期刊文献+

Sectional Warping Corrective Model for Free Edge Stresses in Composite Laminates

复合材料叠层结构边缘应力分析的翘曲修正模型(英文)
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摘要 The edge stress problem in composite laminates under uniform axial extension is analyzed. The displacement distribution in three directions along the thickness are derived respectively by use of the sectional warping corrective theory, and the hierarchical displacement functions are adopted in the width direction. Finally, based on the principle of virtual work, a special finite element model for boundary layer effects is obtained. Accuracy and convergence of the solution are studied, and the present resu... The edge stress problem in composite laminates under uniform axial extension is analyzed. The displacement distribution in three directions along the thickness are derived respectively by use of the sectional warping corrective theory, and the hierarchical displacement functions are adopted in the width direction. Finally, based on the principle of virtual work, a special finite element model for boundary layer effects is obtained. Accuracy and convergence of the solution are studied, and the present resu...
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2002年第4期213-221,共9页 中国航空学报(英文版)
基金 Key Program of National Natural Science Foundation of China (1993 2 0 3 0 )
关键词 composite laminates boundary layer effects sectional warping theory hierarchical finite element methods composite laminates boundary layer effects sectional warping theory hierarchical finite element methods
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参考文献1

  • 1诸德超.论升阶谱有限元技术[J]计算结构力学及其应用,1985(03).

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