![I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/desmos I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/desmos](https://preview.redd.it/4cerrcysnjw61.png?auto=webp&s=12acc6ffff0a900424fa0b57177c84214b7259fb)
I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/desmos
![Parametric angle of attack (aoa) study for airfoil lift and drag calculation - Fluid Flow / CFD - SimScale CAE Forum Parametric angle of attack (aoa) study for airfoil lift and drag calculation - Fluid Flow / CFD - SimScale CAE Forum](https://www.simscale.com/forum/uploads/default/original/3X/6/4/643bc546a4bc5add99229c306fc0096297fa0e99.png)
Parametric angle of attack (aoa) study for airfoil lift and drag calculation - Fluid Flow / CFD - SimScale CAE Forum
![GitHub - janhenrikbern/diamond_airfoil: Calculates and plots pressure distribution across a diamond-shaped airfoil at specified free stream pressure and speed, wedge angle, and angle of attack. GitHub - janhenrikbern/diamond_airfoil: Calculates and plots pressure distribution across a diamond-shaped airfoil at specified free stream pressure and speed, wedge angle, and angle of attack.](https://raw.githubusercontent.com/janhenrikbern/diamond_airfoil/master/example.png)
GitHub - janhenrikbern/diamond_airfoil: Calculates and plots pressure distribution across a diamond-shaped airfoil at specified free stream pressure and speed, wedge angle, and angle of attack.
![aircraft design - How do you calculate the lift coefficient of an airfoil at zero angle of attack? - Aviation Stack Exchange aircraft design - How do you calculate the lift coefficient of an airfoil at zero angle of attack? - Aviation Stack Exchange](https://i.stack.imgur.com/SqspU.jpg)