A general formulation based on the transfer matrix is presented to calculat
e the sensitivity derivatives of eigenvalue problems of one-dimensional str
uctural systems. The method is equally applicable to any discrete or distri
buted system of one variable. The formulation is applied to determine the s
ensitivity derivatives of eigendata of a rotating helicopter blade and also
to an optimization problem of a cantilever beam with frequency constraints
. It is found that the computational efficiency of the present method is su
perior to those of the existing methods by an order of magnitude and that t
his efficacy improves with increasing numbers of design parameters and degr
ees of freedom.