XFOIL Version 6.96 Calculated polar for: AH 79-K-143/18 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -15.250 -0.8581 0.04981 0.04633 -0.0915 0.7745 0.0049 -15.000 -0.8696 0.04415 0.04049 -0.0961 0.7740 0.0048 -14.750 -0.8864 0.03895 0.03507 -0.0990 0.7734 0.0049 -14.500 -0.8779 0.03698 0.03300 -0.1000 0.7727 0.0049 -14.250 -0.8863 0.03367 0.02948 -0.1000 0.7722 0.0049 -14.000 -0.8807 0.03183 0.02754 -0.0997 0.7716 0.0051 -13.750 -0.8752 0.03003 0.02561 -0.0991 0.7710 0.0050 -13.500 -0.8672 0.02844 0.02389 -0.0985 0.7703 0.0052 -13.250 -0.8550 0.02722 0.02256 -0.0979 0.7697 0.0052 -13.000 -0.8468 0.02564 0.02082 -0.0968 0.7690 0.0052 -12.750 -0.8334 0.02452 0.01959 -0.0959 0.7683 0.0052 -12.500 -0.8185 0.02352 0.01849 -0.0951 0.7675 0.0054 -12.250 -0.8059 0.02234 0.01717 -0.0939 0.7668 0.0054 -12.000 -0.7896 0.02151 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0.00213 -0.0596 0.6340 0.8667 2.750 0.6018 0.00625 0.00218 -0.0593 0.6241 0.8678 3.000 0.6275 0.00633 0.00225 -0.0590 0.6143 0.8688 3.250 0.6532 0.00642 0.00232 -0.0587 0.6037 0.8698 3.500 0.6781 0.00653 0.00240 -0.0582 0.5924 0.8707 3.750 0.7025 0.00665 0.00249 -0.0577 0.5812 0.8718 4.000 0.7264 0.00678 0.00261 -0.0571 0.5677 0.8730 4.250 0.7480 0.00699 0.00274 -0.0560 0.5468 0.8744 4.500 0.7651 0.00734 0.00295 -0.0540 0.5115 0.8764 4.750 0.7848 0.00760 0.00313 -0.0526 0.4891 0.8780 5.000 0.8040 0.00786 0.00331 -0.0511 0.4656 0.8792 5.250 0.8248 0.00807 0.00348 -0.0499 0.4502 0.8801 5.500 0.8321 0.00865 0.00381 -0.0462 0.3994 0.8816 5.750 0.8380 0.00921 0.00417 -0.0422 0.3516 0.8833 6.000 0.8302 0.00999 0.00464 -0.0355 0.2893 0.8855 6.250 0.8252 0.01066 0.00510 -0.0295 0.2435 0.8875 6.500 0.8131 0.01166 0.00581 -0.0225 0.1849 0.8898 7.000 0.8225 0.01316 0.00710 -0.0159 0.1330 0.8930 7.250 0.8228 0.01424 0.00798 -0.0124 0.0949 0.8945 7.500 0.8268 0.01520 0.00879 -0.0094 0.0624 0.8958 7.750 0.8390 0.01589 0.00940 -0.0076 0.0458 0.8971 8.000 0.8542 0.01647 0.00995 -0.0064 0.0374 0.8980 8.250 0.8692 0.01709 0.01055 -0.0051 0.0302 0.8989 8.500 0.8852 0.01768 0.01112 -0.0041 0.0247 0.8997 8.750 0.9022 0.01825 0.01169 -0.0032 0.0203 0.9005 9.000 0.9183 0.01889 0.01231 -0.0023 0.0163 0.9014 9.250 0.9343 0.01956 0.01298 -0.0014 0.0135 0.9021 9.500 0.9522 0.02014 0.01358 -0.0008 0.0130 0.9029 9.750 0.9682 0.02086 0.01431 0.0000 0.0109 0.9037 10.000 0.9859 0.02149 0.01498 0.0005 0.0106 0.9044 10.250 1.0024 0.02222 0.01573 0.0012 0.0100 0.9052 10.500 1.0188 0.02296 0.01650 0.0017 0.0093 0.9059 10.750 1.0326 0.02389 0.01745 0.0025 0.0083 0.9066 11.000 1.0481 0.02473 0.01833 0.0031 0.0082 0.9073 11.250 1.0633 0.02559 0.01924 0.0037 0.0083 0.9079 11.500 1.0797 0.02641 0.02009 0.0041 0.0077 0.9085 11.750 1.0947 0.02732 0.02105 0.0046 0.0076 0.9091 12.000 1.1077 0.02837 0.02215 0.0053 0.0075 0.9096 12.250 1.1221 0.02942 0.02324 0.0056 0.0074 0.9102 12.500 1.1375 0.03050 0.02438 0.0057 0.0070 0.9109 12.750 1.1502 0.03185 0.02580 0.0060 0.0070 0.9116 13.000 1.1650 0.03302 0.02702 0.0060 0.0069 0.9123 13.250 1.1781 0.03434 0.02839 0.0061 0.0067 0.9132 13.500 1.1897 0.03582 0.02992 0.0063 0.0064 0.9140 13.750 1.2018 0.03726 0.03142 0.0064 0.0063 0.9147 14.000 1.2090 0.03914 0.03339 0.0068 0.0062 0.9154 14.250 1.2164 0.04103 0.03534 0.0071 0.0060 0.9161 14.500 1.2222 0.04312 0.03753 0.0074 0.0060 0.9167 14.750 1.2365 0.04444 0.03891 0.0072 0.0059 0.9174 15.000 1.2452 0.04633 0.04087 0.0072 0.0059 0.9181 15.250 1.2532 0.04827 0.04289 0.0072 0.0058 0.9190 15.500 1.2583 0.05051 0.04522 0.0073 0.0057 0.9199 15.750 1.2652 0.05262 0.04741 0.0073 0.0056 0.9207 16.000 1.2691 0.05509 0.04997 0.0072 0.0054 0.9214 16.250 1.2772 0.05713 0.05208 0.0069 0.0055 0.9221 16.500 1.2762 0.06017 0.05523 0.0069 0.0053 0.9228 16.750 1.2792 0.06280 0.05795 0.0067 0.0053 0.9234 17.000 1.2839 0.06531 0.06054 0.0063 0.0052 0.9240 17.500 1.2859 0.07159 0.06701 0.0049 0.0051 0.9255 17.750 1.2843 0.07507 0.07061 0.0041 0.0051 0.9262 18.000 1.2812 0.07878 0.07443 0.0033 0.0051 0.9270 18.250 1.2816 0.08218 0.07792 0.0022 0.0050 0.9278 18.500 1.2808 0.08576 0.08160 0.0011 0.0050 0.9287 18.750 1.2778 0.08970 0.08564 -0.0002 0.0049 0.9296 19.000 1.2695 0.09430 0.09038 -0.0016 0.0049 0.9304