YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Multifidelity Model–Assisted Knowledge Transfer Optimization Method for Computationally Intensive Solid Rocket Motor Design

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006::page 04025078-1
    Author:
    Yang, Jiawei
    ,
    Wu, Zeping
    ,
    Wang, Wenjie
    ,
    Zhang, Weihua
    DOI: 10.1061/JAEEEZ.ASENG-5120
    Publisher: American Society of Civil Engineers
    Abstract: AbstractSolid rocket motor design based on high-fidelity simulation models is extremely time-consuming in practical engineering problems. To improve the efficiency of solid rocket motor design problems, this study proposes a multifidelity model–assisted ...
    • Download: (1.676Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Multifidelity Model–Assisted Knowledge Transfer Optimization Method for Computationally Intensive Solid Rocket Motor Design

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4314103
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    contributor authorYang, Jiawei
    contributor authorWu, Zeping
    contributor authorWang, Wenjie
    contributor authorZhang, Weihua
    date accessioned2026-08-20T21:12:00Z
    date available2026-08-20T21:12:00Z
    date copyright2025/07/25
    date issued2025
    identifier otherJAEEEZ.ASENG-5120.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314103
    description abstractAbstractSolid rocket motor design based on high-fidelity simulation models is extremely time-consuming in practical engineering problems. To improve the efficiency of solid rocket motor design problems, this study proposes a multifidelity model–assisted ...
    publisherAmerican Society of Civil Engineers
    titleMultifidelity Model–Assisted Knowledge Transfer Optimization Method for Computationally Intensive Solid Rocket Motor Design
    typeJournal Article
    journal volume38
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5120
    journal fristpage04025078-1
    journal lastpage04025078-14
    page14
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian