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

((xy/key/label "airfoil-wall")
0.00490338	0.466742
0.00555461	0.402218
0.0063	0.339608
0.00741067	0.261179
0.00853185	0.193397
0.00966065	0.136425
0.010795	0.0897221
0.0119335	0.0504041
0.013075	0.0174199
0.0142185	-0.0103591
0.0153636	-0.0337255
0.0165097	-0.0533303
0.0176563	-0.0697108
0.0188032	-0.0833013
0.0199502	-0.0944372
0.0210969	-0.103378
0.0222433	-0.11036
0.0233893	-0.115679
0.0245347	-0.119714
0.0256794	-0.122819
0.0268235	-0.125209
0.0279668	-0.126981
0.0291094	-0.128148
0.0302512	-0.128744
0.0313922	-0.12881
0.0325324	-0.128382
0.0336718	-0.127546
0.0348104	-0.126358
0.0359482	-0.124853
0.0370852	-0.123084
0.0382213	-0.121078
0.0393567	-0.118853
0.0404913	-0.116431
0.0416251	-0.11383
0.042758	-0.111061
0.0438902	-0.108112
0.0450216	-0.104978
0.0461522	-0.101667
0.047282	-0.098165
0.0484109	-0.0944414
0.049539	-0.0904661
0.0506663	-0.0862071
0.0517926	-0.0816477
0.0529181	-0.0767325
0.0540426	-0.0714133
0.0551662	-0.0656363
0.0562887	-0.0593747
0.0574102	-0.0524826
0.0585306	-0.0450543
0.0596498	-0.036775
0.0607678	-0.0282227
0.0618846	-0.0175551
0.063	-0.00510343
0	-0.35926
4.66151e-06	-0.555215
1.87174e-05	-0.756018
4.21977e-05	-0.956959
7.49586e-05	-1.15277
0.000116781	-1.33891
0.000167447	-1.51192
0.000226495	-1.66902
0.000293267	-1.80917
0.000367312	-1.93228
0.000448238	-2.03814
0.000535469	-2.12736
0.000628288	-2.20102
0.000726354	-2.26102
0.000829027	-2.30931
0.000935894	-2.34741
0.0010467	-2.37631
0.00116108	-2.39707
0.00127872	-2.41095
0.00139934	-2.41938
0.00152282	-2.42321
0.0016487	-2.42285
0.00177707	-2.41918
0.00190834	-2.41319
0.00204582	-2.40507
0.00220124	-2.39328
0.00237849	-2.37779
0.00258208	-2.35854
0.00283034	-2.33239
0.00312353	-2.29917
0.00346345	-2.26058
0.00385528	-2.21635
0.00433742	-2.15913
0.00490184	-2.08786
0.00555335	-2.01083
0.0063	-1.92748
0.00741067	-1.80144
0.00853185	-1.6941
0.00966065	-1.60255
0.010795	-1.51446
0.0119335	-1.43227
0.013075	-1.35442
0.0142185	-1.28093
0.0153636	-1.2111
0.0165097	-1.14462
0.0176563	-1.08114
0.0188032	-1.02043
0.0199502	-0.962227
0.0210969	-0.906333
0.0222433	-0.85256
0.0233893	-0.800771
0.0245347	-0.750831
0.0256794	-0.702615
0.0268235	-0.656044
0.0279668	-0.611064
0.0291094	-0.567629
0.0302512	-0.525715
0.0313922	-0.485341
0.0325324	-0.44652
0.0336718	-0.409309
0.0348104	-0.373785
0.0359482	-0.340021
0.00490338	0.466742
0.00433876	0.529103
0.00385644	0.5877
0.00346446	0.639752
0.00312441	0.688296
0.0028311	0.73271
0.00258274	0.771834
0.00237906	0.804842
0.00220174	0.834139
0.00204627	0.860016
0.0019088	0.882644
0.00177764	0.904017
0.00164933	0.924234
0.00152342	0.943186
0.00139985	0.960151
0.0012792	0.974887
0.00116156	0.986071
0.00104718	0.993553
0.000936362	0.997325
0.000829484	0.994297
0.000726775	0.984773
0.000628649	0.966344
0.000535794	0.937314
0.000448534	0.896723
0.00036757	0.842326
0.000293472	0.773194
0.00022665	0.687633
0.000167566	0.584839
0.000116876	0.464315
7.50375e-05	0.327113
4.22589e-05	0.174395
1.87595e-05	0.00775639
4.67737e-06	-0.170758
0	-0.35926
0.0359482	-0.340021
0.0370852	-0.308112
0.0382213	-0.278146
0.0393567	-0.250185
0.0404913	-0.224284
0.0416251	-0.200442
0.042758	-0.178655
0.0438902	-0.158829
0.0450216	-0.140897
0.0461522	-0.124693
0.047282	-0.110125
0.0484109	-0.0969779
0.049539	-0.0851716
0.0506663	-0.0744778
0.0517926	-0.0648447
0.0529181	-0.0560365
0.0540426	-0.0480745
0.0551662	-0.0407082
0.0562887	-0.0340525
0.0574102	-0.0278256
0.0585306	-0.0223522
0.0596498	-0.0169992
0.0607678	-0.011805
0.0618846	-0.00455004
0.063	-0.00510343
)