Airfoil name : NACA1408Upper X Upper Y 0.00000 0.00000 0.10000 0.30000 0.71800 0.93800 1.85200 1.62700 3.49200 2.33900 5.62500 3.02600 8.24200 3.67400 11.31800 4.26400 14.82800 4.78500 18.73500 5.22500 23.00100 5.57100 27.57900 5.81100 32.42000 5.93000 37.46000 5.89900 42.66600 5.69700 47.95600 5.33600 53.27500 4.83500 58.56300 4.23000 63.75800 3.56600 68.00000 3.00600 73.63100 2.27100 78.19500 1.69800 82.43800 1.19700 86.31200 0.78000 89.76900 0.45300 92.76900 0.22000 95.27600 0.08000 97.27200 0.01500 98.75200 0.00500 99.68100 0.00300 100.00000 0.00000 Lower X Lower Y 0.00000 0.00000 0.10000 -0.26000 0.71800 -0.73200 1.85200 -1.16300 3.49200 -1.54600 5.62500 -1.87000 8.24200 -2.13100 11.31800 -2.33100 14.82800 -2.47200 18.73500 -2.55700 23.00100 -2.59300 27.57900 -2.58500 32.42000 -2.53900 37.46000 -2.46000 42.66600 -2.35400 47.95600 -2.22700 53.27500 -2.08300 58.56300 -1.92600 63.75800 -1.75900 68.00000 -1.58600 73.63100 -1.41000 78.19500 -1.23400 82.43800 -1.05900 86.31200 -0.88900 89.76900 -0.72300 92.76900 -0.56400 95.27600 -0.40800 97.27200 -0.24900 98.75200 -0.10900 99.68100 -0.02500 100.00000 0.00000