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

((xy/key/label "airfoil-wall")
0.000829484	0.982681
0.000936362	0.967542
0.00104718	0.94792
0.00116156	0.925648
0.0012792	0.900998
0.00139985	0.874985
0.00152342	0.847843
0.00164933	0.820219
0.00177764	0.792264
0.0019088	0.764148
0.00204627	0.735415
0.00220174	0.7037
0.00237906	0.668846
0.00258274	0.630671
0.0028311	0.586683
0.00312441	0.5381
0.00346446	0.486189
0.00385644	0.431755
0.00433876	0.37195
0.00490338	0.309837
0.00555461	0.246549
0.0063	0.186481
0.00741067	0.114063
0.00853185	0.052489
0.00966065	0.0015676
0.010795	-0.0387905
0.0119335	-0.0718728
0.013075	-0.0987845
0.0142185	-0.120699
0.0153636	-0.138405
0.0165097	-0.152531
0.0176563	-0.16356
0.0188032	-0.171858
0.0199502	-0.177744
0.0210969	-0.181559
0.0222433	-0.183736
0.0233893	-0.184822
0.0245347	-0.185098
0.0256794	-0.184616
0.0268235	-0.183486
0.0279668	-0.181725
0.0291094	-0.179352
0.0302512	-0.176458
0.0313922	-0.173122
0.0325324	-0.16939
0.0336718	-0.165313
0.0348104	-0.160952
0.000829484	0.982681
0.000726775	0.99304
0.000628649	0.998413
0.000535794	0.995048
0.000448534	0.983272
0.00036757	0.96029
0.000293472	0.92426
0.00022665	0.874509
0.000167566	0.809002
0.000116876	0.727691
7.50375e-05	0.629845
4.22589e-05	0.516115
1.87595e-05	0.387664
4.67737e-06	0.24588
0	0.0922681
4.66151e-06	-0.0710517
1.87174e-05	-0.241963
4.21977e-05	-0.416546
7.49586e-05	-0.590221
0.000116781	-0.758905
0.000167447	-0.919231
0.000226495	-1.06836
0.000293267	-1.20451
0.000367312	-1.32725
0.000448238	-1.43628
0.000535469	-1.53134
0.000628288	-1.61294
0.000726354	-1.68252
0.000829027	-1.74152
0.000935894	-1.79112
0.0010467	-1.83209
0.00116108	-1.86524
0.00127872	-1.89173
0.00139934	-1.91264
0.00152282	-1.92874
0.0016487	-1.94062
0.00177707	-1.94894
0.00190834	-1.95446
0.00204582	-1.9579
0.00220124	-1.95867
0.00237849	-1.95637
0.00258208	-1.95118
0.00283034	-1.94103
0.00312353	-1.92513
0.00346345	-1.905
0.00385528	-1.88017
0.00433742	-1.84614
0.00490184	-1.80293
0.00555335	-1.75636
0.0063	-1.69955
0.00741067	-1.60101
0.00853185	-1.51596
0.00966065	-1.44472
0.010795	-1.37532
0.0119335	-1.30949
0.013075	-1.24616
0.0142185	-1.18564
0.0153636	-1.12763
0.0165097	-1.07196
0.0176563	-1.01847
0.0188032	-0.96701
0.0199502	-0.917434
0.0210969	-0.869601
0.0222433	-0.82339
0.0233893	-0.778709
0.0245347	-0.735449
0.0256794	-0.69351
0.0268235	-0.652814
0.0279668	-0.613296
0.0291094	-0.57488
0.0302512	-0.537501
0.0313922	-0.501111
0.0325324	-0.465651
0.0336718	-0.43108
0.0348104	-0.397383
0.0359482	-0.364548
0.0370852	-0.332583
0.0382213	-0.301515
0.0393567	-0.271379
0.0404913	-0.242238
0.0416251	-0.214174
0.042758	-0.187285
0.0438902	-0.161665
0.0450216	-0.13743
0.0461522	-0.11465
0.047282	-0.0934405
0.0484109	-0.0738029
0.049539	-0.0558253
0.0348104	-0.160952
0.0359482	-0.156345
0.0370852	-0.151528
0.0382213	-0.146519
0.0393567	-0.141322
0.0404913	-0.135947
0.0416251	-0.130402
0.042758	-0.124686
0.0438902	-0.118778
0.0450216	-0.112658
0.0461522	-0.106321
0.047282	-0.0997384
0.0484109	-0.092868
0.049539	-0.0856579
0.0506663	-0.0780576
0.0517926	-0.0700354
0.0529181	-0.0615048
0.0540426	-0.0523834
0.0551662	-0.0425847
0.0562887	-0.0320364
0.0574102	-0.0205357
0.0585306	-0.0080893
0.0596498	0.00568562
0.0607678	0.0204673
0.0618846	0.0372556
0.063	0.0543369
0.063	0.0543369
0.0618846	0.057569
0.0607678	0.050799
0.0596498	0.0445633
0.0585306	0.0374883
0.0574102	0.0298254
0.0562887	0.0211188
0.0551662	0.0115638
0.0540426	0.00075853
0.0529181	-0.0111845
0.0517926	-0.0245963
0.0506663	-0.0394017
0.049539	-0.0558253
)