Solved: NACA AEROFOIL 2415 lift coefficient calculation is not accurate !!!!!!! - Autodesk Community - CFD
![I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/AerospaceEngineering I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/AerospaceEngineering](https://preview.redd.it/4cerrcysnjw61.png?width=640&crop=smart&auto=webp&s=065d7cdb4d6c9c7b723d2e46086b95be3aa0915a)
I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/AerospaceEngineering
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Practical Calculation of Second-Order Supersonic Flow Past Nonlifting Bodies of Revolution - UNT Digital Library
![Lift-drag characteristics for a NACA 2412 rectangular wing with AR=5 at... | Download Scientific Diagram Lift-drag characteristics for a NACA 2412 rectangular wing with AR=5 at... | Download Scientific Diagram](https://www.researchgate.net/publication/330087372/figure/fig1/AS:710680059588610@1546450738406/Lift-drag-characteristics-for-a-NACA-2412-rectangular-wing-with-AR5-at-Re27x106.png)