56 lines
1.2 KiB
Text
56 lines
1.2 KiB
Text
NACA 63-015A AIRFOIL
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26. 26.
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0.000000 0.000000
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0.005000 0.012030
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0.007500 0.014480
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0.012500 0.018440
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0.025000 0.025790
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0.050000 0.036180
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0.075000 0.043820
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0.100000 0.049970
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0.150000 0.059420
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0.200000 0.066190
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0.250000 0.070910
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0.300000 0.073840
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0.350000 0.074960
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0.400000 0.074350
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0.450000 0.072150
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0.500000 0.068580
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0.550000 0.063870
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0.600000 0.058200
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0.650000 0.051730
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0.700000 0.044680
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0.750000 0.037310
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0.800000 0.029910
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0.850000 0.022520
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0.900000 0.015120
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0.950000 0.007720
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1.000000 0.000320
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0.000000 0.000000
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0.005000 -0.012030
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0.007500 -0.014480
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0.012500 -0.018440
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0.025000 -0.025790
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0.050000 -0.036180
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0.075000 -0.043820
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0.100000 -0.049970
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0.150000 -0.059420
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0.200000 -0.066190
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0.250000 -0.070910
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0.300000 -0.073840
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0.350000 -0.074960
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0.400000 -0.074350
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0.450000 -0.072150
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0.500000 -0.068580
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0.550000 -0.063870
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0.600000 -0.058200
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0.650000 -0.051730
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0.700000 -0.044680
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0.750000 -0.037310
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0.800000 -0.029910
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0.850000 -0.022520
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0.900000 -0.015120
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0.950000 -0.007720
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1.000000 -0.000320
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