论文信息 - ADVANCES IN BEM FOR CRACK GROWTH MODELLING

ADVANCES IN BEM FOR CRACK GROWTH MODELLING

This paper presents recent advances in the dual boundary element method as applied to modelling crack growth in context of damage tolerance assessment of aircraft panels. The work presented include two- and three-dimensional problems as well as thin plates and shells. Several examples are presented to demonstrate the effectiveness of the method in modeling linear and nonlinear fracture problems.

M. H. Aliabadi

[1] M. H. Aliabadi,et al. Boundary Element Analysis of Fatigue Crack Propagation in Stiffened Panels , 1998 .

[2] D. Rooke,et al. The dual boundary element method: Effective implementation for crack problems , 1992 .

[3] Tatacipta Dirgantara,et al. Numerical simulation of fatigue crack growth in pressurized shells , 2002 .

[4] D. P. Rooke,et al. Dual boundary element incremental analysis of crack propagation , 1993 .

[5] Buckling of Cracked Plates , 2003 .

[6] M. H. Aliabadi,et al. Crack growth analysis for multi-layered airframe structures by boundary element method , 2004 .

[7] M. H. Aliabadi,et al. THREE-DIMENSIONAL CRACK GROWTH SIMULATION USING BEM , 1994 .

[8] Tatacipta Dirgantara,et al. Crack Growth analysis of plates Loaded by bending and tension using dual boundary element method , 2000 .

[9] M. Aliabadi,et al. Dual boundary element method for three-dimensional fracture mechanics analysis , 1992 .

[10] Wole Soboyejo,et al. A STUDY OF THE INTERACTION AND COALESCENCE OF TWO COPLANAR FATIGUE CRACKS IN BENDING , 1989 .

[11] Ferri M.H.Aliabadi,et al. Non-Linear Fracture Mechanics Analysis of Fuselage Panels Using BEM , 2003 .