DU84132V airfoil CAD files

Airfoil measured from an ASW22 wing

(x,y) Coordinates

0 0
0.00228 0.01002
0.00683 0.01731
0.01595 0.02642
0.02506 0.03371
0.03417 0.03918
0.04328 0.04465
0.06606 0.05467
0.08884 0.06287
0.11162 0.07016
0.1344 0.07563
0.15718 0.08109
0.17995 0.0852
0.20273 0.0886
0.22551 0.09112
0.24829 0.09294
0.27107 0.09476
0.29385 0.0959
0.31663 0.0969
0.33941 0.0974
0.36219 0.09749
0.38497 0.09749
0.40774 0.0974
0.43052 0.09658
0.4533 0.09567
0.47608 0.0939
0.49886 0.09203
0.52164 0.09021
0.54442 0.088
0.5672 0.08565
0.58998 0.0832
0.61276 0.08018
0.63554 0.0773
0.65831 0.0738
0.68109 0.0705
0.70387 0.06651
0.72665 0.06287
0.74943 0.0585
0.77221 0.05467
0.79499 0.05
0.81777 0.0452
0.84055 0.04009
0.86333 0.0352
0.8861 0.03007
0.90888 0.0247
0.93166 0.0192
0.95444 0.0131
0.97722 0.0068
1 0
0 0
0.00228 -0.00547
0.00683 -0.01185
0.01595 -0.0167
0.02506 -0.02005
0.03417 -0.02278
0.04328 -0.0244
0.06606 -0.0288
0.08884 -0.03189
0.11162 -0.03462
0.1344 -0.0362
0.15718 -0.03736
0.17995 -0.0384
0.20273 -0.03918
0.22551 -0.0394
0.24829 -0.0396
0.27107 -0.0396
0.29385 -0.0395
0.31663 -0.0393
0.33941 -0.0389
0.36219 -0.03827
0.38497 -0.03736
0.40774 -0.03645
0.43052 -0.03554
0.4533 -0.03462
0.47608 -0.03371
0.49886 -0.0325
0.52164 -0.0312
0.54442 -0.03
0.5672 -0.0284
0.58998 -0.0269
0.61276 -0.0251
0.63554 -0.0229
0.65831 -0.0205
0.68109 -0.0175
0.70387 -0.0144
0.72665 -0.01093
0.74943 -0.00729
0.77221 -0.00364
0.79499 0
0.81777 0.00273
0.84055 0.00456
0.86333 0.00547
0.8861 0.00547
0.90888 0.00547
0.93166 0.0048
0.95444 0.00364
0.97722 0.0018
1 0

DU84132V airfoil CAD files

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