Classical RANS turbulence models have known deficiencies when applied to jets in crossflow. Identifying the linear Boussinesq stress-strain hypothesis as a major contribution to erroneous prediction, we consider and contrast two machine learning frameworks for turbulence model development. Gene Expression Programming, an evolutionary algorithm that employs a survival of the fittest analogy, and a Deep Neural Network, based on neurological processing, add non-linear terms to the stress-strain relationship. The results are Explicit Algebraic Stress Model-like closures. High fidelity data from an inline jet in crossflow study is used to regress new closures. These models are then tested on a skewed jet to ascertain their predictive efficacy. For both methodologies, a vast improvement over the linear relationship is observed.
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ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition
June 26–30, 2017
Charlotte, North Carolina, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5079-4
PROCEEDINGS PAPER
A Comparative Study of Contrasting Machine Learning Frameworks Applied to RANS Modeling of Jets in Crossflow
Jack Weatheritt,
Jack Weatheritt
University of Melbourne, Parkville, Australia
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Richard D. Sandberg,
Richard D. Sandberg
University of Melbourne, Parkville, Australia
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Julia Ling,
Julia Ling
Sandia National Laboratories, Livermore, CA
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Gonzalo Saez,
Gonzalo Saez
Université de Toulouse, Toulouse, France
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Julien Bodart
Julien Bodart
Université de Toulouse, Toulouse, France
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Jack Weatheritt
University of Melbourne, Parkville, Australia
Richard D. Sandberg
University of Melbourne, Parkville, Australia
Julia Ling
Sandia National Laboratories, Livermore, CA
Gonzalo Saez
Université de Toulouse, Toulouse, France
Julien Bodart
Université de Toulouse, Toulouse, France
Paper No:
GT2017-63403, V02BT41A012; 12 pages
Published Online:
August 17, 2017
Citation
Weatheritt, J, Sandberg, RD, Ling, J, Saez, G, & Bodart, J. "A Comparative Study of Contrasting Machine Learning Frameworks Applied to RANS Modeling of Jets in Crossflow." Proceedings of the ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. Volume 2B: Turbomachinery. Charlotte, North Carolina, USA. June 26–30, 2017. V02BT41A012. ASME. https://doi.org/10.1115/GT2017-63403
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