CFD Solver for Stationary Flow Analysis around NACA Airfoils
Version 1.0.0 (3.88 KB) by
abdelhamid bouhelal
2D Incompressible and Compressible Flow Solver for NACA Airfoils Using Central Difference Finite Discretization and Newton Raphson Algorithm
This CFD code solves numerically the subsonic stationary, 2D, incompressible and compressible flows around NACA airfoils. The code is based on solving the combined Euler equations using the approach of small perturbation theory, using central difference finite discretization and the Newton Raphson algorithm.
Cite As
abdelhamid bouhelal (2024). CFD Solver for Stationary Flow Analysis around NACA Airfoils (https://www.mathworks.com/matlabcentral/fileexchange/125860-cfd-solver-for-stationary-flow-analysis-around-naca-airfoils), MATLAB Central File Exchange. Retrieved .
MATLAB Release Compatibility
Created with
R2022b
Compatible with any release
Platform Compatibility
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Version | Published | Release Notes | |
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1.0.0 |