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研究生:葉昶佑
研究生(外文):Yeh, Chang-You
論文名稱:冪函數漸變彈性纖維複合材料之反平面問題
論文名稱(外文):Anti-Plane Problem of Power Law Graded Elastic Fibrous Composites
指導教授:郭心怡郭心怡引用關係
指導教授(外文):Kuo, Hsin-Yi
口試委員:郭志禹、陳誠直
學位類別:碩士
校院名稱:國立交通大學
系所名稱:土木工程系所
學門:工程學門
學類:土木工程學類
論文種類:學術論文
論文出版年:2019
畢業學年度:107
語文別:中文
論文頁數:60
中文關鍵詞:功能梯度材料、纖維複合材料、反平面問題、週期性排列、等效彈性模數
外文關鍵詞:Functionally graded material、Fibrous composite material、Anti-plane problem、Periodic arrangement、Equivalent elastic modulus
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本論文探討冪函數漸變纖維複合材料之彈性力學反平面問題,功能梯度材料(Functionally graded material)之材料性質沿著徑向或厚度方向變化,其漸變性質可使其材料之間無明顯交界面並減少應力集中的現象。本文探討材料性質隨著纖維半徑r呈冪函數 漸變( 為漸變參數)。
本研究將內含物以方形陣列(Square array)及六邊形陣列(Hexagonal array)排列,利用週期性排列時的Rayleigh法求得等效彈性模數 ,並透過聚合複合圓柱模型(Composite cylinder assemblage model)與有限元素法(COMSOL Multiphysics 5.0)驗證其結果之正確性。此外,透過收斂性分析檢核位移係數與位移之收斂性,以及有限元素法分析中所適用的網格,並確認位移函數在交界面上之連續性。
本文分為有無殼層兩種形式,數值結果顯示在無殼層纖維複合材料中,當漸變參數 為-2時,對等效彈性模數 有較顯著的提升,但其誤差也會隨著漸變參數 變大而遞增。後續在改變材料性質比例的部分發現,當 時,對於等效彈性模數 之影響較大。而在具殼層纖維複合材料中,當漸變參數 為+25且c (殼層與核層厚度比例)為0.1時,對等效彈性模數 的影響較為顯著,其誤差在不同內含物體積百分率下皆有良好一致性。最後藉由改變材料性質比例與殼層厚度探討對等效彈性模數 的影響,材料性質比例 對等效彈性模數 變化之影響較大,並發現在不同漸變參數 的情況下,等效彈性模數 皆會在特定的厚度達到極值,而非與厚度成正比。
This research studies the anti-plane problem of functionally graded fibrous composites in power law of elasticity theory, in which the functionally graded material’s gradient properties express without a clear interface between the materials. We investigate the changes in material property with the fiber radius r as a power function ( is a gradient parameter).
This experiment consists of square array and hexagonal array, the equivalent elastic modulus of the composite material that is obtained by the Rayleigh method; finite element analysis (COMSOL Multiphysics 5.0) and composite cylinder assemblages model are used to compare the results predicated by the Rayleigh’s method. In addition, the convergence analysis is used to understand the convergence of the displacement coefficient and the displacement and choose the mesh applied in the finite element analysis. Furthermore, we confirm the continuity of the displacement equation at the interface.
Numerical calculations are divided into two cases. First, in the fiber-matrix case, when the gradient parameter is -2, there is a significant improvement on the equivalent elastic modulus , but the error will increase as the gradient parameter becomes larger. In the section that changes the material property ratio, it is found that has a greater influence on the equivalent elastic modulus . Next, in the fiber-shell-matrix case, when the gradient parameter is +25 and c is 0.1 (where c is the shell thickness to core thickness ratio), the effect on the equivalent elastic modulus is more significant, and the error has good consistency in different volume fractions. Additionally, we discuss the impact on equivalent elastic modulus by changing the material property ratios and shell thickness. Numerical results demonstrated that the material property ratio has a greater influence on the equivalent elastic modulus . In the case of different gradual parameters, the equivalent elastic modulus will reach an extreme value at a particular thickness rather than being proportional to the thickness.
摘要 I
Abstract II
目錄 IV
圖目錄 VII
表目錄 XIV
符號表 XV
第一章 導論 1
1-1 研究背景與目的 1
1-2 功能梯度材料 2
1-2-1 纖維複合材料 2
1-2-2 非等向性材料 3
1-3 文獻回顧 3
1-3-1 功能梯度材料 3
1-3-2 複合材料 5
1-3-3 反平面問題 6
1-4 本文架構 7
第二章 無殼層纖維複合材料 8
2-1 彈性力學基本方程與反平面問題 9
2-1-1 彈性力學基本方程 9
2-1-2 反平面問題 11
2-2 等效彈性模數 14
2-2-1 內含物位移函數 14
2-2-2 內含物為任意排列之位移係數關係 16
2-2-3 內含物為週期性排列之位移係數關係 20
2-2-4 等效彈性模數 22
2-2-5 收斂性分析 25
2-3 聚合複合圓柱模型 47
2-4 有限元素法之收斂性分析 49
2-5 數值結果與分析 54
2-5-1 材料選擇 54
2-5-2 位移圖 54
2-5-3 等效彈性模數 61
2-5-4 數值結果分析 70
第三章 具殼層纖維複合材料 75
3-1 材料性質與反平面問題 76
3-1-1 材料性質 76
3-1-2 反平面問題 77
3-2 位移函數 78
3-2-1 殼層位移函數 79
3-2-2 內含物為週期性排列之位移係數關係 83
3-2-3 收斂性分析 87
3-3 聚合複合圓柱模型 111
3-4 有限元素法之收斂性分析 114
3-5 數值結果與分析 117
3-5-1 材料選擇 118
3-5-2 位移圖 118
3-5-3 等效彈性模數 123
3-5-4 數值結果分析 130
第四章 結論與未來展望 136
4-1 結論 136
4-2 未來展望 138
參考文獻 139
附錄A COMSOL Multiphysics 5.0操作流程 144
A-1 研究領域選擇 144
A-2 全域參數定義 145
A-3 元件定義 145
A-4 元件幾何 148
A-5 元件材料 149
A-6 元件固體力學 150
A-7 元件網格 152
A-8 研究求解器設定 153
A-9 讀取結果設定 154
附錄B 收斂性誤差分析 155
B-1 無殼層纖維複合材料之收斂性誤差 155
B-2 具殼層纖維複合材料之收斂性誤差 158
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