PSU-90-125WL

Designed for Peter Masak for use on an ASW20 winglet.
Designed by Michael S. Selig with design requirements from Mark D. Maughmer.
Design requirements.
cl min .15
cl max 1.0
t/c 12.5%
Rn range 350,000 --> 1,000,000.
cl_min_stall -.5
cl_max_stall 1.5
No bubbles at 0.5 design Reynolds.
No cm restriction.
Previous most used airfoil for winglets: FX60-126