Thermo-elastic constants of cracked symmetric laminates: A refined variational approach

被引:36
|
作者
Hajikazemi, M. [1 ,2 ]
Sadr, M. H. [1 ,2 ]
Hosseini-Toudeshky, H. [1 ,2 ]
Mohammadi, B. [3 ]
机构
[1] Amirkabir Univ Technol, Dept Aerosp Engn, Tehran 158754413, Iran
[2] Amirkabir Univ Technol, Ctr Excellence Computat Aerosp Engn, Tehran 158754413, Iran
[3] Iran Univ Sci & Technol, Sch Mech Engn, Tehran, Iran
关键词
Thermal expansion coefficient; Ply-refinement technique; Intralaminar damage; Stiffness reduction; Levin's theorem; Refined variational approach; THERMAL-EXPANSION COEFFICIENTS; LAYERWISE STRESS APPROACH; TRANSVERSE CRACKING; MATRIX CRACKING; STIFFNESS REDUCTION; MULTILAYERED PLATES; DAMAGE; COMPOSITES; DELAMINATION; MODEL;
D O I
10.1016/j.ijmecsci.2014.08.008
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The present research work is aimed at predicting degradation of laminate stiffness and laminate thermal expansion coefficients (TEC) as a function of crack density for general symmetric laminates containing intralaminar matrix cracks. Therefore, an exact methodology is developed based on Levin's theorem to evaluate the effective thermal expansion coefficients of cracked laminates. Then, an admissible stress field, which satisfies equilibrium equations and all the boundary and continuity conditions, has been considered in conjunction with the principle of minimum complementary energy and a ply refinement technique in order to exactly predict degradation of all thermo-elastic constants of cracked symmetric laminates. Results derived from the developed method for thermo-elastic properties of the cracked laminates showed an excellent agreement with finite element and experimental results available in the literature. Moreover, a comparison has been made between the capability and accuracy of various models in predicting thermo-elastic constants of cracked laminates. It has been shown that the results obtained from the current approach are more accurate and also more consistent with finite element results compared to those obtained from shear-lag approach. (C) 2014 Elsevier Ltd. All rights reserved.
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页码:47 / 57
页数:11
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