A Comparison of Modern Metaheuristics for Multi-Objective Optimization of Transonic Aeroelasticity in a Tow-Steered Composite Wing

A Comparison of Modern Metaheuristics for Multi-Objective Optimization of Transonic Aeroelasticity in a Tow-Steered Composite Wing

This study proposes a design procedure for the multi-objective aeroelastic optimization of a tow-steered composite wing structure that operates at transonic speed. The aerodynamic influence coefficient matrix is generated using the doublet lattice method, with the steady-state component further refi...

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Bibliographic Details
Main Authors: Kantinan Phuekpan, Rachata Khammee, Natee Panagant, Sujin Bureerat, Nantiwat Pholdee, Kittinan Wansasueb
Format: Article
Language:English
Published: MDPI AG 2025-01-01
Series:Aerospace
Subjects:
tow steer composite
aeroelastic analysis
metaheuristic optimization
finite element method
panel aerodynamics method
Online Access:https://www.mdpi.com/2226-4310/12/2/101
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