56 lines
1.2 KiB
Text
56 lines
1.2 KiB
Text
NACA 64-012A AIRFOIL
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26. 26.
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0.000000 0.000000
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0.005000 0.009610
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0.007500 0.011580
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0.012500 0.014640
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0.025000 0.020180
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0.050000 0.027880
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0.075000 0.033640
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0.100000 0.038390
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0.150000 0.045800
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0.200000 0.051320
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0.250000 0.055340
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0.300000 0.058090
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0.350000 0.059650
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0.400000 0.059930
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0.450000 0.058630
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0.500000 0.056050
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0.550000 0.052440
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0.600000 0.048010
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0.650000 0.042890
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0.700000 0.037210
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0.750000 0.031180
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0.800000 0.025000
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0.850000 0.018820
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0.900000 0.012630
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0.950000 0.006440
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1.000000 0.000250
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0.000000 0.000000
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0.005000 -0.009610
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0.007500 -0.011580
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0.012500 -0.014640
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0.025000 -0.020180
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0.050000 -0.027880
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0.075000 -0.033640
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0.100000 -0.038390
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0.150000 -0.045800
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0.200000 -0.051320
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0.250000 -0.055340
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0.300000 -0.058090
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0.350000 -0.059650
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0.400000 -0.059930
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0.450000 -0.058630
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0.500000 -0.056050
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0.550000 -0.052440
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0.600000 -0.048010
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0.650000 -0.042890
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0.700000 -0.037210
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0.750000 -0.031180
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0.800000 -0.025000
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0.850000 -0.018820
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0.900000 -0.012630
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0.950000 -0.006440
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1.000000 -0.000250
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