In order to size a glued plane assembly under low velocity impact, a m
ethod has been developed. An analytical model gives us a quick design
of the optimised dimensions. A finite element model describes the impa
ct mode contact. A viscoelasticimeter gives glue behaviour which is, t
hen, implemented in the numerical code. These models are very close to
experiment, so this method will save time by reducing the number of t
ests.