| 研究生: |
劉嘉文 Liu, Chia-Wen |
|---|---|
| 論文名稱: |
開孔纖維複材疊層板在雙軸張應力之非線性破壞分析 |
| 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: | 2005 |
| 畢業學年度: | 93 |
| 語文別: | 中文 |
| 論文頁數: | 136 |
| 中文關鍵詞: | 複合材料 、雙軸力 |
| 相關次數: | 點閱:137 下載:8 |
| 分享至: |
| 查詢本校圖書館目錄 查詢臺灣博碩士論文知識加值系統 勘誤回報 |
在本篇研究當中,使用一套非線性破壞分析模式,針對開孔纖維加強複合材料疊層板承受雙軸張應力作用下,進行材料之破壞預測及分析探討。此非線性破壞分析模式包含三部分:
1. 材料破壞前的非線性組成律
2. 預測破壞時機的混合破壞準則
3. 後破壞分析模式。
對於開孔複材單層板破壞前之非線性行為,均假設材料在軸向(纖維)及側向(基材)均為彈性-塑性行為,而面內剪力則使用定值剪力參數來描述之。對於用於破壞時機之預測,則結合Tsai-Wu破壞準則及最大應力準則,稱之為混合破壞準則。後破壞分析模式中,對單層板軸向及剪力之行為假設成脆性破壞模式,而側向則採用逐降模式模擬之。
該非線性破壞分析模式所預測之結果,將分別與開孔複材疊層板之實驗數據結果做比較,以證明纖維加強開孔複合材料疊層板在雙軸拉力作用下,本文所建議之分析模式正確且合理。最後,將影響複材疊層板強度的三種因素:孔徑、疊序及應力比三者之間相互做一系列的探討,以期能適切應用於工程上。
none
參考文獻
[1] Akbar Khatibi, A., Ye, L. and Mai Y.-W., "An Effective Crack Growth Model for Residual Strength Evaluation of Composite Laminates with Circular Holes", Journal of Composite Materials, Vol.30, pp.142-163, 1996.
[2] Azzi, V.-D. and Tsai, S.-W., "Anisotropic Strength of Composite," Exp. Mech., Vol.5, pp. 283-288, 1965.
[3] Backlund, J. and Aronsson, C.-G., "Tensile Fracture of Laminates with Hole", Journal of Composite Materials, Vol.20, pp.259-281, 1988.
[4] Chang, F.-K. and Chang, K.-Y., "A Progressive Damage Model for Laminated Composites Containing Stress Concentrations", Journal of Composite Materials, Vol.21, pp.834-855, 1987.
[5] Chang, F.-K. and Chang, K.-Y., "Post-Failure Analysis of Bolted Composites Joints in Tension or Shear-out Mode Failure ", Journal of Composite Materials,, Vol.21, pp.809-833, 1987.
[6] Chang, F.-K. and Lessard, L.-B., "Damage Tolerance of Laminated Composite Containing an Open Hole and Subjected to Compressive Loadings: Part I-Analysis", Journal of Composite Materials, Vol.25, pp.2-43, 1991.
[7] Chang, F.-K. and Lessard, L.-B., "Damage Tolerance of Laminated Composite Containing an Open Hole and Subjected to Compressive Loadings: Part Ⅱ-Experiment", Journal of Composite Materials, Vol.25, pp.44-64, 1991.
[8] Chang, F.-K., Liu Sheng and Chang, K.-Y., "Damage Tolerance of Laminated Composite Containing an Open Hole and Subjected to Tensile Loadings ", Journal of Composite Materials, Vol.25, pp.274-301, 1991.
[9] Daniel, I.-M., "Behavior of Graphite/Epoxy Composites Plates with Holes Biaxial Loading ", Experimental Mechanics, Vol.20, pp.1-8.1980.
[10] Daniel, I.-M., "Biaxial Testing of Graphite/Epoxy Composites Containing Stress Concentrations", Air Force Materials Laboratory, Report AFML-TR-76-244, Part I 1976., Part II 1977.
[11] Daniel, I.-M., "Biaxial Testing of Graphite/Epoxy Laminates with cracks ", Test Methods and Design Allowables for Fibrous Composites, ASTM STP 734, American Society for Testing and Materials, pp. 109-128, 1981.
[12] Daniel, I.-M., "Biaxial Testing of Graphite/Epoxy Plates with Holes ", Experimental Mechanics, Vol.22, pp.188-195, 1982.
[13] Filiou, C. and Soutis, C., "Approximate Biaxial Stress Solution for Orthotropic Open-Hole Composite Laminates", Adventure Composite Letters 5, pp.107-112, 1996.
[14] Filiou, C. and Soutis, C., "Approximate Stress Solution for Orthotropic Open-Hole Subjected to Biaxial Loading ", 4th Internet. Conf. Deformation and Fracture of Composite , Sponsored by the Institute of Materials, UMIST, Manchester, UK, 24-26, pp.121-130, 1997.
[15] Hahn, H.-T., "Nonlinear Behavior of Laminated Composites", Journal of Composite Materials, Vol.7, pp.257-271, 1973.
[16] Hahn, H.-T. and Tsai, S.-W., "Nonlinear Elastic Behavior of Unidirectional Composite Laminates", Journal of Composite Materials, Vol.7, pp.102-118, 1973.
[17] Hakan K. and Rami H.-A., "Progressive damage and nonlinear analysis of pultruded composite structures", Composites : Part B, Vol.34, pp.235-250, 2003.
