LES informed data-driven modelling of a spatially varying turbulent diffusivity coefficient in film cooling flows
A novel data-driven approach is used to describe a spatially varying turbulent diffusivity coefficient for the Higher Order Generalised Gradient Diffusion Hypothesis (HOGGDH) closure of the turbulent heat flux to improve upon RANS cooling predictions in film cooling flows. Machine learning algorithms are trained on two film cooling flows and tested on a case of a different density and blowing ratio. The Random Forests and Neural Network algorithms successfully reproduced the LES described coefficient and the magnitude of the turbulent heat flux vector. The Random Forests model was implemented in a steady RANS solver with a k-ω SST turbulence model and applied to four cases. All cases saw improvements in the predicted Adiabatic Cooling Effectiveness (ACE) over the cooled surface compared to the standard Gradient Diffusion Hypothesis (GDH) approach, but only minor improvements in the centreline and lateral spread are seen compared to a HOGGDH model with a constant cθ of 0.6. Further improvements to cooling predictions are highlighted by extending these data-driven approaches into turbulence modelling to improve flow field predictions.
Funding
EPSRC Centre for Doctoral Training in Gas Turbine Aerodynamics
Engineering and Physical Sciences Research Council
Find out more...Proposal for a Tier 2 Centre - HPC Midlands Plus
Engineering and Physical Sciences Research Council
Find out more...History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Published in
Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and ExpositionVolume
7B: Heat TransferSource
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition (GT2020)Publisher
American Society of Mechanical Engineers (ASME)Version
- VoR (Version of Record)
Rights holder
© ASMEPublisher statement
This paper was first published in the Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition and is available in the ASME Digital Library at https://doi.org/10.1115/GT2020-14789.Publication date
2021-01-11Copyright date
2020ISBN
9780791884171Publisher version
Other identifier
Paper No: GT2020-14789, V07BT12A029Language
- en