NASA/LANGLEY NLF(1)-0215F AIRFOIL 33. 29. 0.000000 0.000000 0.002400 0.009170 0.009090 0.019470 0.020040 0.030270 0.035270 0.041200 0.054690 0.052010 0.078160 0.062500 0.105460 0.072470 0.136350 0.081750 0.170500 0.090190 0.207580 0.097610 0.247200 0.103890 0.288940 0.108870 0.332370 0.112400 0.377020 0.114280 0.422530 0.114270 0.468640 0.112190 0.515240 0.107840 0.562470 0.101470 0.610100 0.093730 0.657520 0.085130 0.704080 0.076030 0.749140 0.066730 0.792060 0.057460 0.832220 0.048440 0.869020 0.039830 0.901930 0.031750 0.930440 0.024280 0.954090 0.017370 0.972850 0.010820 0.987100 0.005070 0.996580 0.001260 1.000000 0.000000 0.000000 0.000000 0.002450 -0.007040 0.010990 -0.012110 0.025920 -0.016560 0.046530 -0.020520 0.072420 -0.023990 0.103240 -0.026990 0.138540 -0.029540 0.177880 -0.031660 0.220730 -0.033340 0.266540 -0.034560 0.314730 -0.035310 0.364680 -0.035540 0.415760 -0.035190 0.467310 -0.034150 0.518670 -0.032250 0.569200 -0.029250 0.618250 -0.024410 0.666620 -0.016630 0.716140 -0.007050 0.766450 0.001670 0.815650 0.008040 0.861980 0.011550 0.903590 0.011980 0.938620 0.009900 0.965880 0.006550 0.985040 0.003230 0.996300 0.000860 1.000000 0.000000