[18] Hashin, Z., "Failure Criteria for Unidirectional Fiber Composites", J. Appl. Mech., Vol.47, pp.329-334, 1980.
[19] Hu, H.-T., "Influence of In-plane Shear Nonlinearity on Buckling and Postbuckling Responses of Composite Laminate Plates and Shells", Journal of Composite Materials, Vol.27, pp.138-151, 1993.
[20] Kenaga D., Doyle, J.-F. and Sun, C.-T., "The Characterization of Boron/Aluminum Composite in the Nonlinear Range as an Orthotropic Elastic-Plastic Material", Journal of Composite Materials, Vol.21, pp.516-531, 1987.
[21] Konish, H.-J. and Whitney, J.-M., " Approximate Stresses in an Orthotropic Plate Containing a Circular Hole", Journal of Composite Materials, Vol.9, pp.157-166, 1975.
[22] Lee, J.-D., "Three Dimensional Finite Element Analysis of Damage Accumulation in Composite Laminate", Computers & Structures, Vol.15, pp.335-350, 1982.
[23] Liu, K.-S. and Tsai, S.-W., "A Progressive Quadratic Failure Criterion of a Laminate", Composites Science and Technology, Vol.58, pp.1023-1032, 1998.
[24] Lo, K.-H. and Wu, E.-M., "Failure Strength Of Laminates with Holes", Air Force Materials Laboratory, Contract No. F33615-76-C-5344, Seventh Quarterly Report 1978.
[25] Petit, P.-H. and Waddoups, M.-E., "A Method of Predicting the Nonlinear Behavior of Laminated Composites", Journal of Composite Materials, Vol.3, pp.2-19, 1969.
[26] Rotem, A., "Prediction of Laminate Failure with the Rotem Failure Criterion", Composites Science and Technology, Vol.58, pp.1083-1094, 1998.
[27] Rotem, A. and Nelson, H.-G., "Fatigue Behavior of Graphite-Epoxy Laminate at Elevated Temperatures", ASTM STP 723, pp.152-173, 1981.
[28] Rowlands, R.-E., "Strength (Failure) Theories and Their Experimental Correlation", Failure Mechanics of Composites, Elsevier, Amsterdam, pp.71-125, 1985.
[29] Rowlands, R.-E., Daniel, I.-M. and Whiteside, J.-B., "Stress and Failure Analysis of a Glass-Epoxy Plate with a Hole", Experimental Mechanics, Vol.13, pp.31-37, 1973.
[30] Rowlands, R.-E., Daniel, I.-M. and Whiteside, J.-B., " Deformation and Failure of Boron-Epoxy Plate with circular Hole ", Analysis of the Test Methods for High Modulus Fibers and Composites, ASTM STP 521, American Society for Testing and Materials, pp. 143-164, 1973.
[31] Soden, P.-D., Kitching, R. and Tse, P.-C., "Experimental Failure Stresses for Filament Wound Glass Fiber Reinforced Plastic Tubes under Biaxial Loads", Composites, Vol.20, pp.125-135, 1989.
[32] Soutis, C. and Fleck, N.-A., "Static Compression Failure of Carbon Fiber T800/924C Composite Plate with a Single Hole", Journal of Composite Materials, Vol.24, pp.536-558, 1990.
[33] Sun, C.-T. and Chen, J.-L., "A Simple Flow Rule for Characterizing Nonlinear Behavior of Fiber Composite", Journal of Composite Materials, Vol.23, pp.1009-1020, 1989.
[34] Tan, S.-C., "Effective Stress Fracture Models for Unnotched and Notched Multidirectional Laminates ", Journal of Composite Materials, Vol.22, pp.322-340, 1988.
[35] Tan, S.-C., " Laminated Composites Containing an Elliptical Opening. I-Approximate Stress Analysis and Fracture Models", Journal of Composite Materials, Vol.21, pp.925-948, 1987.
[36] Tan, S.-C., " Laminated Composites Containing an Elliptical Opening. Ⅱ-Experiment and Model Modification", Journal of Composite Materials, Vol.21, pp.949-968, 1987.
[37] Tan, S.-C., "Notched Strength Prediction and Design Laminated Composite Under In-Plane Loadings", Journal of Composite Materials, Vol.21, pp.750-780, 1987.
[38] Tan, S.-C., "Tensile and Compressive Notched Strength of PEEK Matrix Composite Laminates", Journal of Reinforced Plastics and Composite, Vol.6, pp.253-267, 1987.
[39] Tsai, S.-W. and Wu, E.-M., "A General Theory of Strength for Anisotropic Materials", Journal of Composite Materials, Vol.5, pp.58-80, 1971.
[40] Vaziri, R., Olson, M.-D. and Anderson, D.-L., "A Plasticity-Based Constitutive Model for Fiber-Reinforced Composite Laminates", Journal of Composite Materials, Vol.25, pp.512-535, 1991.
[41] 林文賓,"纖維複材疊層板在單軸及雙軸張力載重下之非線性破壞分析",國立成功大學土木工程學系,博士論文,中華民國九十年十二月。
[42] 柯龍聖,"纖維複材疊層板在單軸壓力載重下之非線性破壞分析",國立成功大學土木工程學系,碩士論文,中華民國九十一年六月。
[43] 杜方泰,"纖維複材疊層板在雙軸載重下之非線性破壞分析",國立成功大學土木工程學系,碩士論文,中華民國九十二年六月。
[44] 李凱元,"開孔纖維複材疊層板受單軸壓力之非線性破壞分析",國立成功大學土木工程學系,碩士論文,中華民國九十三年六月。