Dylan Dooner

Dr. Dylan Dooner is a Researcher in the Hypersonic Vehicles Group at the University of New South Wales (UNSW) Canberra. His work focuses on fluid-thermal-structural interactions (FTSI), particularly in hypersonic aerothermodynamics, thermal-structural modeling, and subsonic aeroelasticity. He holds a Researcher academic rank and is affiliated with the Hypersonic Vehicles Group, contributing to advanced aerospace engineering challenges.

His research interests include hypersonic propulsion systems, shock-boundary layer interactions, and the development of coupled numerical models for aeroelastic analysis. Notable projects involve wind tunnel model design for hypersonic flow studies and the investigation of nonlinear structural dynamics in high-speed environments.

Dr. Dooner has authored multiple conference papers on topics such as conformal heater characterization, coupled ONERA-EDLIN models, and flutter behavior in aerodynamically coupled wings. His work emphasizes multi-physics validation and experimental techniques for high-speed vehicles.

He is active on LinkedIn and ResearchGate, and his ORCID identifier is 0009-0006-0832-1089. His research contributes to advancing understanding of thermal-structural interactions and fluid dynamics in extreme aerospace environments.