owaisali10's repositories
Gauss_Seidel_General
Python code for Gauss-Seidel Iterative Solution
Language:Python000
MATLAB-code-for-a-4-digit-NACA-airfoil
Performance characteristics of a 4-digit NACA airfoil. Kuethe and Chow Vortex Panel Method, Thin airfoil method and the Finite Wing Method is used. The resulting values are also compared.
Language:MATLAB000
Language:MATLAB000