WAL (AIRBUS R 1.25) AIRFOIL
 0.99998     0.00000
 0.99068     0.00214
 0.97422     0.00582
 0.95397     0.01019
 0.93035     0.01508
 0.90595     0.01991
 0.88192     0.02450
 0.85820     0.02890
 0.83442     0.03318
 0.81036     0.03738
 0.78600     0.04151
 0.76141     0.04556
 0.73674     0.04953
 0.71208     0.05339
 0.68754     0.05716
 0.66315     0.06080
 0.63892     0.06427
 0.61480     0.06753
 0.59071     0.07052
 0.56654     0.07325
 0.54222     0.07575
 0.51778     0.07804
 0.49329     0.08013
 0.46891     0.08203
 0.44475     0.08366
 0.42080     0.08496
 0.39695     0.08589
 0.37301     0.08642
 0.34883     0.08658
 0.32439     0.08643
 0.29984     0.08603
 0.27548     0.08542
 0.25163     0.08447
 0.22837     0.08303
 0.20564     0.08096
 0.18319     0.07813
 0.16071     0.07449
 0.13814     0.07010
 0.11583     0.06496
 0.09477     0.05908
 0.07572     0.05252
 0.05749     0.04457
 0.04073     0.03572
 0.02780     0.02772
 0.01712     0.01993
 0.00980     0.01395
 0.00553     0.01001
 0.00285     0.00693
 0.00116     0.00426
 0.00024     0.00182
 0.00000    -0.00050
 0.00047    -0.00280
 0.00162    -0.00511
 0.00346    -0.00747
 0.00611    -0.00985
 0.00978    -0.01221
 0.01490    -0.01420
 0.02227    -0.01515
 0.03376    -0.01571
 0.05057    -0.01686
 0.07071    -0.01754
 0.09378    -0.01768
 0.11701    -0.01727
 0.14065    -0.01649
 0.16509    -0.01568
 0.18985    -0.01497
 0.21457    -0.01422
 0.23921    -0.01336
 0.26378    -0.01235
 0.28824    -0.01131
 0.31262    -0.01041
 0.33706    -0.00971
 0.36165    -0.00915
 0.38642    -0.00865
 0.41132    -0.00816
 0.43623    -0.00764
 0.46108    -0.00715
 0.48582    -0.00673
 0.51049    -0.00642
 0.53514    -0.00623
 0.55980    -0.00608
 0.58450    -0.00593
 0.60921    -0.00569
 0.63390    -0.00537
 0.65853    -0.00504
 0.68310    -0.00476
 0.70765    -0.00461
 0.73221    -0.00461
 0.75681    -0.00467
 0.78141    -0.00467
 0.80591    -0.00454
 0.83020    -0.00423
 0.85430    -0.00380
 0.87840    -0.00330
 0.90291    -0.00279
 0.92752    -0.00233
 0.95192    -0.00189
 0.97328    -0.00150
 0.99042    -0.00118
 1.00000    -0.00100