11/26/2015 airfoiltools.com/airfoil/seligdatfile?airfoil=naca23015-il

http://airfoiltools.com/airfoil/seligdatfile?airfoil=naca23015-il 1/1

NACA 23015 1.000000 0.001600 0.950000 0.011200 0.900000 0.020400 0.800000 0.037300 0.700000 0.052500 0.600000 0.066100 0.500000 0.077400 0.400000 0.085900 0.300000 0.090500 0.250000 0.090800 0.200000 0.089200 0.150000 0.085200 0.100000 0.076400 0.075000 0.069000 0.050000 0.058900 0.025000 0.044400 0.012500 0.033400 0.000000 0.000000 0.012500 -0.015400 0.025000 -0.022500 0.050000 -0.030400 0.075000 -0.036100 0.100000 -0.040900 0.150000 -0.048400 0.200000 -0.054100 0.250000 -0.057800 0.300000 -0.059600 0.400000 -0.059200 0.500000 -0.055000 0.600000 -0.048100 0.700000 -0.039100 0.800000 -0.028300 0.900000 -0.015900 0.950000 -0.009000 1.000000 -0.001600