Matlab implementation to simulate the non-linear dynamics of a fixed-wing unmanned areal glider. Includes tools to calculate aerodynamic coefficients using a vortex lattice method implementation, and to extract longitudinal and lateral linear systems around the trimmed gliding state.

Library for Aircraft Dynamics And Control

Full dynamic model for the Babyshark 260 VTOL UAV.

Developed a missile guidance and ballistic control system for autonomous mid-air and surface-to-air target chase and interception

Computational Aerodynamics Lab

Fluid-Structure Interaction Analysis Using FEM and UVLM

Get airfoil characteristics from an experimental database.

This repository contains the source code for a modified Beddoes-Leishman dynamic stall model

PteraControls is a tool for designing control systems for flapping wing vehicles.

System identification for Monash UAS aircraft

A MATLAB code incorporating the analysis method described by Barrowman (1967) to analyse the aerodynamic properties of a supersonic sounding rocket.

Genetic algorithm optimisation of a small-scale wind turbine blade

getWAKE is a collection of Matlab subroutines and GUI for post-processing of bluff-bodies wake data measured using Particle Image Velocimetry (PIV), and analyzed by OpenPIV (or other) software. getWAKE accepts PIV wake data as .mat files extracted by the OpenPIV-spatial-analysis-toolbox. getWAKE allows the user to re-construct a full unsteady wa…

The study aims to develop a preliminary design of a fixed-wing aerodyne (Business Jet) able to carry a reduced number of people in intercontinental flights at the maximum possible Mach number.

Source and vortex panel method codes

This is a matlab program for wind tunnel post processing.

This project calculates the pressure coefficient for a given number of airfoils [NACA0006, NACA0012, NACA0018] using a source vortex panel method.

Numerical and Analytical Flow Solution over Joukowski Aerofoil, Using O-grid Meshing Method and PSOR solving algorithm.

Developed in Matlab, using Q3D and EMWET