Presents a simple heuristic optimization algorithm to determine weight-mini
mal laminate structures. The algorithm is based on an inverted form of grow
th strategy, where material is removed in areas with low stresses. In the p
resented algorithm the removal of material is performed in a layerwise mann
er in areas with low stress or in areas where the layer orientation angle d
iffers significantly from the principal stress direction. In order to get a
production-adapted structure, the layer orientation angles of the availabl
e individual plies are not modified and the material is removed only locall
y in the respective plies Contrary to a more formal mathematical optimizati
on no sensitivity analyses are needed by the procedure outlined so far and
this keeps the corresponding numerical effort reasonably low. The structura
l analyses have been performed by the Finite Element Program ANSYS and the
outlined heuristic algorithm has been implemented by ANSYS-MACROS. Several
examples of rectangular laminate plates show the effectiveness of the prese
nt algorithm.