On the calibration of the intermittency transition turbulence model for wind turbine airfoil by machine learning algorithm
On the calibration of the intermittency transition turbulence model for wind turbine airfoil by machine learning algorithm
Fully turbulent wind turbine computational fluid dynamics simulations have been shown to overpredict the aerodynamic performances. To ensure a correct prediction, modelling of flow transition from laminar to turbulent over the blade is becoming necessary. While several transitional turbulence models exist, the one equation intermittency γ model coupled with the kω SST turbulence model offers a simple framework against wide range of generic industrial application. However, the model is yet to be calibrated for certain cases especially for external aerodynamic flows at low turbulent intensity. In this paper, the epistemic uncertainty of several model constants related to the transitional triggering function is investigated using machine learning. The procedure is demonstrated for the S809 airfoil. It was found that:(a) some coefficients have a large impact on the results at high angles of attack, causing fluctuation of the results and (b) the calibration of the turbulence model is influenced by several factors, for instance, the solver limiters.
International Council of the Aeronautical Sciences
Abd Bari, Muhammad Anas
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Da Ronch, Andrea
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Panzeri, Marco
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Drofelnik, Jernej
e785f695-61ef-4afc-bf0a-9dc7966f5516
September 2018
Abd Bari, Muhammad Anas
7110ef35-7471-4699-b95f-0d418523da9e
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Panzeri, Marco
f2ca7e93-7087-4f38-a94c-26a7c1a67536
Drofelnik, Jernej
e785f695-61ef-4afc-bf0a-9dc7966f5516
Abd Bari, Muhammad Anas, Da Ronch, Andrea, Panzeri, Marco and Drofelnik, Jernej
(2018)
On the calibration of the intermittency transition turbulence model for wind turbine airfoil by machine learning algorithm.
In Proceedings of the 31st Congress of the International Council of the Aeronautical Sciences.
International Council of the Aeronautical Sciences.
10 pp
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
Fully turbulent wind turbine computational fluid dynamics simulations have been shown to overpredict the aerodynamic performances. To ensure a correct prediction, modelling of flow transition from laminar to turbulent over the blade is becoming necessary. While several transitional turbulence models exist, the one equation intermittency γ model coupled with the kω SST turbulence model offers a simple framework against wide range of generic industrial application. However, the model is yet to be calibrated for certain cases especially for external aerodynamic flows at low turbulent intensity. In this paper, the epistemic uncertainty of several model constants related to the transitional triggering function is investigated using machine learning. The procedure is demonstrated for the S809 airfoil. It was found that:(a) some coefficients have a large impact on the results at high angles of attack, causing fluctuation of the results and (b) the calibration of the turbulence model is influenced by several factors, for instance, the solver limiters.
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Published date: September 2018
Venue - Dates:
31st Congress of the International Council of the Aeronautical Sciences (ICAS 2018), , Belo Horizonte, Brazil, 2018-09-09 - 2018-09-14
Identifiers
Local EPrints ID: 483970
URI: http://eprints.soton.ac.uk/id/eprint/483970
PURE UUID: 38479b6d-67f0-4629-ae49-7aa3cd7308d2
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Date deposited: 08 Nov 2023 17:50
Last modified: 18 Mar 2024 03:25
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Contributors
Author:
Muhammad Anas Abd Bari
Author:
Marco Panzeri
Author:
Jernej Drofelnik
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