Simulations of stretch flange forming operations are undertaken using expli
cit dynamic finite element calculations utilizing various quadratic and non
-quadratic yield criteria. Both circular and square cut-out blanks are inve
stigated with corresponding circular and square punches. Simple stretch fla
nges are considered, utilizing a single punch to expand the cut-out, as wel
l as z-flanges, which employ a back-up punch to form the second bend needed
in the z-flange profile. Results from a model of an automotive inner compo
nent incorporating a cutout with stretch flange corner features are also pr
esented. Predictions utilizing the Barlat-89 criterion are shown to accurat
ely capture the effect of yield anisotropy (R-value). The predicted strains
from the corner regions of square cut-out stretch flange laboratory specim
ens are shown to be similar to those within the automotive inner panel, sup
porting the use of laboratory-scale stretch flange experiments to simulate
the larger panels. Measured limit strains from the stretch flange formabili
ty experiments are compared to forming limit diagram (FLD) data from dome s
pecimens. Stretch flange formability is shown to exceed allowable levels pr
edicted using a classical FLD approach, particularly for simple stretch fla
nges, indicating that the FLD approach is overly conservative. (C) 2000 Els
evier Science Ltd. All rights reserved.