The potential of a multi-fidelity approach to gas turbine combustor design optimization

Abstract

The desire to reduce gas turbine emissions drives the use of design optimization approaches within the combustor design process. However, the relative cost of combustion simulations can prohibit such optimizations from being carried out within an industrial setting. Strategies which can significantly reduce the cost of such studies can enable designers to further improve emissions performance. The following paper investigates the application of a multi-fidelity surrogate modelling approach to the design optimization of a typical gas turbine combustor from a civil airliner engine. Results over three different case studies of varying problem dimensionality indicate that a multi-fidelity surrogate modelling based design optimization, whereby the simulation fidelity is varied by adjusting the coarseness of the mesh, can indeed improve optimization performance. These results indicate that such an approach has the potential to significantly reduce design optimization cost whilst achieving similar, or in some cases superior, design performance.

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Identifiers

ORCID for David Toal: orcid.org/0000-0002-2203-0302

ORCID for Xu Zhang: orcid.org/0000-0002-6918-1861

ORCID for Andy Keane: orcid.org/0000-0001-7993-1569

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