(title "Pressure Coefficient") (labels "Position" "Pressure Coefficient") ((xy/key/label "airfoil-wall") 0 0.769302 0 0.769302 4.66151e-06 0.681949 4.67737e-06 0.843947 1.87174e-05 0.582525 1.87595e-05 0.90412 4.21977e-05 0.473512 4.22589e-05 0.949821 7.49586e-05 0.357779 7.50375e-05 0.980267 0.000116781 0.238376 0.000116876 0.996336 0.000167447 0.118088 0.000167566 0.999989 0.000226495 -0.000236628 0.00022665 0.990372 0.000293267 -0.114294 0.000293472 0.971896 0.000367312 -0.222671 0.00036757 0.945097 0.000448238 -0.324242 0.000448534 0.910743 0.000535469 -0.418097 0.000535794 0.871743 0.000628288 -0.503807 0.000628649 0.829072 0.000726354 -0.581719 0.000726775 0.78439 0.000829027 -0.652177 0.000829484 0.738511 0.000935894 -0.715634 0.000936362 0.692384 0.0010467 -0.772396 0.00104718 0.646555 0.00116108 -0.822824 0.00116156 0.601598 0.00127872 -0.867592 0.0012792 0.557804 0.00139934 -0.907397 0.00139985 0.515357 0.00152282 -0.942765 0.00152342 0.474336 0.0016487 -0.974008 0.00164933 0.435016 0.00177707 -1.00166 0.00177764 0.397296 0.00190834 -1.02646 0.0019088 0.361002 0.00204582 -1.04927 0.00204627 0.325337 0.00220124 -1.07108 0.00220174 0.287521 0.00237849 -1.09194 0.00237906 0.247439 0.00258208 -1.11196 0.00258274 0.205188 0.00283034 -1.1307 0.0028311 0.158568 0.00312353 -1.1468 0.00312441 0.1092 0.00346345 -1.16029 0.00346446 0.0583745 0.00385528 -1.17059 0.00385644 0.00717576 0.00433742 -1.17595 0.00433876 -0.0463734 0.00490184 -1.17568 0.00490338 -0.0994273 0.00490338 -0.0994273 0.00555335 -1.17418 0.00555461 -0.152121 0.0063 -1.16491 0.0063 -0.199334 0.00741067 -1.13325 0.00741067 -0.249734 0.00853185 -1.1005 0.00853185 -0.290701 0.00966065 -1.06769 0.00966065 -0.323111 0.010795 -1.03081 0.010795 -0.345489 0.0119335 -0.994597 0.0119335 -0.361587 0.013075 -0.958939 0.013075 -0.372323 0.0142185 -0.923787 0.0142185 -0.378792 0.0153636 -0.888808 0.0153636 -0.381511 0.0165097 -0.854059 0.0165097 -0.380855 0.0176563 -0.819674 0.0176563 -0.377697 0.0188032 -0.785789 0.0188032 -0.372913 0.0199502 -0.752491 0.0199502 -0.367137 0.0210969 -0.719814 0.0210969 -0.360631 0.0222433 -0.687767 0.0222433 -0.353382 0.0233893 -0.656365 0.0233893 -0.345405 0.0245347 -0.625603 0.0245347 -0.336753 0.0256794 -0.595458 0.0256794 -0.327509 0.0268235 -0.565922 0.0268235 -0.317789 0.0279668 -0.536991 0.0279668 -0.307702 0.0291094 -0.508626 0.0291094 -0.297314 0.0302512 -0.4808 0.0302512 -0.286702 0.0313922 -0.453498 0.0313922 -0.275933 0.0325324 -0.426662 0.0325324 -0.265023 0.0336718 -0.400253 0.0336718 -0.253996 0.0348104 -0.374242 0.0348104 -0.242878 0.0359482 -0.348587 0.0359482 -0.348587 0.0359482 -0.231683 0.0370852 -0.323248 0.0370852 -0.220417 0.0382213 -0.29818 0.0382213 -0.209074 0.0393567 -0.273338 0.0393567 -0.197633 0.0404913 -0.248685 0.0404913 -0.186086 0.0416251 -0.224185 0.0416251 -0.174418 0.042758 -0.199818 0.042758 -0.162603 0.0438902 -0.175561 0.0438902 -0.150605 0.0450216 -0.151393 0.0450216 -0.138376 0.0461522 -0.127345 0.0461522 -0.125892 0.047282 -0.113098 0.047282 -0.103435 0.0484109 -0.0999321 0.0484109 -0.0797404 0.049539 -0.0863203 0.049539 -0.0563234 0.0506663 -0.0721942 0.0506663 -0.0333415 0.0517926 -0.0574661 0.0517926 -0.0109002 0.0529181 -0.0420619 0.0529181 0.0107244 0.0540426 -0.0258375 0.0540426 0.0314678 0.0551662 -0.0087805 0.0551662 0.050907 0.0562887 0.00934583 0.0562887 0.069145 0.0574102 0.02837 0.0574102 0.0855938 0.0585306 0.0487979 0.0585306 0.100734 0.0596498 0.0696453 0.0596498 0.113749 0.0607678 0.0924527 0.0607678 0.125673 0.0618846 0.112946 0.0618846 0.135511 0.063 0.129693 0.063 0.129693 )