Howard probably knows
Try 00 series, 16.5% thickness and move the high point from 30% to 25%
I did that with compufoil, and it looks extremely close when I put it on top of the plan airfoil from the pdf
A bit different between the LE and the high point, but probably within sanding error.
(I don't have the dxf generator option of Compufoil, so this was from a dat file and lacked LE points)