The dynamic response of multiple-degree-of-freedom nonlinear structure
s is usually determined by numerical integration of the equations of m
otion, an approach which is computationally very expensive for steady-
state response analysis of large structures. In this paper, an alterna
tive semianalytical quasilinear method based on the describing functio
n formulation is proposed for the harmonic response analysis of struct
ures with symmetrical nonlinearities. The equations of motion are conv
erted to a set of nonlinear algebraic equations and the solution is ob
tained iteratively. The linear and nonlinear parts of the structure ar
e dealt with separately, the former being represented by the constant
linear receptance matrix [alpha], and the latter by the generalized qu
asilinear matrix [DELTA] which is updated at each iteration. A special
technique that reduces the computation time significantly when the no
nlinearities are localized is used with success to analyze large struc
tures. The proposed method is fully compatible with standard modal ana
lysis procedures. Several examples dealing with cubic stiffness, piece
wise linear stiffness, and coulomb friction type of nonlinearities are
presented in the case of a ten-degree-of-freedom structure.