56 lines
1.2 KiB
Text
56 lines
1.2 KiB
Text
NACA 642-015A AIRFOIL
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26. 26.
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0.000000 0.000000
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0.005000 0.011930
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0.007500 0.014360
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0.012500 0.018150
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0.025000 0.025080
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0.050000 0.034770
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0.075000 0.042020
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0.100000 0.047990
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0.150000 0.057320
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0.200000 0.064230
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0.250000 0.069260
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0.300000 0.072700
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0.350000 0.074630
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0.400000 0.074870
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0.450000 0.073130
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0.500000 0.069780
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0.550000 0.065170
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0.600000 0.059560
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0.650000 0.053110
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0.700000 0.046000
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0.750000 0.038470
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0.800000 0.030840
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0.850000 0.023210
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0.900000 0.015580
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0.950000 0.007950
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1.000000 0.000320
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0.000000 0.000000
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0.005000 -0.011930
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0.007500 -0.014360
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0.012500 -0.018150
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0.025000 -0.025080
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0.050000 -0.034770
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0.075000 -0.042020
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0.100000 -0.047990
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0.150000 -0.057320
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0.200000 -0.064230
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0.250000 -0.069260
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0.300000 -0.072700
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0.350000 -0.074630
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0.400000 -0.074870
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0.450000 -0.073130
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0.500000 -0.069780
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0.550000 -0.065170
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0.600000 -0.059560
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0.650000 -0.053110
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0.700000 -0.046000
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0.750000 -0.038470
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0.800000 -0.030840
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0.850000 -0.023210
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0.900000 -0.015580
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0.950000 -0.007950
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1.000000 -0.000320
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