EPPLER 664 (EXTENDED) AIRFOIL 35. 34. 0.000230 0.002290 0.004680 0.011550 0.013710 0.021830 0.027140 0.032610 0.044870 0.043480 0.066740 0.054160 0.092580 0.064410 0.122160 0.074010 0.155210 0.082770 0.191450 0.090550 0.230510 0.097200 0.272050 0.102620 0.315640 0.106700 0.360870 0.109380 0.407270 0.110600 0.454370 0.110290 0.501670 0.108400 0.548690 0.104820 0.594970 0.099370 0.640630 0.091670 0.685490 0.081970 0.730080 0.071220 0.773530 0.060200 0.815120 0.049420 0.854070 0.039270 0.921100 0.021930 0.969230 0.008810 1.000000 0.000000 1.037090 -0.011320 1.070540 -0.022940 1.100000 -0.035000 1.143910 -0.057080 1.175000 -0.074960 1.193730 -0.086200 1.200000 -0.090000 0.000230 0.002290 0.001460 -0.005210 0.009030 -0.011730 0.022340 -0.018170 0.040970 -0.024230 0.064710 -0.029790 0.093340 -0.034820 0.126510 -0.039360 0.163800 -0.043410 0.204740 -0.046930 0.248820 -0.049900 0.295520 -0.052290 0.344290 -0.054060 0.394520 -0.055220 0.445560 -0.055720 0.496780 -0.055460 0.547540 -0.054330 0.597190 -0.052190 0.645120 -0.048670 0.691170 -0.043220 0.741840 -0.036410 0.791520 -0.030410 0.840000 -0.026500 0.881800 -0.025420 0.921880 -0.026390 0.960000 -0.029000 1.004110 -0.034010 1.044210 -0.040780 1.080000 -0.049000 1.122800 -0.061770 1.156310 -0.073510 1.180470 -0.082540 1.195100 -0.088120 1.200000 -0.090000