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首页> 外文期刊>Uludag University Journal of The Faculty of Engineering >STRESS ANALYSIS AND EXPANSION OF PLASTIC ZONECOMPOSITE LAMINATED PLATES ([?0/-??0]2) UNDER TRANSVERSELOADS BY MEANS OF FEM
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STRESS ANALYSIS AND EXPANSION OF PLASTIC ZONECOMPOSITE LAMINATED PLATES ([?0/-??0]2) UNDER TRANSVERSELOADS BY MEANS OF FEM

机译:横向有限元作用下塑性带状复合材料层合板([?0 /-?? 0] 2)的应力分析与扩展

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The aim of this work is to predict the expansion of the plastic zone and residual stresses in layers ofstainless steel woven fiber-reinforced thermoplastic matrix composite laminated plates ([?0/-??0]2) with rectangular hole. The elastic and elastic-plastic stresses are analyzed by using FEM by means of a developed computerprogram with FORTRAN 90. The laminated plates arranged in ([?0/-??0]2) configuration under uniform transverse loading are formed by stacking four composite layers bonded symmetrically or antisymmetrically. Loadingis gradually increased from yield point of the plate as 0.0001 Mpa at each load step. The elastic, elastic-plasticand residual stress components and the expansion of the plastic zones are obtained according to the load steps,different orientation angles and rectangular hole dimensions under clamped and simply supported boundaryconditions. Results showed that the maximum stress levels and the plastic zones appear the vicinity of the rectangular hole at the upper and lower layers.
机译:这项工作的目的是预测带矩形孔的不锈钢编织纤维增强热塑性基体复合层压板([α0/-α0] 2)的层中塑性区的扩展和残余应力。弹性应力和弹塑性应力通过FEM借助开发的带有FORTRAN 90的计算机程序进行分析。通过堆叠四个复合材料,在均匀的横向载荷下以([?0 /-?0] 2)形式布置的层压板对称或反对称粘合的涂层。在每个加载步骤中,载荷从板的屈服点逐渐增加为0.0001 Mpa。弹性,弹塑性和残余应力分量以及塑性区的扩展是根据载荷步长,在夹紧和简单支撑的边界条件下的不同定向角和矩形孔尺寸而获得的。结果表明,最大应力水平和塑性区出现在上下两层矩形孔的附近。

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