Multi-Fidelity Surrogate-Assisted Aerodynamic Optimization of Aircraft Wings

Multi-Fidelity Surrogate-Assisted Aerodynamic Optimization of Aircraft Wings

This paper presents a multi-fidelity optimization procedure for aircraft wing design, implemented in the early stages of the aircraft design process. Since wing shape is a key factor that influences aerodynamic performance, having an accurate estimate of its efficiency at the conceptual design phase...

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Bibliographic Details
Main Authors: Eleftherios Nikolaou, Spyridon Kilimtzidis, Vassilis Kostopoulos
Format: Article
Language:English
Published: MDPI AG 2025-04-01
Series:Aerospace
Subjects:
aircraft wings
low-fidelity aerodynamics
Computational Fluid Dynamics (CFD)
aircraft conceptual design
aircraft aerodynamics
multi-fidelity optimization
Online Access:https://www.mdpi.com/2226-4310/12/4/359
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