The energy dissipation on the bow structure is calculated during a "head-on
" collision with a rigid body, using finite element analysis. Gerard's meth
od (Gerard, G., 1958. The crippling strength of compression elements. Journ
al of the Aeronautical Sciences), an empirical approach, is compared with t
he results produced by ABAQUS in terms of velocity, energy and penetrating
distance. The energy conservation theorem is applied and the contribution o
f all individual structural members in terms of elastic and plastic energy
is calculated The strain distribution is shown for those members responsibl
e for the water tightness and structural integrity of the structure. The gl
obal bending of the upper part of the bow is shown as well as the effect of
the total ship mass inertia, phenomena which have not been incorporated in
to Gerard's approach (Gerard, 1958). The final time of rest predicted from
both methods is compatible and this validates the reliability of the numeri
cal approach. (C) 2000 Elsevier Science Ltd. All rights reserved.