Implementazione di metodi numerici in ambito aerodinamico

Tutorial for the aerodyn software for teaching in ENERGI210

Fork of the original repository by Rafael Oliveira. Launch XFOIL from MATLAB

Scripts for pressure measurement processing

Drone Theoretical Simulation. Analytic Lab 1 of MECE3080 - Intelligent Physical System (abbr. IPS)

This paper is prepared as part of CA course and it contains a study on the classical thin airfoil theory for a cambered airfoil, NACA 1408.

Matlab script to analyze 2D airfoils (single, tandem and ground effect)

To model supersonic flow around a bullet, calculate Cd and drag forces using MATLAB, and validate these with Fluent CFD simulations, comparing analytical and numerical approaches for accuracy.

Source codes, datasets, and flight simulation scripts for the 'Applied Flight Performance' Udemy Course. Focusing on T-38 Talon aerodynamics and physics-based modeling in MATLAB

A parametric wing generator for 2- and 3-element wings.

repo for the A3 project

GNU OCTAVE script for calculating Mean Aerodynamic Chord of arbitrary shaped wing

Aircraft designer - Aerodynamics and Stability design. Based on: https://www.aircraftflightmechanics.com/AircraftPerformance/Introduction.html

Analysis And Computation Of Aerodynamics Parameters of a 4-digit NACA Airfoil With Flaps Using The Discrete Vortex Method (DVM)

1D Euler solver for academic purposes.

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

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

Comparison between the flow field around a cone (3D) and a wedge (2D). Analysis of the Taylor-Maccoll flow field within the supersonic boundary layer of a cone at zero angle of attack in a hypersonic flow.

Developed in Matlab, using Q3D and EMWET

Rotorcraft Design for Helicopter Emergency Medical Services (HEMS) Operations