受轴向温度梯度影响的层压复合材料带材的边缘应力

D. Swett, G. Shiflett
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引用次数: 0

摘要

在热环境中使用层压复合材料结构最严重的问题之一是由于组成层之间的热膨胀不匹配引起的边缘效应应力而容易分层。此外,极端热梯度效应的引入也可能使问题复杂化。迄今为止,由于缺乏对这些热负荷产生的边缘效应的准确分析评估,为这些类型的热环境开发令人满意的设计的贸易研究相当有限。对这些类型的热梯度问题的主要研究仅限于详细的数值有限元分析,这不利于快速的并行工程设计过程。目前还没有一种解析解可以解决由热梯度引起的复合材料层合板的热弹性边缘效应。本文采用Airy应力函数和直接位移函数相结合的方法,得到了纵向任意对称温度梯度作用下多层各向异性层合带材的应力和位移的平面弹性解。由于只使合力为零,不能保证解满足自由边法向牵引力要求;然而,由于特征函数是正交的,因此可以建立条形两端强制零横向斜率的收敛性。因此,对于这些边缘条件,解是精确的。给出了几个实例的数值结果,并与我们自己的MSC/NASTRAN有限元分析结果进行了比较。通过与有限元数值结果的相关性验证了该解的正确性,并表明在涉及温度梯度效应的广泛实际情况下,将该解近似应用于自由边缘工程问题是非常合理的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Edge Stresses in a Laminated Composite Strip Subjected to Axial Temperature Gradients
One of the most severe problems associated with the use of laminated composite structures in thermal environments is the susceptibility to delamination due to the edge effect stresses arising from the thermal expansion mismatch between the constituent laminae. In addition, the problem may be compounded by the introduction of extreme thermal gradient effects as well. Trade studies to develop a satisfactory design for these types of thermal environments have heretofore been rather limited due to the lack of accurate analytical assessments for the edge effects that arise from these thermal loads. The predominant amount of investigation for these types of thermal gradient problems has been restricted to detailed numerical finite element analyses that do not lend to rapid concurrent engineering design processes. No analytical solution has been available to address the thermoelastic edge effects in composite laminates resulting from thermal gradients. In this paper, a combination of Airy stress functions and direct displacement functions is utilized to obtain the plane elasticity solution for the stresses and displacements in a multilayer laminated anisotropic strip subjected to a temperature gradient that is arbitrarily symmetric in the longitudinal direction. The solution cannot be guaranteed to satisfy the free edge normal traction requirement since only resultant force is enforced to zero; however, convergence for enforced zero transverse slope at the strip ends can be established, as the eigenfunctions are orthogonal. Thus the solution is exact for these edge conditions. Numerical results are presented for several examples and compared to those obtained from our own MSC/NASTRAN finite element analyses. The correlation with the finite element numerical results was determined to verify the solution and indicated application of the solution as an approximation to free edge engineering problems is very reasonable for a broad range of practical cases involving temperature gradient effects.
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