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研究生: 楊登鈞
Yang, Teng-Chun
論文名稱: 開孔複合材料板受軸力及螺栓應力之非線性分析
NONLINEAR ANALYSIS OF COMPOSITE LAMINATE WITH PIN-FILLED HOLE SUBJECTED TO TENSILE FORCE AND WASHER CLAMPING PRESSURE
指導教授: 胡宣德
Hu, Hsuan-Teh
學位類別: 碩士
Master
系所名稱: 工學院 - 土木工程學系
Department of Civil Engineering
論文出版年: 2006
畢業學年度: 94
語文別: 中文
論文頁數: 174
中文關鍵詞: 非線性分析螺栓應力
外文關鍵詞: pin-filled hole, clmping pressure
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  • 本研究針對開孔纖維複材板受集中載重及側向箝制之下,使用一套非線性破壞分析模式,進行材料之破壞預測及破壞行為分析探討。此非線性破壞分析模式主要包含三部分:(1)材料局部破壞前的非線性組成律,(2)材料局部預測破壞時機的混合破壞準則,(3)材料局部破壞後的後破壞分析模式。
    模擬複材單層板破壞前之非線性行為,係假設材料在軸向及側向均為彈性-塑性行為,剪力參數則使用非定值來模擬之。判斷材了局部破壞的依據,則使用混合破壞準則。在後破壞行為分析中,單層板軸向和剪力之行為皆假設為脆性破壞模式,側向採用逐降破壞模式模擬之。
    最後,非線性破壞模擬並且分析結果,將與開孔複材板受插銷集中載重及側向箝制作用之實驗數據加以比較,驗證明本論文所建議之分析模式是否適用。

    In this study, using a nonlinear failure analysis model, for predicting the response of composite laminate, which has pin concentrated load on the hole and lateral constrained load with washers. A nonlinear failure load analysis mode, which includes nonlinear constitutive law, mixed failure criterion and post failure mode.
    The fiber and matrix are assumed to have elastic-plastic behavior and to behave nonlinear with a variable shear parameter, as the composite lamina being in the pre-damage region, which the response of an individual lamina within the laminate is described by the nonlinear law. Beginning the local damage on individual lamina is detected by the mixed failure criterion, which is composed of Tasi-Wu failure criterion and maximum stress criterion. The fiber and in-plane shear are assumed to exhibit brittle behavior, and the matrix is assumed to exhibit degrading behavior.
    Finally, the nonlinear failure analysis model has been compared with the experimental results and the predictions by other criteria. It is proved that the model is suitable analysis model to predict the response of composite laminate, which has pin concentrated load on the hole and lateral constrained load with washers.

    論文摘要................................................................I ABSTRACT.............................................................II 誌謝...................................................................III 目錄...................................................................IV 圖目錄................................................................VII 符號說明.............................................................XIII 第一章 緒論..........................................................1 1.1 研究動機及方向.................................................1 1.2 研究主題及目的.................................................4 第二章 纖維複材疊層板之基本分析模式............................6 2.1 複材簡介.......................................................6 2.2 正向單層板的線性應力-應變關係.................................7 2.3 正向單層板之非線性分析模式....................................9 2.4 單層板在任意座標之非線性應力應變關係..........................10 第三章 複材之破壞準則理論........................................13 3.1 序言..........................................................13 3.2 破壞準則之內容................................................13 3.3 極限理論概述..................................................14 3.3.1 最大應力準則..........................................14 3.3.2 最大應變準則..........................................15 3.4 應變能理論概述................................................18 3.4.1 von Mises等向降伏準則.................................18 3.4.2 Tsai-Hill破壞準則......................................19 3.5 多項式理論概述................................................21 3.5.1 Hoffman破壞準則......................................21 3.5.2 Tsai-Wu破壞準則.......................................23 3.6 直接模式運算理論概述..........................................25 3.6.1 Hashin-Rotem破壞準則..................................25 3.6.2 Hashin破壞準則........................................28 3.6.3 Lee破壞準則..........................................29 3.6.4 Edge破壞準則.........................................30 3.6.5 Chang破壞準則........................................32 第四章 建議之非線性破壞分析模式.................................34 4.1 概述..........................................................34 4.2 非線性組成律..................................................35 4.3 混合破壞準則..................................................36 4.4 後破壞分析模式................................................37 4.5 複材疊層板之控制方程式........................................40 4.6 正規化破壞應力及破壞貢獻度....................................41 第五章 數值分析結果...............................................43 5.1 序論..........................................................43 5.2 數值模型的建立與材料性質描述..................................45 5.2.1 數值模型的建立........................................45 5.2.2 材料性質描述..........................................47 5.3 非線性破壞分析模式之確認與收斂性分析..........................48 5.4 開孔纖維複材疊層板受螺栓集中應力及側向箝制作用之數值分析......50 5.4.1 概述..................................................50 5.4.2 探討固定側向箝制壓力,改變墊圈受力表面積影響...........51 5.4.3 探討固定墊圈受力表面積,改變側向箝制壓力影響...........58 5.4.4 探討固定側向箝制力,改變墊圈受力表面積影響.............62 第六章 結論與建議.................................................66 參考文獻...............................................................69 附圖...................................................................74 附錄..................................................................138 附錄A Fortran Subroutine-Mixed Failure Criterion...........................139 附錄B ABAQUS Program Input File......................................148 自述..................................................................156

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