aeroelasticity

Main repository for the NLR-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.

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

Multidisciplinary-design Adaptation and Sensitivity Toolkit (MAST) - Sensitivity-enabled multiphysics FEA for design

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.

Harmonic balance solvers

High-aspect-ratio composite wing nonlinear aeroelastic toolbox

Some usefull routines for aeroelastic analysis with NASTRAN.

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.

Multifidelity aeroelastic optimization with application to a BWB

A Julia package for the simulation of aeroelastic problems in beam structures

Mapping, Radial Basis Function, RBF, FSI

A Open-Source Horizontal axis-Aero-Wave-Turbulence Coupling(HawtC) Tool for dynamic simulation of floating offshore wind turbine(FOWT).And supports the dynamic coupling simulation of the tuned mass damper and tuned mass inertia damper for wind turbine blades and towers

Structural Wing Model Reduction in Fluid-Structure Interactions

Repository for the Q4 2021 assignments of the course Wind Turbine Aeroelasticity (AE4W21-14) at TU Delft.

POD+K in Real-Time Aeroelastic Pre-design Problem

GPU-Accelerated Finite Element Structural Analysis and Optimization

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.

MATLAB benchmark for coupled nonlinear aeroelastic simulation and control of a Pazy-wing aircraft, with scheduled ROMs, LQR, nMHE, nMPC, actuator dynamics, and native acceleration.