TY - JOUR
T1 - The effect of a spew fillet on adhesive stress distributions in laminated composite single-lap joints
AU - Tsai, M. Y.
AU - Morton, J.
PY - 1995
Y1 - 1995
N2 - A laminated composite single-lap joint without a spew fillet, subjected to tensile loading, is investigated experimentally and numerically. By directly comparing the experimentally- and numerically-determined deformations of the single-lap joints with and without a fillet, the effect of a spew fillet on adhesive stress distributions is discussed. Moiré interferometry is used to measure the in-plane surface deformation of the overlap region of the test specimens. The deformation interactions of the laminated adherends, adhesive layer and a fillet are documented in the form of orthogonal components of the displacement fields (u and v). Two-dimensional, geometrically linear and nonlinear finite element analyses are performed to simulate the mechanical response of the laminated composite single-lap joint and the effect of a spew fillet. Experimental and numerical results indicate that the adhesive shear and peel strain (stress) concentrations can be reduced greatly by introducing a fillet at the end of the overlap, and these concentrations are affected by the geometrically nonlinear deformation of the single-lap joint.
AB - A laminated composite single-lap joint without a spew fillet, subjected to tensile loading, is investigated experimentally and numerically. By directly comparing the experimentally- and numerically-determined deformations of the single-lap joints with and without a fillet, the effect of a spew fillet on adhesive stress distributions is discussed. Moiré interferometry is used to measure the in-plane surface deformation of the overlap region of the test specimens. The deformation interactions of the laminated adherends, adhesive layer and a fillet are documented in the form of orthogonal components of the displacement fields (u and v). Two-dimensional, geometrically linear and nonlinear finite element analyses are performed to simulate the mechanical response of the laminated composite single-lap joint and the effect of a spew fillet. Experimental and numerical results indicate that the adhesive shear and peel strain (stress) concentrations can be reduced greatly by introducing a fillet at the end of the overlap, and these concentrations are affected by the geometrically nonlinear deformation of the single-lap joint.
UR - https://www.scopus.com/pages/publications/0029180360
U2 - 10.1016/0263-8223(95)00059-3
DO - 10.1016/0263-8223(95)00059-3
M3 - 文章
AN - SCOPUS:0029180360
SN - 0263-8223
VL - 32
SP - 123
EP - 131
JO - Composite Structures
JF - Composite Structures
IS - 1-4
ER -