(title "Pressure Coefficient")
(labels "Position" "Pressure Coefficient")

((xy/key/label "airfoil-wall")
0.000829484	0.955147
0.000936362	0.975796
0.00104718	0.988705
0.00116156	0.99528
0.0012792	0.996382
0.00139985	0.992931
0.00152342	0.986227
0.00164933	0.976638
0.00177764	0.964573
0.0019088	0.950551
0.00204627	0.93455
0.00220174	0.9152
0.00237906	0.892219
0.00258274	0.865268
0.0028311	0.832107
0.00312441	0.793208
0.00346446	0.749402
0.00385644	0.701146
0.00433876	0.645585
0.00490338	0.585027
0.00555461	0.521235
0.0063	0.458022
0.00741067	0.376385
0.00853185	0.304774
0.00966065	0.243685
0.010795	0.192343
0.0119335	0.148292
0.013075	0.11056
0.0142185	0.078096
0.0153636	0.0501401
0.0165097	0.026055
0.0176563	0.00529928
0.0188032	-0.0125791
0.0199502	-0.0279459
0.0210969	-0.0410925
0.0222433	-0.0522585
0.0233893	-0.0616578
0.0245347	-0.0694891
0.0256794	-0.0760026
0.0268235	-0.0815336
0.0279668	-0.0863506
0.0291094	-0.0905649
0.0302512	-0.0942272
0.0313922	-0.0973718
0.0325324	-0.100012
0.0336718	-0.102191
0.0348104	-0.103971
0.000829484	0.955147
0.000726775	0.925362
0.000628649	0.884813
0.000535794	0.831938
0.000448534	0.764947
0.00036757	0.682385
0.000293472	0.583039
0.00022665	0.465784
0.000167566	0.329612
0.000116876	0.175259
7.50375e-05	0.00454853
4.22589e-05	-0.181079
1.87595e-05	-0.379335
4.67737e-06	-0.587718
0	-0.804014
4.66151e-06	-1.02545
1.87174e-05	-1.24892
4.21977e-05	-1.46918
7.49586e-05	-1.68023
0.000116781	-1.87751
0.000167447	-2.05714
0.000226495	-2.2169
0.000293267	-2.35645
0.000367312	-2.47541
0.000448238	-2.57453
0.000535469	-2.6549
0.000628288	-2.71809
0.000726354	-2.76644
0.000829027	-2.80236
0.000935894	-2.82759
0.0010467	-2.84342
0.00116108	-2.85122
0.00127872	-2.8521
0.00139934	-2.8475
0.00152282	-2.83873
0.0016487	-2.82639
0.00177707	-2.81111
0.00190834	-2.7938
0.00204582	-2.77458
0.00220124	-2.751
0.00237849	-2.72295
0.00258208	-2.69041
0.00283034	-2.64935
0.00312353	-2.5995
0.00346345	-2.54289
0.00385528	-2.47796
0.00433742	-2.39369
0.00490184	-2.29222
0.00555335	-2.18935
0.0063	-2.08707
0.00741067	-1.93662
0.00853185	-1.80637
0.00966065	-1.69453
0.010795	-1.58849
0.0119335	-1.49047
0.013075	-1.39828
0.0142185	-1.31168
0.0153636	-1.22975
0.0165097	-1.15201
0.0176563	-1.07802
0.0188032	-1.00745
0.0199502	-0.940014
0.0210969	-0.875518
0.0222433	-0.813821
0.0233893	-0.754862
0.0245347	-0.698632
0.0256794	-0.645169
0.0268235	-0.594591
0.0279668	-0.547013
0.0291094	-0.502582
0.0302512	-0.461418
0.0313922	-0.423598
0.0325324	-0.389161
0.0336718	-0.358038
0.0348104	-0.330105
0.0359482	-0.305162
0.0370852	-0.282957
0.0382213	-0.263211
0.0393567	-0.245633
0.0404913	-0.229951
0.0416251	-0.215902
0.042758	-0.203265
0.0438902	-0.191835
0.0450216	-0.18145
0.0461522	-0.171952
0.047282	-0.163233
0.0484109	-0.155178
0.049539	-0.147731
0.0348104	-0.103971
0.0359482	-0.105406
0.0370852	-0.106546
0.0382213	-0.107426
0.0393567	-0.108073
0.0404913	-0.108517
0.0416251	-0.108789
0.042758	-0.108914
0.0438902	-0.108888
0.0450216	-0.108718
0.0461522	-0.108432
0.047282	-0.108023
0.0484109	-0.107482
0.049539	-0.106791
0.0506663	-0.105942
0.0517926	-0.104944
0.0529181	-0.103772
0.0540426	-0.102408
0.0551662	-0.100854
0.0562887	-0.0991335
0.0574102	-0.0971933
0.0585306	-0.0952327
0.0596498	-0.093228
0.0607678	-0.0919724
0.0618846	-0.0890903
0.063	-0.0825402
0.063	-0.0825402
0.0618846	-0.0839619
0.0607678	-0.0930643
0.0596498	-0.0998836
0.0585306	-0.10469
0.0574102	-0.108695
0.0562887	-0.112923
0.0551662	-0.11755
0.0540426	-0.122732
0.0529181	-0.128321
0.0517926	-0.134357
0.0506663	-0.140799
0.049539	-0.147731
)