Look at the image I posted in the previous image - the Ta 152H used a NACA 230xx airfoil at the root. The NACA 5-digit airfoils have very little laminar flow.
Hi,
Thanks for that original data page. The Ta 152 H-1 profile seems to indicate both "NACA 230" and Fw in the box, which is different to all the other types shown. Given the very different detail of the 152 H high aspect ratio wing, is it not likely that this shows a root area NACA 230 profile, developing into an unspecified Fw profile in the very different outer sections?
Cheers
Eng