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正交层合板压缩条件下平均层间剪应力计算 被引量:1

ANALYTIC SOLUTIONS TO MEAN INTERLAMINAR SHEAR STRESS OF CROSS-PLY LAMINATE UNDER COMPRESSION LOADS
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摘要 根据正交层合板在压缩载荷作用下的泊松效应和变形协调原理,分析了平均层间剪应力的产生机制,并建立了平均层间剪应力的解析模型。算例分析表明纵横铺层比k=1时,层间剪应力最大,k值大于3时可有效降低层间剪应力;层间剪应力与平均压应力和受压截面宽厚比成正比关系,需要根据实际情况选取合适的k值和厚宽比以有效降低平均层间剪应力。 according to Poisson effect and deformation coordination mechanism of the cross-ply laminates under compression loads, the mean interlaminar shear stress mechanism is analyzed and shear stress analytic model constructed. The computational examples show that the interlaminar shear stress reaches maximum when longitudinal transverse plies ratio k = 1 and interlaminar shear stress decreases effectively when k 〉 3. The interlaminar shear stress is proportional to even compression stress and thickness-width ratio of the compressed section. It needs choosing a suitable longitudinal transverse plies ratio and thickness-width ratio to decrease the even interlaminar stress.
出处 《玻璃钢/复合材料》 CAS CSCD 北大核心 2006年第3期3-6,共4页 Fiber Reinforced Plastics/Composites
基金 国家863项目(2003AA724052)
关键词 正交层合板 层间剪应力 泊松效应 变形协调 cross-ply laminate interlaminar shear stress Poisson effect deformation coordination
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参考文献6

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同被引文献14

  • 1蒋邦海,张若棋.碳纤维织物增强树脂复合材料准静态压缩力学性能实验[J].强度与环境,2005,32(3):39-44. 被引量:4
  • 2蒋邦海,张若棋.一种碳纤维织物增强复合材料的层间冲击拉伸力学性能实验研究[J].复合材料学报,2005,22(5):107-112. 被引量:5
  • 3杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:1054
  • 4赵稼祥.民用航空和先进复合材料[J].高科技纤维与应用,2007,32(2):6-10. 被引量:40
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