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

    Multidisciplinary Design Optimization of the Vertical Takeoff and Landing for Fixed-Wing Hybrid Unmanned Aerial Vehicles

    Source: Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 002::page 04025129-1
    Author:
    Zhang, Hang
    ,
    Xiang, Tao
    ,
    Zhang, Shenwei
    ,
    Wang, Wei
    DOI: 10.1061/JAEEEZ.ASENG-6104
    Publisher: American Society of Civil Engineers
    Abstract: AbstractVertical takeoff and landing (VTOL) fixed-wing hybrid unmanned aerial vehicle is currently the most noteworthy and practical solution for VTOL fixed-wing aircraft. However, several issues persist in existing electric fixed-wing hybrid unmanned ...
    • Download: (3.854Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Multidisciplinary Design Optimization of the Vertical Takeoff and Landing for Fixed-Wing Hybrid Unmanned Aerial Vehicles

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4314124
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    contributor authorZhang, Hang
    contributor authorXiang, Tao
    contributor authorZhang, Shenwei
    contributor authorWang, Wei
    date accessioned2026-08-20T21:12:55Z
    date available2026-08-20T21:12:55Z
    date copyright2025/11/22
    date issued2026
    identifier otherJAEEEZ.ASENG-6104.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314124
    description abstractAbstractVertical takeoff and landing (VTOL) fixed-wing hybrid unmanned aerial vehicle is currently the most noteworthy and practical solution for VTOL fixed-wing aircraft. However, several issues persist in existing electric fixed-wing hybrid unmanned ...
    publisherAmerican Society of Civil Engineers
    titleMultidisciplinary Design Optimization of the Vertical Takeoff and Landing for Fixed-Wing Hybrid Unmanned Aerial Vehicles
    typeJournal Article
    journal volume39
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-6104
    journal fristpage04025129-1
    journal lastpage04025129-9
    page9
    treeJournal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 002
    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