Record number :
1346145
Title of article :
Modelling bearing failure in countersunk composite joints under quasi-static loading using 3D explicit finite element analysis
Author/Authors :
B. Egan، نويسنده , , M.A. McCarthy، نويسنده , , R.M. Frizzell، نويسنده , , P.J. Gray، نويسنده , , C.T. McCarthy، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2014
Pages :
15
From page :
963
To page :
977
Abstract :
Three-dimensional explicit finite element modelling is used to predict the quasi-static bearing response of typical countersunk composite fuselage skin joints. In order to accurately simulate bearing failure, a user-defined 3D composite damage model was formulated for Abaqus/Explicit and included Puck failure criteria, a nonlinear shear law and a crack band model to mitigate mesh sensitivity. A novel approach was developed to employ characteristic element lengths which account for the orientation of composite ply cracks in the Abaqus/Explicit solver. Resulting models accurately predicted initial joint sticking behaviour and the elastic loading response of single-bolt and three-bolt joints, but preliminary predictions of bearing failure onset were overly-conservative. Improved failure predictions were obtained by utilising a fracture energy for compressive fibre failure which was considered more relevant for simulating bearing damage. The explicit models were exceptionally robust, showing capability to predict extensive hole crushing. Methods of dramatically improving joint model efficiency were highlighted.
Keywords :
Finite element analysis , Progressive damage , Explicit dynamics , Carbon-epoxy , Bolted joints , Countersunk fasteners
Journal title :
COMPOSITE STRUCTURES
Link To Document :