L1003 Airfoil

Liebeck high lift airfoil

L1003 Airfoil (x,y) Co-ordinates

0 0
0.0125 0.02307
0.025 0.03981
0.0375 0.05093
0.05 0.06296
0.075 0.08333
0.1 0.09722
0.15 0.12222
0.2 0.13704
0.25 0.14815
0.3 0.1537
0.35 0.14815
0.4 0.13518
0.45 0.11852
0.5 0.0963
0.55 0.08056
0.6 0.06667
0.65 0.05185
0.7 0.04074
0.75 0.0287
0.8 0.02037
0.85 0.01204
0.9 0.00556
0.95 0.00185
1 0
1 0
0.95 -0.00093
0.9 -0.00185
0.85 -0.00278
0.8 -0.0037
0.75 -0.00556
0.7 -0.00741
0.65 -0.00926
0.6 -0.01111
0.55 -0.01296
0.5 -0.01481
0.45 -0.01667
0.4 -0.01852
0.35 -0.02037
0.3 -0.02315
0.25 -0.02593
0.2 -0.0287
0.15 -0.03333
0.1 -0.03981
0.075 -0.04352
0.05 -0.04907
0.0375 -0.04907
0.025 -0.0463
0.0125 -0.03704
0 0

L1003 Airfoil CAD files

DOWNLOAD FROM HERE

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