kc135winglet Airfoil

Boeing KC-135 winglet airfoil

kc135winglet Airfoil (x,y) Co-ordinates

1 -0.002
0.975 0.0038
0.95 0.0089
0.925 0.0138
0.9 0.0184
0.875 0.0228
0.85 0.027
0.825 0.0311
0.8 0.0349
0.775 0.0384
0.75 0.0419
0.725 0.0451
0.7 0.0481
0.675 0.0508
0.65 0.0533
0.625 0.0554
0.6 0.0572
0.575 0.0587
0.55 0.0599
0.5 0.0618
0.45 0.0627
0.4 0.0628
0.35 0.0621
0.3 0.0605
0.25 0.0581
0.2 0.0547
0.175 0.0525
0.15 0.0499
0.125 0.0469
0.1 0.0433
0.075 0.0389
0.05 0.0333
0.0375 0.0296
0.025 0.0249
0.0125 0.0179
0.005 0.0119
0.002 0.0077
1 -0.0067
0.975 -0.0013
0.95 0.0021
0.925 0.0045
0.9 0.0059
0.875 0.0064
0.85 0.0065
0.825 0.006
0.8 0.0049
0.775 0.0036
0.75 0.002
0.725 0.0004
0.7 -0.0015
0.675 -0.0033
0.65 -0.0052
0.625 -0.0071
0.6 -0.009
0.575 -0.0106
0.55 -0.0122
0.5 -0.0144
0.45 -0.0158
0.4 -0.0168
0.35 -0.0174
0.3 -0.0176
0.25 -0.0175
0.2 -0.0167
0.175 -0.0161
0.15 -0.0154
0.125 -0.0144
0.1 -0.0132
0.075 -0.0118
0.05 -0.01
0.0375 -0.009
0.025 -0.0077
0.0125 -0.006
0.005 -0.0041
0.002 -0.0032
0 0

kc135winglet Airfoil CAD files

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