The dynamic stiffness method applies mainly to excitations of harmonic noda
l forces. For distributed loads, modal analysis is generally required. In t
he case of a clamped-clamped beam, the modal decomposition of a uniformly d
istributed load by the eigen beam functions inherits slow convergence becau
se the finite loads at the beam-ends cannot be represented efficiently by t
he zero deflection and zero slope of the clamped-clamped beam functions. Th
e computed reactions at the supports do not converge at all. The problem is
eliminated in this paper by using the finite element interpolation functio
ns for the distributed load. If the distributed load is adequately represen
ted, explicit exact solutions are found. Otherwise, the residual load is ex
panded in the modal space. As the residual modal force is much smaller and
agrees well with the clamped-clamped conditions, fast convergence is achiev
ed. By means of the principle of superposition, a structure with members ha
ving distributed loads can be analyzed by two systems: one is associated wi
th the individual members having distributed loads and the other is associa
ted with resulting equivalent nodal forces. The required frequency function
s are given for all possible cases. The results presented are exact if the
load is interpolated adequately by finite element shape functions. Both det
erministic and random loads are considered. Closed-form solutions are obtai
ned for the first time. (C) 2001 Academic Press.