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研究生: 黃婉詒
Huang, Wan-Yi
論文名稱: 非對稱複材疊層厚樑之結構分析
Structural Analysis of Unsymmetric Laminated Composite Thick Beams
指導教授: 胡潛濱
Hwu, Chyan-Bin
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2023
畢業學年度: 111
語文別: 英文
論文頁數: 70
中文關鍵詞: 明示解析解邊界有限元素法自由振動分析複材疊層樑Timoshenko樑理論
外文關鍵詞: Explicit analytical solutions, Boundary-based finite element method, Free vibration analysis, Laminated composite beam, Timoshenko beam theory
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  • 本研究考慮側向剪切變形之拉伸彎矩偶合的複材疊層厚樑結構分析。根據Timoshenko樑理論我們建立了任意疊層樑之數學模型,藉由狀態空間法(state-space approach)推得以矩陣指數形式呈現的通解,可應用於各種負載和邊界條件,如常見樑問題之明示解析解抑或是無窮域複材疊層厚樑的格林函數(Green’s function)。為解決更複雜的樑結構問題,我們以所推得之格林函數求取基本解,並應用至邊界有限元素法(Boundary-based finite element method)。透過互易定理(Reciprocal theorem of Betti and Rayleigh)可推導出邊界積分方程式(Boundary integral equations)。而所有涉及的積分項皆以解析積分的方式解出,不涉及任何奇異積分或數值積分。我們提出的邊界有限元素法只需兩端節點的單一元素即可為均勻厚度的直樑提供明示解。對於非均勻厚度的曲線梁,即使邊界有限元素法只能提供近似解,其收斂速度也遠比傳統有限元素法快。此研究也進一步延伸至自由振動分析,建構出以矩陣形式呈現之統御方程式,利用狀態空間法以及分離變數法求得自然頻率之通解,再透過施加邊界條件來建立特徵方程式,並利用二分法(Bisection method)和最小平方法(Least-squares technique)求解自然頻率和模態形狀。在數值範例中我們將其數值結果與有限元素商用軟體ANSYS進行比對,並驗證了明示解析解、邊界有限元素法以及分析自由振動方法之適用性。

    This research focuses on the structural analysis of laminated composite thick beams with coupled stretching-bending and transverse shear deformation. A mathematical model based on Timoshenko beam theory is established for general laminated beams. With the state-space approach, a general solution in terms of matrix exponential is obtained, which is applicable to various loading and boundary conditions. With the obtained general solutions, several analytical solutions are derived explicitly such as the Green’s functions for an infinite laminated composite thick beam. To cover more complicated beam structures, we develop the boundary-based finite element method (BFEM) using the obtained Green's functions. Since the boundary integral equations (BIEs) derived through the reciprocal theorem of Betti and Rayleigh do not involve singular integrals or numerical integration, our proposed BFEM provides an exact solution for a straight beam with uniform thickness using only one element with two end nodes. Even only an approximate solution is obtained for a curvilinear beam with non-uniform thickness, BFEM converges faster than the conventional finite element method. The research further extends to free vibration analysis, constructing displacement-based governing equations in matrix form. By enforcing boundary conditions, the eigen-relation is established to solve for natural frequencies and mode shapes using the bisection method and least-squares technique. Numerical examples validate the applicability of newly derived explicit solutions, the BFEM and the proposed free vibration method by comparing the results with commercial finite element software ANSYS.

    摘要 I Abstract II Acknowledgements III Contents IV List of Tables VI List of Figures VII Nomenclature IX Chapter 1 Introduction 1 1.1 Literature Review 1 1.2 Structure of Thesis 4 Chapter 2 Timoshenko Beam Theory for Laminated Composite Thick Beams 5 2.1 Static Analysis 5 2.2 Vibration Analysis 6 2.3 Beam Stiffnesses 7 Chapter 3 Analytical Solutions for Uniform Straight Beams 10 3.1 Solutions in Terms of Matrix Exponential 10 3.2 Explicit-Form Solutions 11 3.3 Green's Function 13 3.4 Typical Beam Problems 15 Chapter 4 Boundary-based Finite Element Method for Non-uniform Curved Beams 21 4.1 Boundary Integral Equations 21 4.2 Explicit Solutions Solved by Using BIE 25 4.3 Solutions by BFEM 28 Chapter 5 Free Vibration 31 5.1 General Solutions 31 5.2 Natural Frequencies and Mode Shapes 32 Chapter 6 Numerical Results and Discussions 34 6.1 Analytical Solutions 34 6.2 BFEM Solutions 37 6.3 Free Vibration 43 Chapter 7 Conclusions 45 References 47

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