56 lines
1.2 KiB
Text
56 lines
1.2 KiB
Text
NACA 63A010 AIRFOIL
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26. 26.
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0.000000 0.000000
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0.005000 0.008160
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0.007500 0.009830
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0.012500 0.012500
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0.025000 0.017370
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0.050000 0.024120
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0.075000 0.029170
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0.100000 0.033240
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0.150000 0.039500
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0.200000 0.044000
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0.250000 0.047140
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0.300000 0.049130
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0.350000 0.049950
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0.400000 0.049680
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0.450000 0.048370
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0.500000 0.046130
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0.550000 0.043110
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0.600000 0.039430
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0.650000 0.035170
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0.700000 0.030440
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0.750000 0.025450
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0.800000 0.020400
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0.850000 0.015350
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0.900000 0.010300
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0.950000 0.005250
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1.000000 0.000210
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0.000000 0.000000
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0.005000 -0.008160
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0.007500 -0.009830
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0.012500 -0.012500
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0.025000 -0.017370
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0.050000 -0.024120
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0.075000 -0.029170
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0.100000 -0.033240
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0.150000 -0.039500
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0.200000 -0.044000
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0.250000 -0.047140
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0.300000 -0.049130
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0.350000 -0.049950
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0.400000 -0.049680
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0.450000 -0.048370
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0.500000 -0.046130
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0.550000 -0.043110
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0.600000 -0.039430
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0.650000 -0.035170
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0.700000 -0.030440
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0.750000 -0.025450
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0.800000 -0.020400
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0.850000 -0.015350
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0.900000 -0.010300
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0.950000 -0.005250
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1.000000 -0.000210
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