Wing Flutter Laboratory
Do you want to see an experimental Investigation of Aeroelastic Behaviour in a Highly Flexible Wing?
Nottingham Trent University | 2025–2026
Module: Advanced Dynamics and Vibration
Project Type: Experimental Aerodynamics and Aeroelasticity
Team Size: 5
Equipment: Low-Speed Wind Tunnel, Three-Component Force Balance, Flexible Polymer Wing
Airfoil Optimisation and Aerodynamic Analysis
Do you want to see a computational investigation of parametric airfoil geometries using CFD?
Nottingham Trent University | 2025–2026
Module: Industrial Design and Product Case Studies
Project Type: Computational Fluid Dynamics and Aerodynamic Optimisation
Team Size: 5
Individual Role: CFD Modelling, Mesh Independence Investigation, Residual Convergence and Aerodynamic Analysis
Software: Autodesk Fusion 360, ANSYS CFX, Microsoft Excel
Methods: Latin Hypercube Sampling, Parametric Modelling, Mesh Independence, Residual Convergence Analysis
Aircraft Longitudinal Stability and Flight Test Analysis
Do you want to see an experimental investigation of static and manoeuvre stability using the Saab 340B+
Nottingham Trent University / Cranfield University | 2025–2026
Module: Advanced Dynamics and Vibration
Project Type: Experimental Flight Testing and Aircraft Stability Analysis
Aircraft: Saab 340B+
Facility: Cranfield University National Flying Laboratory Centre
Individual Role: Flight Test Task Specialist, Experimental Data Collection and Independent Stability Analysis
Methods: Aircraft Weight and Balance, Stability Derivatives, Linear Regression, Neutral Point and Manoeuvre Point Estimation
