There are 5 repositories under aeroelasticity topic.
Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique in many ways, while the most prominent feature is that it is entirely based in .NET. Recompiling the project is very easy and you can have tons of fun extending the source code.
Multidisciplinary-design Adaptation and Sensitivity Toolkit (MAST) - Sensitivity-enabled multiphysics FEA for design
Harmonic balance solvers
Some usefull routines for aeroelastic analysis with NASTRAN.
High-aspect-ratio composite wing nonlinear aeroelastic toolbox
Multifidelity aeroelastic optimization with application to a BWB
The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and frequency domain as well as dynamic landing loads based on a generic landing gear module.
A simple framework that automatically generates SU2 configuration (.cfg) files and make calls to SU2 to perform aeroelastic simulations all within Python. The Matrix Pencil method is then used to compute the damping coefficient.
Structural Wing Model Reduction in Fluid-Structure Interactions
POD+K in Real-Time Aeroelastic Pre-design Problem
Repository for the Q4 2021 assignments of the course Wind Turbine Aeroelasticity (AE4W21-14) at TU Delft.
Relevant case/data for TrimOpt paper
Hinged wingtip modelling in NeoCASS based on Airbus AlbatrossONE