A numerical-experimental method for identification of elastic properties of
laminated composites from the experimental results is developed. It is pro
posed to use the method of experiment design and the response surface appro
ach to solve the identification (inverse) problems. The response surface ap
proximations are obtained by using the information on the behavior of a str
ucture in the reference points of the experiment design. The finite element
modeling of the structure is performed only in the reference points. There
fore, a significant reduction (about 50-100 times) in calculations of the i
dentification functional can be achieved in comparison with the conventiona
l methods of minimization. The functional to be minimized describes the dif
ference between the measured and numerically calculated eigenfrequencies of
structure. By minimizing the functional the identification parameters are
obtained. It was shown that identification functional is convex if the stif
fness matrix linearly depends on unknown parameters. The method is employed
to identify the elastic properties of cross-ply laminates from the measure
d eigenfrequencies of composite plates. (C) 2001 Elsevier Science Ltd. All
rights reserved.