Analysis of out-of-plane bending in one-sided bonded repair

被引:35
|
作者
Wang, CH [1 ]
Rose, LRF [1 ]
Callinan, R [1 ]
机构
[1] Def Sci & Technol Org, Aeronaut & Maritime Res Lab, Airframes & Engines Div, Melbourne, Vic 3001, Australia
关键词
D O I
10.1016/S0020-7683(97)00129-7
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
An un-supported cracked plate repaired with a reinforcement bonded on one side may experience a considerable out-of-plane bending, resulting mainly from the load-path eccentricity. A geometrically linear analysis is presented in this paper for the crack extension force after the application of a one-sided repair. It is found that although the stress intensity factor K for a one-sided repair is higher than in two-sided repairs where there is no bending present, the key feature is retained that K does not increase indefinitely with increasing crack length, but instead approaches asymptotically a finite upper-bound corresponding to the solution for a semi-infinite crack. An analytical expression is derived for this upper bound, which provides a conservative estimate suitable for design purposes and parametric studies. This analytical solution is shown to agree well with a fully three-dimensional finite element analysis. Strategies to minimize the detrimental effect of out-of-plane bending are briefly discussed. (C) 1998 Elsevier Science Ltd.
引用
收藏
页码:1653 / 1675
页数:23
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