VORTEX LATTICE

Version 1.1.1 (19,1 ko) par Miguel Crespo
Vortex Lattice Mehod for steady aerodynamics
4.9
(9)
3,2K téléchargements
Mise à jour 1 mai 2019

Afficher la licence

This code solves steady aerodynamics using the vortex lattice method. The geometry of the wing can be generated according to is Sweep, Taper ratio, dihedral, Aspect Ratio and chord. In the Main.m just change the parameters and you're up to go. Also, it can be specified the flight conditions like the angle of attack, or more than one, the flying Mach and altitude.
Finally, the panelization can be specified for more accuracy.
This is the first version I've created for college, and as I improve it, I'll try to keep the version updated.

*** What to expect in future updates

- General code improvements.
- Addition of control surfaces to the wing.
- Possibility of studying more surfaces, like a tail, winglets,...
- Being able to solve steady and unsteady cases.
- Creation of a full App program.
- Introduction to aeroelasticity.
- Possibility of running a Doublet Lattice Method to simplify unsteady problems.

Citation pour cette source

Miguel Crespo (2025). VORTEX LATTICE (https://fr.mathworks.com/matlabcentral/fileexchange/67608-vortex-lattice), MATLAB Central File Exchange. Extrait(e) le .

Compatibilité avec les versions de MATLAB
Créé avec R2019a
Compatible avec toutes les versions
Plateformes compatibles
Windows macOS Linux
Tags Ajouter des tags

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!

Version Publié le Notes de version
1.1.1

.
1.1.0

Addition of control surfaces to the wing. Control surface deflection can be interpreted as symmetrical, flap example, or antisymmetrical, aileron example.
1.0.0.0

- Code fix and improvements.