
Dr Fintan Healy
MEng, PhD
Expertise
I work on the experimental and numerical aeroelastic testing of highly flexible aircraft, developing modelling tools to evaluate nonlinear deflections and assess novel load alleviation strategies for next-generation aircraft.
Current positions
Lecturer in Aerospace Engineering
School of Civil, Aerospace and Design Engineering
Contact
Press and media
Many of our academics speak to the media as experts in their field of research. If you are a journalist, please contact the University’s Media and PR Team:
Biography
Fintan Healy is an aerospace researcher focused on the aeroelastic behaviour of highly flexible aircraft. He has a background in structural dynamics, experimental testing, and numerical modelling, developed through his engineering studies and a stint in industry.
He completed a PhD at the University of Bristol on floating wingtips—hinged wing extensions designed to reduce loads during manoeuvres. This work combined wind tunnel experiments with low-order nonlinear modelling to study how large deflections affect aircraft stability.
Since then, his research has included the conceptual design of hydrogen-powered aircraft and the influence of liquid sloshing on flight dynamics. He is currently developing techniques for predicting nonlinear instabilities in flexible structures, alongside a software framework to support the modeling and analysis of flexible aircraft. His work aims to support the design of lighter, safer, and more sustainable aircraft.
He completed a PhD at the University of Bristol on floating wingtips—hinged wing extensions designed to reduce loads during manoeuvres. This work combined wind tunnel experiments with low-order nonlinear modelling to study how large deflections affect aircraft stability.
Since then, his research has included the conceptual design of hydrogen-powered aircraft and the influence of liquid sloshing on flight dynamics. He is currently developing techniques for predicting nonlinear instabilities in flexible structures, alongside a software framework to support the modeling and analysis of flexible aircraft. His work aims to support the design of lighter, safer, and more sustainable aircraft.
Publications
Recent publications
04/01/2024Aeroelastic scaling of a high aspect ratio wing incorporating semi aeroelastic hinge
AIAA SCITECH 2024 Forum
Nonlinear Stability Analysis of Floating Wingtips with Control Surface Freeplay
AIAA SCITECH 2024 Forum
Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge
AIAA Journal
Experimental and Numerical Nonlinear Stability Analysis of Wings Incorporating Flared Folding Wingtips
Journal of Aircraft
Flight dynamics of aircraft incorporating the semi-aeroelastic hinge
Aerospace Science and Technology
Thesis
The Impact of Geometric Nonlinearities on the Behaviour of Floating Wingtips
Supervisors
Award date
23/01/2024
Teaching
I support the running of the postgraduate Master's in Aerospace Engineering.