SOLVED: 3. The question is often asked: Can an airfoil fly upside-down? To answer this, make the following calculation. Consider a positively cambered airfoil with a zero-lift angle of -2. The lift
Airfoil Geometry - an overview | ScienceDirect Topics
NACA airfoil - Wikipedia
Lift Coefficient | Glenn Research Center | NASA
MATLAB Aerofoil Lift Calculation - Computational Fluid Dynamics is the Future
NACA aerodynamic properties calculator using thin airfoil theory : r/desmos
Reynolds number calculator
aerodynamics - How can I calculate airfoil thickness? - Aviation Stack Exchange
wing area and lift of the airfoil
A simplified method for the calculation of airfoil pressure distribution - UNT Digital Library
JavaFoil - Users Manual
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.
Applied Sciences | Free Full-Text | Fast Airfoil Selection Methodology for Small Unmanned Aerial Vehicles
Section 7: Supersonic Flow Over Flat Plates, Wedges, and Airfoils
Airfoil Calculator | PDF | Airfoil | Wing
Subsonic Aerofoil and Wing Theory | Aerodynamics for Students
I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/desmos