Adjoint Methods

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4314111
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    contributor authorXiao, Yang
    contributor authorZhang, Yufei
    date accessioned2026-08-20T21:12:22Z
    date available2026-08-20T21:12:22Z
    date copyright2025/08/12
    date issued2025
    identifier otherJAEEEZ.ASENG-5602.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314111
    description abstractAbstractThe aerodynamic shape optimization of air-breathing hypersonic vehicles often involves a high computational load due to the large number of design variables. Additionally, the complex shockwave structures and shockwave-geometry interactions can ...
    publisherAmerican Society of Civil Engineers
    titleAerodynamic Shape Optimization of Forebodies Based on the GEK and Discrete Adjoint Methods
    typeJournal Article
    journal volume38
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5602
    journal fristpage04025086-1
    journal lastpage04025086-15
    page15
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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