56 lines
1.2 KiB
Text
56 lines
1.2 KiB
Text
NACA 63012A AIRFOIL
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26.0000 26.0000
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0.000000 0.000000
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0.005000 0.009730
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0.007500 0.011730
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0.012500 0.014920
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0.025000 0.020780
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0.050000 0.028950
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0.075000 0.035040
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0.100000 0.039940
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0.150000 0.047470
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0.200000 0.052870
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0.250000 0.056640
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0.300000 0.059010
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0.350000 0.059950
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0.400000 0.059570
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0.450000 0.057920
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0.500000 0.055170
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0.550000 0.051480
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0.600000 0.047000
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0.650000 0.041860
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0.700000 0.036210
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0.750000 0.030260
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0.800000 0.024260
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0.850000 0.018260
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0.900000 0.012250
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0.950000 0.006250
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1.000000 0.000250
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0.000000 0.000000
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0.005000 -0.009730
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0.007500 -0.011730
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0.012500 -0.014920
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0.025000 -0.020780
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0.050000 -0.028950
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0.075000 -0.035040
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0.100000 -0.039940
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0.150000 -0.047470
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0.200000 -0.052870
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0.250000 -0.056640
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0.300000 -0.059010
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0.350000 -0.059950
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0.400000 -0.059570
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0.450000 -0.057920
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0.500000 -0.055170
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0.550000 -0.051480
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0.600000 -0.047000
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0.650000 -0.041860
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0.700000 -0.036210
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0.750000 -0.030260
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0.800000 -0.024260
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0.850000 -0.018260
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0.900000 -0.012250
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0.950000 -0.006250
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1.000000 -0.000250
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