Skip to main content
Article thumbnail
Location of Repository

Topology optimization of aircraft with non-conventional configurations

By J. Eves, V.V. Toropov, H.M. Thompson, P.H. Gaskell, J.J. Doherty and J. Harris


The optimal structural layouts of new aircraft configurations such as the flying wing and blended wing body (BWB) are not yet understood. These new configurations may require quite different design methods from those\ud used conventionally and one promising alternative that is attracting increasing levels of interest is topology optimization, an approach which is significantly different from conventional approaches and valuable in applications where there is little or no collective knowledge on what an optimal structure may be. This paper proposes a new approach for using topology optimization for developing conceptual designs of an aircraft's structural layout. Its aim is to overcome some of the problems associated with the inclusion of local displacement and buckling constraints. The approach is applied to the design of a BWB UAV’s wing and is shown to offer significant advantages over a baseline design.\u

Year: 2009
OAI identifier:

Suggested articles

To submit an update or takedown request for this paper, please submit an Update/Correction/Removal Request.