Robust Algorithm Software for NACA 4-Digit Airfoil Shape Optimization Using the Adjoint Method

Optimizing the aerodynamic shape of an airfoil is a critical concern in the aviation industry. The introduction of flexible airfoils has allowed the shape of the airfoil to vary, depending on the flight conditions. Therefore, in this study, we propose an algorithm that is capable of robustly optimiz...

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Bibliographic Details
Main Authors: Naser Tanabi, Agesinaldo Matos Silva, Marcosiris Amorim Oliveira Pessoa, Marcos Sales Guerra Tsuzuki
Format: Article
Language:English
Published: MDPI AG 2023-03-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/13/7/4269