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.
参考文献
[1] | European Space Research Technology Centre.Composites design handbook for space structure application[M].ESA Publications Division,1988 |
[2] | Xiaoyu Li;Dahsin Liu .Zigzag Theory for Composite Laminates[J].AIAA journal,1995(6):1163-1165. |
[3] | Maenghyo Cho;R Reid Parmerter .Efficient higher order composite plate theory for general lamination configurations[J].AIAA Journal,1993,31(07) |
[4] | Chun Ying Lee;Dahsin Liu .An interlaminar stress continuity theory for laminated composite analysis[J].Computers and Structures,1992,42(01):69-78. |
[5] | Wu CML.Nonlinear analysis of edge effects in angle ply laminates[J].Computers and Structures,1987(25):787-798. |
[6] | Larry B Lessard .Three dimensional stress analysis of free edge effects in a simple composite cross ply laminate[J].International Journal of Solids and Structures,1994,33(15):2243-2259. |
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