SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) 48. 50. 0.000000 0.000000 0.002000 0.009500 0.005000 0.015800 0.010000 0.021900 0.020000 0.029300 0.030000 0.034300 0.040000 0.038100 0.050000 0.041100 0.070000 0.046200 0.100000 0.051800 0.120000 0.054800 0.150000 0.058500 0.170000 0.060600 0.200000 0.063200 0.220000 0.064600 0.250000 0.066400 0.270000 0.067300 0.300000 0.068500 0.330000 0.069200 0.350000 0.069600 0.380000 0.069800 0.400000 0.069700 0.430000 0.069500 0.450000 0.069200 0.480000 0.068400 0.500000 0.067800 0.530000 0.066600 0.550000 0.065600 0.570000 0.064500 0.600000 0.062500 0.620000 0.061000 0.650000 0.058500 0.680000 0.055500 0.700000 0.053300 0.720000 0.050900 0.750000 0.046900 0.770000 0.043900 0.800000 0.038900 0.820000 0.035300 0.850000 0.029400 0.870000 0.025100 0.900000 0.018100 0.920000 0.013100 0.950000 0.004900 0.970000 -0.000900 0.980000 -0.003900 0.990000 -0.007100 1.000000 -0.010400 0.000000 0.000000 0.002000 -0.009300 0.005000 -0.016000 0.010000 -0.022100 0.020000 -0.029500 0.030000 -0.034400 0.040000 -0.038100 0.050000 -0.041200 0.070000 -0.046200 0.100000 -0.051700 0.120000 -0.054700 0.150000 -0.058500 0.170000 -0.060600 0.200000 -0.063300 0.220000 -0.064700 0.250000 -0.066600 0.280000 -0.068000 0.300000 -0.068700 0.320000 -0.069200 0.350000 -0.069600 0.370000 -0.069600 0.400000 -0.069200 0.420000 -0.068800 0.450000 -0.067600 0.480000 -0.065700 0.500000 -0.064400 0.530000 -0.061400 0.550000 -0.058800 0.580000 -0.054300 0.600000 -0.050900 0.630000 -0.045100 0.650000 -0.041000 0.680000 -0.034600 0.700000 -0.030200 0.730000 -0.023500 0.750000 -0.019200 0.770000 -0.015000 0.800000 -0.009300 0.830000 -0.004800 0.850000 -0.002400 0.870000 -0.001300 0.890000 -0.000800 0.920000 -0.001600 0.940000 -0.003500 0.950000 -0.004900 0.960000 -0.006600 0.970000 -0.008500 0.980000 -0.010900 0.990000 -0.013700 1.000000 -0.016300