English  |  正體中文  |  简体中文  |  Items with full text/Total items : 49287/83828 (59%)
Visitors : 7147357      Online Users : 81
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/987654321/62581


    Title: 單質點減振器於非線性氣體彈性系統減振之研究
    Other Titles: The Analysis of The Point Mass Vibration Absorber on a Nonlinear Aeroelastic System
    Authors: 王怡仁;陳柏翰
    Contributors: 淡江大學航空太空工程學系
    Keywords: 非穩態空氣動力學;減振裝置;三次方非線性彈簧;Unsteady Aerodynamic;Absorber;Cubic Spring
    Date: 2008-12
    Issue Date: 2011-10-18 21:55:42 (UTC+8)
    Publisher: 淡江大學
    臺北市:中華民國航空太空學會
    Abstract: 本研究餘採取非線性的物理模式來模擬整個振動體之運動,非線性的物理模式停將彈簧模擬成三次方才的變化量(cubic spring) ,以使振動變成非線性的模式。並使用Multiple Scales Analysis 求得時間域性動態解析解。上述非線性系統之解析解,將與頻率域的數值解作比對,以驗證本論文之結果。本研究豆中之二維振動系統可視為翼剖面(airfoil) ,亦可視為吊橋;而單一質點減振器可視為一般之派龍架局亦可視為吊橋下之減振裝置。吾人在考慮不變動大部分的設計之下,改變減振器位置以及材料特性,達到最經濟的減振效果。
    The Newton's second law is used to analyze a system of nonlinearly vibrational rigid body, doing pitching and plunging in conjunction with an unsteady nonlinear aerodynamic force and an absorber. The cubic spring is employed to simulate a nonlinear vibration system. The""Multiple Scales Analysis""is used to get the analytic solution in time domain. The analytic solutions will be correlated with the numerical results to ensure the nonlinear model and the effects of the absorber. By using the mathematical model presented in this study, one can adjust the position or design of the absorber to reduce vibration, without changing the main configuration or original design. In conclusion, this model has an enormous applicable value towards
    applied engineering and related fields.
    Relation: 中華民國航空太空學會第五十屆年會暨學術研討會國科會航太學門成果發表會會議首冊暨論文摘要集,頁110
    Appears in Collections:[航空太空工程學系暨研究所] 會議論文

    Files in This Item:

    File SizeFormat
    index.html0KbHTML103View/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