Data-driven Modelling and Linear Mean-Flow Analyses of Airfoil Instabilities in Transitional Flow Regimes (Modélisation Basée sur les Données et Approches Linéarisées pour la Prédiction des Instabilités d’un Profil d’Aile dans des Régimes d’Écoulements Transitionnels)

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Authors: Romain Peron
Cited by: 0

Abstract

This research investigates how air flows around wings when it shifts from smooth (laminar) to irregular patterns (turbulent). These complex motions can cause dangerous vibrations and loud noise in aircraft and wind turbines. While engineers increasingly rely on computer simulations to design safe and efficient systems, available models describing complex air motion are often either too slow or lack accuracy. This work explores optimisation techniques to improve the modelling these motions at a low computational cost. The findings offer a step toward creating improved tools that help engineers address noise and safety risks more effectively during design.

Fields of Study & Subjects

Model Reduction and Neural Networks Computational Fluid Dynamics and Aerodynamics Aeroelasticity and Vibration Control

Publication details

Journal / source
Swinburne figshare (Swinburne University of Technology)
Publication date
1 January 2026
Language
EN
Document type
Thesis