PSU-90-125WL
# Designed for Peter Masak for use on an ASW20 winglet.
# Designed by M.S. Selig with design requirements from M.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 .5 design Reynolds.
# No cm restriction.
# Previous most airfoil used for winglets: FX60-126
#
 1.00000  0.00000 
 0.99646  0.00062 
 0.98627  0.00269 
 0.97034  0.00630 
 0.94931  0.01099 
 0.92336  0.01635 
 0.89265  0.02238 
 0.85770  0.02912 
 0.81908  0.03646 
 0.77741  0.04423 
 0.73333  0.05217 
 0.68748  0.05999 
 0.64048  0.06725 
 0.59265  0.07341 
 0.54409  0.07826 
 0.49509  0.08194 
 0.44618  0.08446 
 0.39787  0.08580 
 0.35064  0.08593 
 0.30495  0.08482 
 0.26123  0.08249 
 0.21989  0.07893 
 0.18131  0.07420 
 0.14582  0.06835 
 0.11371  0.06149 
 0.08524  0.05373 
 0.06062  0.04523 
 0.04002  0.03617 
 0.02356  0.02681 
 0.01134  0.01745 
 0.00343  0.00850 
 0.00002  0.00063 
 0.00240 -0.00590 
 0.01088 -0.01194 
 0.02456 -0.01782 
 0.04321 -0.02324 
 0.06663 -0.02804 
 0.09462 -0.03211 
 0.12693 -0.03539 
 0.16327 -0.03786 
 0.20328 -0.03951 
 0.24657 -0.04033 
 0.29269 -0.04037 
 0.34116 -0.03965 
 0.39144 -0.03822 
 0.44300 -0.03610 
 0.49525 -0.03331 
 0.54770 -0.02975 
 0.60004 -0.02548 
 0.65193 -0.02083 
 0.70276 -0.01622 
 0.75178 -0.01192 
 0.79827 -0.00814 
 0.84149 -0.00502 
 0.88073 -0.00261 
 0.91534 -0.00093 
 0.94469  0.00007 
 0.96829  0.00051 
 0.98567  0.00049 
 0.99638  0.00018 
 1.00000  0.00000 
