Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Machine Learning Based Predictions of Airfoil Aerodynamic Coefficients for Reynolds Number Extrapolations
Download
Özgören_2024_J._Phys.__Conf._Ser._2767_022049.pdf
Date
2024-01-01
Author
Özgören, Ahmet Can
Acar, Deniz Alper
Kamrak, Recep
Eriş, Görkem Mahir
Özdemir, Yasin
Sezer Uzol, Nilay
Uzol, Oğuz
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
51
views
163
downloads
Cite This
This study investigates the application of various machine learning (ML) algorithms for predicting two critical aerodynamic coefficients, i.e. the maximum lift coefficient (C l max ) and the minimum drag coefficient (C d min ), for wind turbine airfoils at any given Reynolds number. We propose to use clustering techniques to group similar airfoil shapes and use the created partitions to predict unseen airfoil properties utilizing their similarity. Here, we also represent airfoils in the PARSEC low dimensional space, rather than high dimensional airfoil points space, to remedy the small number of training data. For this purpose, an extended experimental airfoil database is created and used for training models based on five different ML algorithms. We observe that the Decision Tree Ensemble (DTE), Random Forest (RF) and multi-layer perceptron (MLP) models emerge as the most effective predictors for C l max and C d min . Testing these two ML models on three additional airfoil cases not included in the training database shows that the C l max prediction performance is generally reasonable, with error levels being around 5% on average. In contrast, the prediction error levels for C d min are usually higher, with an average of around 15%.
Subject Keywords
Airfoils
,
Aerodynamic drag
,
Decision trees
,
Decision trees
,
Forecasting
URI
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85196422848&origin=inward
https://hdl.handle.net/11511/110241
DOI
https://doi.org/10.1088/1742-6596/2767/2/022049
Conference Name
2024 Science of Making Torque from Wind, TORQUE 2024
Collections
Department of Aerospace Engineering, Conference / Seminar
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
A. C. Özgören et al., “Machine Learning Based Predictions of Airfoil Aerodynamic Coefficients for Reynolds Number Extrapolations,” Florence, İtalya, 2024, vol. 2767, Accessed: 00, 2024. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85196422848&origin=inward.