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

((xy/key/label "airfoil-wall")
0.00490338	-1.17574
0.00555461	-1.17422
0.0063	-1.16502
0.00741067	-1.13333
0.00853185	-1.10055
0.00966065	-1.06774
0.010795	-1.03087
0.0119335	-0.994649
0.013075	-0.95899
0.0142185	-0.923836
0.0153636	-0.888856
0.0165097	-0.854105
0.0176563	-0.819718
0.0188032	-0.785832
0.0199502	-0.752533
0.0210969	-0.719856
0.0222433	-0.687807
0.0233893	-0.656404
0.0245347	-0.625643
0.0256794	-0.595497
0.0268235	-0.56596
0.0279668	-0.537028
0.0291094	-0.508663
0.0302512	-0.480837
0.0313922	-0.453535
0.0325324	-0.426698
0.0336718	-0.400289
0.0348104	-0.374279
0.0359482	-0.348623
0.0370852	-0.323284
0.0382213	-0.298217
0.0393567	-0.273374
0.0404913	-0.248722
0.0416251	-0.224221
0.042758	-0.199854
0.0438902	-0.175596
0.0450216	-0.151428
0.0461522	-0.127378
0.047282	-0.103467
0.0484109	-0.0797695
0.049539	-0.0563495
0.0506663	-0.0333639
0.0517926	-0.0109181
0.0529181	0.0107118
0.0540426	0.0314613
0.0551662	0.0509069
0.0562887	0.0691519
0.0574102	0.0856073
0.0585306	0.100754
0.0596498	0.113775
0.0607678	0.125704
0.0618846	0.135546
0.063	0.129728
0	0.769359
4.66151e-06	0.843849
1.87174e-05	0.904084
4.21977e-05	0.949798
7.49586e-05	0.980303
0.000116781	0.996505
0.000167447	1.00006
0.000226495	0.990487
0.000293267	0.971986
0.000367312	0.945167
0.000448238	0.910877
0.000535469	0.871875
0.000628288	0.829241
0.000726354	0.784576
0.000829027	0.738714
0.000935894	0.692581
0.0010467	0.646748
0.00116108	0.601784
0.00127872	0.557982
0.00139934	0.515533
0.00152282	0.474532
0.0016487	0.435211
0.00177707	0.397468
0.00190834	0.361139
0.00204582	0.325435
0.00220124	0.287557
0.00237849	0.247647
0.00258208	0.205475
0.00283034	0.158687
0.00312353	0.109358
0.00346345	0.0585514
0.00385528	0.00734734
0.00433742	-0.0462066
0.00490184	-0.0992728
0.00555335	-0.151995
0.0063	-0.199277
0.00741067	-0.249696
0.00853185	-0.290675
0.00966065	-0.323078
0.010795	-0.345456
0.0119335	-0.361555
0.013075	-0.372292
0.0142185	-0.378761
0.0153636	-0.38148
0.0165097	-0.380825
0.0176563	-0.377668
0.0188032	-0.372885
0.0199502	-0.367109
0.0210969	-0.360603
0.0222433	-0.353354
0.0233893	-0.345378
0.0245347	-0.336726
0.0256794	-0.327483
0.0268235	-0.317763
0.0279668	-0.307676
0.0291094	-0.297289
0.0302512	-0.286677
0.0313922	-0.275908
0.0325324	-0.264998
0.0336718	-0.253971
0.0348104	-0.242853
0.0359482	-0.231658
0.00490338	-1.17574
0.00433876	-1.17601
0.00385644	-1.17072
0.00346446	-1.16047
0.00312441	-1.14695
0.0028311	-1.13084
0.00258274	-1.11211
0.00237906	-1.0921
0.00220174	-1.07125
0.00204627	-1.04944
0.0019088	-1.02666
0.00177764	-1.00189
0.00164933	-0.974262
0.00152342	-0.943038
0.00139985	-0.907676
0.0012792	-0.867892
0.00116156	-0.823149
0.00104718	-0.772751
0.000936362	-0.716021
0.000829484	-0.652593
0.000726775	-0.582148
0.000628649	-0.504231
0.000535794	-0.418527
0.000448534	-0.324673
0.00036757	-0.223081
0.000293472	-0.114651
0.00022665	-0.000522503
0.000167566	0.117868
0.000116876	0.238213
7.50375e-05	0.35767
4.22589e-05	0.47341
1.87595e-05	0.582329
4.67737e-06	0.681801
0	0.769359
0.0359482	-0.231658
0.0370852	-0.220393
0.0382213	-0.20905
0.0393567	-0.197608
0.0404913	-0.186062
0.0416251	-0.174393
0.042758	-0.162578
0.0438902	-0.15058
0.0450216	-0.138351
0.0461522	-0.125866
0.047282	-0.113072
0.0484109	-0.0999053
0.049539	-0.086293
0.0506663	-0.0721662
0.0517926	-0.0574375
0.0529181	-0.0420325
0.0540426	-0.0258071
0.0551662	-0.00874913
0.0562887	0.00937842
0.0574102	0.0284038
0.0585306	0.0488333
0.0596498	0.0696818
0.0607678	0.0924908
0.0618846	0.112985
0.063	0.129728
)