Main repository for the NREL-supported OpenFAST whole-turbine and FAST.Farm wind farm simulation codes.

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

An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.

Some usefull routines for aeroelastic analysis with NASTRAN.

High-aspect-ratio composite wing nonlinear aeroelastic toolbox

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.

Mapping, Radial Basis Function, RBF, FSI

Multifidelity aeroelastic optimization with application to a BWB

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

QHAST2 is the upgraded version of OpenHastV6, significantly enhancing the simulation speed of floating offshore wind turbines! It introduces new features, supporting linear and co-rotational nonlinear finite element calculation methods for framework structures. QHAST2 implements efficient and high-precision simulation calculation methods for flexib

Nastran helper code to design and analyse the aeroelastic response of a wing, plot the pannels for the doubblet lattice method and the FEM mesh.

Hinged wingtip modelling in NeoCASS based on Airbus AlbatrossONE