posted on 2011-01-17, 11:31authored byDavid C. Panni
This thesis documents fundamental new research in to a specific application of structural
box-section beams, for which weight reduction is highly desirable. It is proposed and
demonstrated that the weight of these beams can be significantly reduced by using
advanced, laminated fibre-reinforced composites in place of steel. Of the many issues
raised during this investigation two, of particular importance, are considered in detail;
(a) the detection and quantification of damage in composite structures and (b) the
optimisation of laminate design to maximise the performance of loaded composite
structuress ubject to given constraints. It is demonstrated that both these issues can be
formulated and solved as optimisation problems using the finite element method, in
which an appropriate objective function is minimised (or maximised). In case (a) the difference in static response obtained from a loaded structure containing damage and an equivalent mathematical model of the structure is minimised by iteratively updating the model. This reveals the damage within the model and subsequently allows the residual properties of the damaged structure to be quantified. Within the scope of this work is the ability to resolve damage, that consists of either
penny-shaped sub-surface flaws or tearing damage of box-section beams from surface
experimental data. In case (b) an objective function is formulated in terms of a given structural response, or combination of responses that is optimised in order to return an optimal structure, rather than just a satisfactory structure.
For the solution of these optimisation problems a novel software tool, based on the
integration of genetic algorithms and a commercially available finite element (FE)
package, has been developed. A particular advantage of the described method is its
applicability to a wide range of engineering problems. The tool is described and its
effectiveness demonstrated with reference to two inverse damage detection and
quantification problems and one laminate design optimisation problem.
The tool allows the full suite of functions within the FE software to be used to solve
non-convex optimisation problems, formulated in terms of both discrete and continuous variables, without explicitly stating the form of the stiffness matrix. Furthermore, a priori
knowledge about the problem may be readily incorporated in to the method.
History
School
Mechanical, Electrical and Manufacturing Engineering