1. HICAS. High velocity impact of composite aircraft structures, CEC DG XII BRITE-EURAM Project BE 96-4238, 1998.
2. Damage modelling of the elementary ply for laminated composites;Ladevèze;Composites Science and Technology,1992
3. Interlaminar interface modelling for the prediction of delamination;Allix;Composites Structures,1992
4. Finite element methods and the progressive failure modelling of composite structures;Crisfield,1997
5. PAM-CRASH™ FE Code, Engineering Systems International, F-94578 Rungis Cedex, France.