Machine Learning for the Development of Data-Driven Turbulence Closures in Coolant Systems

Author:

Hammond James1,Montomoli Francesco1,Pietropaoli Marco1,Sandberg Richard D.2,Michelassi Vittorio3

Affiliation:

1. UQLab, Department of Aeronautics, Imperial College London, London SW7 2AZ, UK

2. Department of Mechanical Engineering, University of Melbourne, Parkville, Victoria 3010, Australia

3. Baker Hughes, Florence 50127, Italy

Abstract

Abstract This work shows the application of Gene Expression Programming to augment RANS turbulence closures for flows though complex geometries. Specifically, an optimized internal cooling channel of a turbine blade, designed for additive manufacturing. One of the challenges in internal cooling design is the heat transfer accuracy of the RANS formulation in comparison to higher fidelity methods, which are still not used in design on account of their computational cost. However, high fidelity data can be extremely valuable for improving current lower fidelity models and this work shows the application of data-driven approaches to develop turbulence closures for an internally ribbed duct. Different approaches are compared and the results of the improved model are illustrated; first on the same geometry, and then for an unseen predictive case. The work shows the potential of using data-driven models for accurate heat transfer predictions even in non-conventional configurations and indicates the ability of closures learnt from complex flow cases to adapt successfully to unseen test cases.

Funder

Engineering and Physical Sciences Research Council

Publisher

ASME International

Subject

Mechanical Engineering

Reference33 articles.

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2. A Survey of the Design Methods for Additive Manufacturing to Improve Functional Performance;Tang;Rapid. Prototyp. J.,2016

3. Three-Dimensional Fluid Topology Optimization for Heat Transfer;Pietropaoli;Struct. Multidiscipl. Optim.,2018

4. Direct Numerical Simulation, Up-Scaled Measurement and RANS Analysis of Additively and Conventionally Manufactured Internal Turbine Cooling Passages;Kunz,2018

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