The sizes of Fiber Metal Laminate (FML) sheets available can be increased c
onsiderably with the application of the splicing concept. A disadvantage of
this concept can be the occurrence of delamination caused by load transfer
over the splice. An experimental program has been carried out to investiga
te the delamination behavior for different splicing geometries and metal la
yer thicknesses. Griffith's energy criterion is applied to calculate a dela
mination resistance for the configurations tested. The approach is modified
for the presence of residual stresses in the laminate and plasticity in th
e metal layers. (C) 1999 Elsevier Science Ltd. All rights reserved.