A Rayleigh quotient approximation is applied to the design of structur
es while guarding against elastic instability. It approximates bucklin
g eigenvalues by separately estimating the modal strain energy due to
the linear and geometric stiffness of the structure. Previously used d
uring structural optimization for the fundamental natural eigenvalue,
the Rayleigh quotient approximation is derived for the buckling design
problem for the first time. The critical buckling load is found by so
lving the eigenvalue problem that arises by considering the geometric
nonlinearity of the deforming structure. Rayleigh's principle is used
to justify the choice of intermediate design variables for approximati
ng terms in the Rayleigh quotient. A truss model illustrates the impor
tance of the design space chosen for approximating the modal strain en
ergy. A beam-column, two plane frames, and a space frame are used to v
erify the formulation. Special attention is paid to difficult bimodal
optima.