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

((xy/key/label "airfoil-wall")
0.000829484	0.900379
0.000936362	0.867804
0.00104718	0.833663
0.00116156	0.798491
0.0012792	0.762951
0.00139985	0.727373
0.00152342	0.692053
0.00164933	0.657377
0.00177764	0.623405
0.0019088	0.590116
0.00204627	0.556876
0.00220174	0.521019
0.00237906	0.482449
0.00258274	0.441039
0.0028311	0.394343
0.00312441	0.343897
0.00346446	0.291052
0.00385644	0.236809
0.00433876	0.178563
0.00490338	0.11944
0.00555461	0.0600085
0.0063	0.00500978
0.00741067	-0.0581024
0.00853185	-0.110749
0.00966065	-0.153482
0.010795	-0.185712
0.0119335	-0.211035
0.013075	-0.230554
0.0142185	-0.245424
0.0153636	-0.256338
0.0165097	-0.2638
0.0176563	-0.268262
0.0188032	-0.270187
0.0199502	-0.270045
0.0210969	-0.268504
0.0222433	-0.266103
0.0233893	-0.262976
0.0245347	-0.259134
0.0256794	-0.254567
0.0268235	-0.249345
0.0279668	-0.243566
0.0291094	-0.237307
0.0302512	-0.230649
0.0313922	-0.223678
0.0325324	-0.216427
0.0336718	-0.208941
0.0348104	-0.201269
0.000829484	0.900379
0.000726775	0.930128
0.000628649	0.956483
0.000535794	0.9772
0.000448534	0.99168
0.00036757	0.9993
0.000293472	0.996118
0.00022665	0.982242
0.000167566	0.955091
0.000116876	0.913191
7.50375e-05	0.856717
4.22589e-05	0.784356
1.87595e-05	0.69693
4.67737e-06	0.595181
0	0.480273
4.66151e-06	0.353736
1.87174e-05	0.217201
4.21977e-05	0.0737444
7.49586e-05	-0.0728311
0.000116781	-0.218943
0.000167447	-0.361504
0.000226495	-0.497542
0.000293267	-0.625059
0.000367312	-0.742899
0.000448238	-0.850389
0.000535469	-0.947228
0.000628288	-1.03309
0.000726354	-1.10883
0.000829027	-1.17545
0.000935894	-1.23374
0.0010467	-1.28425
0.00116108	-1.32756
0.00127872	-1.3646
0.00139934	-1.39625
0.00152282	-1.42318
0.0016487	-1.44583
0.00177707	-1.46481
0.00190834	-1.48095
0.00204582	-1.49496
0.00220124	-1.50706
0.00237849	-1.51719
0.00258208	-1.5255
0.00283034	-1.53077
0.00312353	-1.5318
0.00346345	-1.52925
0.00385528	-1.52279
0.00433742	-1.50918
0.00490184	-1.48894
0.00555335	-1.46741
0.0063	-1.43725
0.00741067	-1.37337
0.00853185	-1.31237
0.00966065	-1.25954
0.010795	-1.20732
0.0119335	-1.15745
0.013075	-1.10861
0.0142185	-1.06104
0.0153636	-1.01466
0.0165097	-0.969565
0.0176563	-0.925767
0.0188032	-0.883246
0.0199502	-0.841957
0.0210969	-0.801847
0.0222433	-0.762861
0.0233893	-0.72496
0.0245347	-0.688082
0.0256794	-0.652161
0.0268235	-0.617157
0.0279668	-0.583033
0.0291094	-0.54973
0.0302512	-0.517195
0.0313922	-0.485393
0.0325324	-0.454253
0.0336718	-0.423725
0.0348104	-0.393773
0.0359482	-0.364351
0.0370852	-0.335427
0.0382213	-0.306967
0.0393567	-0.278948
0.0404913	-0.251353
0.0416251	-0.224195
0.042758	-0.197495
0.0438902	-0.171287
0.0450216	-0.14564
0.0461522	-0.120643
0.047282	-0.0964095
0.0484109	-0.0730579
0.049539	-0.0507403
0.0348104	-0.201269
0.0359482	-0.19343
0.0370852	-0.185449
0.0382213	-0.177326
0.0393567	-0.169059
0.0404913	-0.160649
0.0416251	-0.152084
0.042758	-0.143359
0.0438902	-0.134439
0.0450216	-0.125289
0.0461522	-0.115903
0.047282	-0.106232
0.0484109	-0.0962177
0.049539	-0.0858032
0.0506663	-0.0749177
0.0517926	-0.0635027
0.0529181	-0.051467
0.0540426	-0.0386982
0.0551662	-0.0251111
0.0562887	-0.010567
0.0574102	0.00504122
0.0585306	0.0219127
0.0596498	0.0400225
0.0607678	0.059754
0.0618846	0.0798417
0.063	0.0987357
0.063	0.0987357
0.0618846	0.103956
0.0607678	0.0961283
0.0596498	0.0876394
0.0585306	0.077957
0.0574102	0.0670505
0.0562887	0.0547046
0.0551662	0.0409133
0.0540426	0.0255483
0.0529181	0.00866018
0.0517926	-0.00975614
0.0506663	-0.0295872
0.049539	-0.0507403
)