Vortex-Panel-Method-for-Airfoil-Aerodynamic-Coefficients/NASA_LS(1)_0413MOD_DATA_POINTS.dat at main · Eliasfarah0/Vortex-Panel-Method-for-Airfoil-Aerodynamic-Coefficients · GitHub

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1.000000 -0.006850
0.975000 0.001500
0.950000 0.007000
0.925000 0.012300
0.900000 0.017400
0.875000 0.022400
0.850000 0.027300
0.825000 0.032100
0.800000 0.036800
0.775000 0.041400
0.750000 0.045800
0.725000 0.050100
0.700000 0.054200
0.675000 0.058100
0.650000 0.061800
0.625000 0.065300
0.600000 0.068500
0.575000 0.071500
0.550000 0.074200
0.525000 0.076600
0.500000 0.078700
0.475000 0.080500
0.450000 0.082000
0.425000 0.083200
0.400000 0.084100
0.375000 0.084700
0.350000 0.085000
0.325000 0.084900
0.300000 0.084400
0.275000 0.083500
0.250000 0.082200
0.225000 0.080500
0.200000 0.078300
0.175000 0.075600
0.150000 0.072200
0.125000 0.068000
0.100000 0.062900
0.075000 0.056400
0.050000 0.047600
0.037500 0.041800
0.025000 0.034200
0.012500 0.024400
0.005000 0.015900
0.002000 0.010400
0.000000 0.000000
0.002000 -0.005000
0.005000 -0.009400
0.012500 -0.014500
0.025000 -0.019100
0.037500 -0.022800
0.050000 -0.025500
0.075000 -0.029900
0.100000 -0.033300
0.125000 -0.036000
0.150000 -0.038200
0.175000 -0.040000
0.200000 -0.041500
0.225000 -0.042700
0.250000 -0.043600
0.275000 -0.044300
0.300000 -0.044800
0.325000 -0.045100
0.350000 -0.045200
0.375000 -0.045000
0.400000 -0.044700
0.425000 -0.044200
0.450000 -0.043500
0.475000 -0.042600
0.500000 -0.041500
0.525000 -0.040100
0.550000 -0.038500
0.575000 -0.036600
0.600000 -0.034400
0.625000 -0.031900
0.650000 -0.029100
0.675000 -0.026200
0.700000 -0.023200
0.725000 -0.020200
0.750000 -0.017200
0.775000 -0.014200
0.800000 -0.011200
0.825000 -0.008400
0.850000 -0.006000
0.875000 -0.003900
0.900000 -0.002600
0.925000 -0.002100
0.950000 -0.002800
0.975000 -0.005100
1.000000 -0.006850