[Kit62]

Hello all,

For my Master's degree individual research project/thesis I have been using the SU2 aeroelastic solver to predict the flutter speed boundary for inviscid and viscous flows of a two-degree freedom airfoil, and also to simulate limit-cycle oscillations (LCOs) to investigate the effect of aerodynamic non-linearities (shocks and flow separation) on the behaviour of LCOs.

I would like to develop a better understanding of how exactly the aeroelastic solver in SU2 works. If anyone has knowledge in this area or knows of any reference material I can read that explains how the SU2 CFD code solves aeroelastic problems I would greatly appreciate it.

Thank you for any help.

Kit