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Experimental and analytical investigation of failure behavior in satin-weave composites and uni-weave/satin-weave hybrid composites.

机译:缎纹编织复合材料和单织/缎纹编织复合材料破坏行为的实验和分析研究。

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The objectives of this dissertation research are to identify the failure modes in satin-weave composites and uni-weave/satin weave hybrid composites under different mechanical load and environmental conditions and develop a better understanding of the factors that affect failure behavior.; To reach these aims, various experimental techniques have been utilized to characterize damage initiation and development under tension and compression. A three-dimensional Finite Element Analysis was used to understand the observed damage behavior. The effects of hygrothermal aging, free surfaces and hybridization on failure mechanisms were also investigated.; Experimental observations indicate that the damage initiation and development under uniaxial tension are different between satin-weave composites and uni-weave/satin-weave hybrid composites. Compressive failure strains and failure modes are affected by the lay-up of the composite laminates. Fiber bundle kinking induced by intra-ply delamination was the dominant failure modes in the satin-weave ([S] 12) and the axial hybrid composites ([(0/S)3/0/S/0/(S/0) 3]). However, the failure mode is fiber crushing for the transverse hybrid composites ([(90/S)3/90/S/90/(S/90)3]). The deterioration of the interfacial adhesion as a result of hygrothermal aging is the most important factor contributing to the degradation of the mechanical performance of BMI composites, especially for compressive strength.; Finite element results successfully explain some experimental observations. The stress distributions in the surface layer were found to be independent of the thickness of the laminates for the symmetrically stacked laminates. However, for simply stacked laminates, the response of the surface layers is quite sensitive to the thickness except for fairly thick laminate. The hybridization effects on the stress distribution are also largely dependent on the degree of waviness and the stacking configurations.
机译:本论文的研究目的是确定缎纹编织复合材料和单织/缎纹编织复合材料在不同的机械载荷和环境条件下的破坏模式,并更好地理解影响破坏行为的因素。为了达到这些目的,已经使用了各种实验技术来表征在拉伸和压缩下的破坏的发生和发展。使用三维有限元分析来了解观察到的损伤行为。还研究了湿热老化,自由表面和杂交对破坏机理的影响。实验观察表明,缎纹编织复合材料和单织/缎纹编织复合材料在单轴拉伸下的损伤萌生和发展是不同的。压缩破坏应变和破坏模式受复合材料层压板放置的影响。层间分层引起的纤维束扭结是缎纹编织([S] 12 )和轴向混杂复合材料([(0 / S) 3 / 0 / S / 0 /(S / 0) 3 ])。但是,失效模式是横向混合复合材料的纤维破碎([(90 / S) 3 / 90 / S / 90 /(S / 90) 3 ]) 。湿热老化导致的界面粘合力下降是导致BMI复合材料机械性能下降的最重要因素,尤其是抗压强度下降。有限元结果成功地解释了一些实验观察。对于对称堆叠的层压板,发现表面层中的应力分布与层压板的厚度无关。然而,对于简单堆叠的层压板,除了相当厚的层压板之外,表面层的响应对厚度非常敏感。杂化对应力分布的影响在很大程度上还取决于波纹度和堆叠构型。

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