Rapid Prediction of Ice Accretion on Swept Wings Based on Proper Orthogonal Decomposition and Surrogate Modelling

Numerical simulations of three-dimensional airfoil icing are computationally intensive, with icing complexities on swept wings surpassing those on straight wings. To enable rapid and accurate ice formation predictions on swept wings, this study proposes a prediction methodology integrating proper or...

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Bibliographic Details
Main Authors: J. Du, Q. Guo, Y. Yue, Y. Ma, H. Cheng
Format: Article
Language:English
Published: Isfahan University of Technology 2025-06-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Online Access:https://www.jafmonline.net/article_2689_37f27db8e5790313a3953fae7e411fa1.pdf
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