naca1408 Airfoil

 NACA 1408 airfoil

naca1408 Airfoil (x,y) Coordinates

1 0.00084
0.95016 0.00698
0.90027 0.01271
0.80039 0.02305
0.70041 0.03193
0.60034 0.03931
0.5002 0.04502
0.4 0.04869
0.2995 0.04939
0.24926 0.04819
0.19904 0.04574
0.14889 0.04171
0.09883 0.03558
0.07386 0.03138
0.04896 0.02602
0.02418 0.01862
0.01189 0.01324
0 0
0.01311 -0.012
0.02582 -0.0162
0.05104 -0.02134
0.07614 -0.02458
0.10117 -0.02682
0.15111 -0.02953
0.20096 -0.03074
0.25074 -0.03101
0.3005 -0.03063
0.4 -0.02869
0.4998 -0.02556
0.59966 -0.02153
0.69959 -0.01693
0.79961 -0.01193
0.89973 -0.00659
0.94984 -0.00378
1 -0.00084

naca1408 Airfoil CAD files

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