GitHub repository: mankarali/NACA_AIRFOIL
Primary language: Jupyter Notebook
Created: 2021-01-14T15:35:22Z
Description: The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA). The shape of the NACA airfoils is described using a series of digits following the word "NACA". The parameters in the numerical code can be entered into equations to precisely generate the cross-section of the airfoil and calculate its properties.