LA5055 Airfoil

Liebeck high lift airfoil

LA5055 Airfoil (x,y) Co-ordinates

0 0
0.0125 0.0306
0.025 0.0426
0.0375 0.0528
0.05 0.0611
0.075 0.0769
0.1 0.088
0.15 0.1065
0.2 0.1185
0.25 0.1287
0.3 0.1343
0.35 0.1389
0.4 0.137
0.45 0.1315
0.5 0.1194
0.55 0.1037
0.6 0.087
0.65 0.0704
0.7 0.0583
0.75 0.0454
0.8 0.0324
0.85 0.0222
0.9 0.0148
0.95 0.0065
1 0
0.95 -0.0005
0.9 -0.0009
0.85 -0.0019
0.8 -0.0037
0.75 -0.0056
0.7 -0.0074
0.65 -0.0083
0.6 -0.0102
0.55 -0.012
0.5 -0.0139
0.45 -0.0148
0.4 -0.0185
0.35 -0.0204
0.3 -0.0231
0.25 -0.025
0.2 -0.0278
0.15 -0.0287
0.1 -0.0306
0.075 -0.0315
0.05 -0.0324
0.0375 -0.0324
0.025 -0.0315
0.0125 -0.0259
0 0

LA5055 Airfoil CAD files

DOWNLOAD FROM HERE

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