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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/7450

    Title: 考慮非穩態尾流系統之直昇機旋翼扭角最佳化設計
    Other Titles: The Optimum Design for Helicopter Rotor Blade Twist Angel with Unsteady Wake System
    Authors: 王怡仁;張永康;陳慶祥
    Contributors: 淡江大學航空太空工程學系
    Keywords: Peters尾流動力理論;直昇機旋翼;葉片扭角;最佳設計;Peters' unsteady wake theory;Helicopter rotor;Blade twist angle;Optimumdesign
    Date: 1996
    Issue Date: 2009-03-16 16:16:16 (UTC+8)
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Research Paper

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