NACA 63-212 AIRFOIL 26. 26. 0.000000 0.000000 0.004170 0.010320 0.006570 0.012600 0.011450 0.016220 0.023780 0.022840 0.048630 0.032380 0.073580 0.039630 0.098590 0.045540 0.148680 0.054700 0.198820 0.061370 0.249000 0.066060 0.299200 0.069010 0.349410 0.070300 0.399620 0.069910 0.449820 0.067990 0.500000 0.064730 0.550160 0.060300 0.600290 0.054910 0.650380 0.048700 0.700430 0.041820 0.750450 0.034510 0.800420 0.026980 0.850350 0.019470 0.900250 0.012240 0.950120 0.005660 1.000000 0.000000 0.000000 0.000000 0.005380 -0.009320 0.008430 -0.011200 0.013550 -0.014080 0.026220 -0.019120 0.051370 -0.026060 0.076420 -0.031150 0.101410 -0.035200 0.151320 -0.041240 0.201180 -0.045450 0.251000 -0.048160 0.300800 -0.049570 0.350590 -0.049700 0.400380 -0.048490 0.450180 -0.046090 0.500000 -0.042670 0.548480 -0.038400 0.599710 -0.033490 0.649620 -0.028100 0.699570 -0.022380 0.749550 -0.016610 0.799580 -0.011060 0.849650 -0.006010 0.899750 -0.001900 0.949880 0.000660 1.000000 0.000000