Affiliation:
1. Department of Mechanical Engineering, Grattan Street, University of Melbourne, Parkville, 3010, Australia
Abstract
Accurate prediction of the wall temperature downstream of the trailing-edge slot is crucial to designing turbine
blades that can withstand the harsh aerothermal environment in a modern gas turbine. Because of their computational
efficiency, industry relies on low-fidelity tools like RANS for momentum and thermal field calculations, despite their
known underprediction of wall temperature. In this paper, a novel framework using a branch of machine learning, geneexpression
programming (GEP) [Zhao et al. 2020, J. Comp. Physics, 411:109413] is used to develop closures for the
turbulent heat-flux to improve upon this underprediction. In the original use of GEP (“frozen” approach), the turbulent
heat-flux from a high-fidelity database was used to evaluate the fitness of the candidate closures during the symbolic
regression, however, the resulting closure had no information of the temperature field during the optimisation process.
In this work, the regression process of the GEP instead incorporates RANS calculations to evaluate the fitness of the
candidate closures. This allows the inclusion of the temperature field from RANS to advance the iterative regression,
leading to a more integrated heat-flux closure development, and consequently more accurate and robust models. The
GEP-based CFD-driven framework is demonstrated on a trailing edge slot configuration with three blowing ratios. Full
a posteriori predictions from the new closures are compared to high-fidelity reference data and both conventional RANS
closures and closures obtained from the “frozen” approach.
Publisher
Global Power and Propulsion Society
Cited by
6 articles.
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