淡江大學機構典藏:Item 987654321/120829
English  |  正體中文  |  简体中文  |  Items with full text/Total items : 58617/92280 (64%)
Visitors : 564109      Online Users : 61
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
Scope Tips:
  • please add "double quotation mark" for query phrases to get precise results
  • please goto advance search for comprehansive author search
  • Adv. Search
    HomeLoginUploadHelpAboutAdminister Goto mobile version
    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/120829


    Title: Design, Manufacturing, and Flight Testing od an Experimental Flying Wing UAV
    Authors: Chung, Pei-Hsiang;Ma, Der-Ming;Shiau, Jaw-Kuen
    Keywords: UAV design;flight testing;flying wing
    Date: 2010-07-28
    Issue Date: 2021-06-10 12:10:21 (UTC+8)
    Abstract: This paper presents the design, manufacturing, and flight testing of an electric-powered
    experimental flying wing unmanned aerial vehicle (UAV). The design process starts with defining
    the performance requirements including the stall speed, maximal speed, cruise altitude, absolute
    ceiling, and turn radius and speed. The wing loading and associated power loading are obtained
    based on the defined performance requirements. The wing area, UAV mass, and power requirements
    are determined from the endurance and payload requirements. The power requirement determines
    the motor size. Aerodynamics and stability designs are obtained based on the selected airfoil and
    obtained wing area. After completing the design, the UAV is manufactured using composite materials.
    The UAV is equipped with an AXi 4130/20 kv305 brushless motor and a Pixhawk flight control board.
    Its total weight is 8.6 kg. Flight tests were conducted to evaluate the UAV’s performance and dynamic
    characteristics and to demonstrate the success of the design.
    Relation: Applied Science 9(15), 3043
    DOI: 10.3390/app9153043
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

    Files in This Item:

    File Description SizeFormat
    index.html0KbHTML12View/Open

    All items in 機構典藏 are protected by copyright, with all rights reserved.


    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - Feedback