2012 ©
             Publication
Journal Publication
Title of Article Airfoil Shape Optimisation Using a Multi-Fidelity Surrogate-Assisted Metaheuristic with a New Multi-Objective Infill Sampling Technique 
Date of Acceptance 17 March 2023 
Journal
     Title of Journal CMES : Access Computer Modeling in Engineering & Sciences 
     Standard SCOPUS 
     Institute of Journal Tech Science Press 
     ISBN/ISSN ISSN:1526-1506 
     Volume 2023 
     Issue ID: 28632 
     Month March
     Year of Publication 2023 
     Page  
     Abstract This work presents multi-fidelity multi-objective infill-sampling surrogate-assisted optimization for airfoil shape optimization. The optimization problem is posed to maximize the lift and drag coefficient ratio subject to airfoil geometry constraints. Computational Fluid Dynamic (CFD) and XFoil tools are used for high and low-fidelity simulations of the airfoil to find the real objective function value. A special multi-objective sub-optimization problem is proposed for multiple points infill sampling exploration to improve the surrogate model constructed. To validate and further assess the proposed methods, a conventional surrogate-assisted optimization method and an infill sampling surrogate-assisted optimization criterion are applied with multi-fidelity simulation, while their numerical performance is investigated. The results obtained show that the proposed technique is the best performer for the demonstrated airfoil shape optimization. According to this study, applying multi-fidelity with multi-objective infill sampling criteria for surrogate-assisted optimization is a powerful design tool. 
     Keyword Multi-fidelity modelling; differential evolution; kriging; infill sampling criteria; metaheuristics 
Author
617040031-0 Ms. CHO MAR AYE [Main Author]
Engineering Doctoral Degree

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