A theoretical formulation of a method to solve structural problems is
given from a general point of view. The procedure creates a mathematic
al model of typical elements taking into account the whole behavior of
the structure under concern such as static, dynamic, aerodynamic . .
. thermal actions. in analogy with other numerical methods like finite
elements, a ''library'' of models, named parameter-transfer finite el
ements (P-TFE) can be obtained for simple structures. Complex geometri
es can be approached by a discretization technique assembling the cont
ributions from each element. An application to the panel flutter probl
em is given in which the proposed method overcomes most difficulties o
f the usual techniques of solution. To assess the validity of the meth
od, a comparison with results obtained by other authors is made.