Airfoil design for X-Plane using XFLR5 and polar2afl | Recorded Stream
Channel: totoritko
Date: 01/11/2019

ERRATA: since making this video I dug a little into the innards of X-Plane. Airfoil files in X-Plane store Reynolds number for a UNIT CHORD WING, not the actual chord length of the wing. X-Plane pre-multiplies the Reynolds table with the actual chord length of the wing section it is examining. So whenever you do your XFLR5 simulations and generate airfoils, assume a unit length chord (i.e. leave chord length as "1" in your Reynolds number calculator) and only vary the other parameters.

X-Plane: https://www.x-plane.com/
XFLR5: https://www.xflr5.tech/xflr5.htm
polar2afl: https://github.com/skiselkov/polar2afl/releases