基于指数剪切法向变形理论的层状复合材料及夹层拱的动静响应评价

IF 3.2 Q2 MATERIALS SCIENCE, MULTIDISCIPLINARY
Valmik M. Mahajan , Amit Sharma
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引用次数: 1

摘要

本理论利用指数剪切和法向变形理论(ESNDT)研究多层和夹层拱的无量纲振动频率、变形和应力。目前的研究在选取均布荷载作用下拱的位移场时考虑了[1+(z/R)]曲率半径的影响。它包括横向剪切效应(γxz≠0)和横向法向变形效应(εz≠0),即厚度拉伸效应。利用纳维耶法和哈密顿虚功原理得到了控制关系。所提出的分层拱完全不受剪切修正,其顶、底表面均满足零牵引力自由端条件。由于现有文献未考虑厚度拉伸效应,即(εz=0),本研究获得的层状夹层拱的固有频率比其他理论更精确。因此,本科学研究考虑厚度拉伸的影响,即(εz≠0)。然而,层状夹层拱的弯曲和动力响应的精确弹性结果尚未得到。本理论得到了层状复合材料和夹层拱的振动频率、位移和应力;通过先前发表的文献对结果进行了比较和验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Evaluation of static and dynamic responses considering thickness stretching effect for layered composite and sandwich arches using exponential shear and normal deformation theory

Present theory investigates the dimensionless vibration frequencies, deformations, and stresses for multilayered and sandwich arches using exponential shear and normal deformation theory (ESNDT). Present studies consider the effect of [1+(z/R)]radius of curvature while selecting the displacement field of arches under the action of uniform load. It includes the effects of transverse shear (γxz0) and transverse normal deformation(εz0) i.e., effect of thickness stretching. The governing relations are obtained using the Navier's method, and Hamilton's virtual work principle. The proposed layered arches are completely free from shear correction, and its top and bottom surfaces is satisfies zero traction free end conditions. Present study obtained very accurate natural frequencies for layered sandwich arches than other theories because, available literature not considered the thickness stretching effect i.e.,(εz=0). Hence, the present scientific investigation accounts the effect of thickness stretching i.e.,(εz0). However, the non-availability of exact elasticity results of bending and dynamic responses for layered sandwich arches. Present theory is obtained vibration frequencies, displacements, and stresses of layered composite and sandwich arches; the results are compared and validates through prior published literature.

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来源期刊
Forces in mechanics
Forces in mechanics Mechanics of Materials
CiteScore
3.50
自引率
0.00%
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审稿时长
52 days
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