XFOIL Version 6.96 Calculated polar for: NACA 8-H-12 AIRFOIL 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 ------ -------- --------- --------- -------- -------- -------- -14.000 -1.0843 0.05124 0.04882 -0.0241 0.7843 0.0070 -13.500 -1.1736 0.03636 0.03317 -0.0188 0.7637 0.0070 -13.250 -1.1758 0.03338 0.02992 -0.0167 0.7538 0.0071 -13.000 -1.1703 0.03104 0.02734 -0.0149 0.7441 0.0072 -12.750 -1.1591 0.02924 0.02535 -0.0135 0.7353 0.0074 -12.500 -1.1443 0.02780 0.02374 -0.0122 0.7261 0.0075 -12.250 -1.1281 0.02646 0.02224 -0.0110 0.7182 0.0076 -12.000 -1.1094 0.02541 0.02104 -0.0100 0.7099 0.0077 -11.750 -1.0901 0.02437 0.01987 -0.0090 0.7024 0.0079 -11.500 -1.0698 0.02343 0.01879 -0.0081 0.6948 0.0080 -11.250 -1.0491 0.02251 0.01773 -0.0072 0.6878 0.0082 -11.000 -1.0274 0.02169 0.01678 -0.0064 0.6804 0.0084 -10.750 -1.0054 0.02088 0.01583 -0.0056 0.6740 0.0086 -10.500 -0.9827 0.02013 0.01495 -0.0049 0.6673 0.0088 -10.000 -0.9364 0.01870 0.01325 -0.0035 0.6543 0.0091 -9.750 -0.9127 0.01805 0.01247 -0.0028 0.6475 0.0093 -9.500 -0.8894 0.01729 0.01159 -0.0021 0.6418 0.0096 -9.250 -0.8647 0.01676 0.01099 -0.0015 0.6353 0.0099 -8.750 -0.8139 0.01591 0.00999 -0.0006 0.6225 0.0104 -8.500 -0.7883 0.01550 0.00950 -0.0002 0.6158 0.0107 -8.250 -0.7625 0.01509 0.00901 0.0003 0.6103 0.0110 -8.000 -0.7367 0.01467 0.00850 0.0007 0.6042 0.0113 -7.750 -0.7108 0.01428 0.00801 0.0012 0.5975 0.0116 -7.500 -0.6845 0.01393 0.00757 0.0016 0.5915 0.0119 -7.250 -0.6586 0.01351 0.00710 0.0020 0.5849 0.0123 -7.000 -0.6317 0.01328 0.00683 0.0022 0.5793 0.0128 -6.750 -0.6047 0.01303 0.00654 0.0025 0.5737 0.0133 -6.500 -0.5778 0.01278 0.00623 0.0028 0.5677 0.0137 -6.250 -0.5510 0.01250 0.00589 0.0031 0.5621 0.0142 -6.000 -0.5240 0.01223 0.00555 0.0034 0.5560 0.0147 -5.750 -0.4970 0.01199 0.00524 0.0037 0.5496 0.0150 -5.500 -0.4705 0.01163 0.00485 0.0041 0.5446 0.0156 -5.250 -0.4433 0.01142 0.00460 0.0043 0.5390 0.0161 -5.000 -0.4159 0.01125 0.00439 0.0045 0.5336 0.0168 -4.750 -0.3885 0.01104 0.00415 0.0047 0.5290 0.0174 -4.500 -0.3611 0.01084 0.00390 0.0050 0.5237 0.0180 -4.250 -0.3336 0.01068 0.00368 0.0052 0.5182 0.0183 -4.000 -0.3067 0.01039 0.00335 0.0055 0.5133 0.0191 -3.750 -0.2794 0.01018 0.00313 0.0057 0.5079 0.0199 -3.500 -0.2518 0.01003 0.00294 0.0058 0.5029 0.0207 -3.250 -0.2242 0.00987 0.00275 0.0060 0.4988 0.0213 -3.000 -0.1965 0.00971 0.00257 0.0062 0.4944 0.0220 -2.750 -0.1687 0.00959 0.00241 0.0063 0.4898 0.0225 -2.500 -0.1412 0.00943 0.00222 0.0065 0.4856 0.0237 -2.250 -0.1134 0.00928 0.00207 0.0066 0.4819 0.0248 -2.000 -0.0855 0.00917 0.00194 0.0067 0.4776 0.0260 -1.750 -0.0576 0.00908 0.00182 0.0068 0.4732 0.0272 -1.500 -0.0297 0.00898 0.00172 0.0069 0.4691 0.0299 -1.250 -0.0017 0.00887 0.00162 0.0070 0.4656 0.0337 -1.000 0.0260 0.00875 0.00154 0.0071 0.4619 0.0451 -0.750 0.0537 0.00864 0.00148 0.0072 0.4583 0.0618 -0.500 0.0815 0.00856 0.00143 0.0073 0.4548 0.0771 -0.250 0.1094 0.00845 0.00138 0.0074 0.4521 0.0947 0.000 0.1367 0.00828 0.00134 0.0075 0.4491 0.1378 0.250 0.1633 0.00803 0.00130 0.0077 0.4460 0.2108 0.500 0.1886 0.00767 0.00127 0.0081 0.4427 0.3261 0.750 0.2113 0.00710 0.00124 0.0089 0.4395 0.5089 1.000 0.2289 0.00634 0.00120 0.0110 0.4371 0.7290 1.250 0.2657 0.00578 0.00133 0.0094 0.4343 0.9334 1.500 0.3192 0.00595 0.00149 0.0041 0.4310 0.9651 1.750 0.3572 0.00611 0.00162 0.0021 0.4282 0.9765 2.000 0.4001 0.00626 0.00172 -0.0011 0.4252 0.9823 2.250 0.4336 0.00636 0.00179 -0.0022 0.4227 0.9859 2.500 0.4697 0.00640 0.00182 -0.0040 0.4203 0.9873 2.750 0.5029 0.00645 0.00186 -0.0052 0.4176 0.9885 3.000 0.5352 0.00650 0.00190 -0.0062 0.4152 0.9898 3.250 0.5669 0.00656 0.00195 -0.0070 0.4127 0.9912 3.500 0.5980 0.00664 0.00201 -0.0078 0.4102 0.9925 3.750 0.6287 0.00671 0.00208 -0.0084 0.4076 0.9938 4.000 0.6599 0.00676 0.00214 -0.0092 0.4056 0.9948 4.250 0.6920 0.00680 0.00219 -0.0102 0.4029 0.9955 4.500 0.7237 0.00686 0.00225 -0.0111 0.3983 0.9964 4.750 0.7550 0.00696 0.00232 -0.0120 0.3927 0.9973 5.000 0.7865 0.00700 0.00238 -0.0129 0.3872 0.9982 5.250 0.8174 0.00712 0.00247 -0.0137 0.3773 0.9990 5.500 0.8482 0.00726 0.00256 -0.0146 0.3630 0.9997 5.750 0.8769 0.00742 0.00268 -0.0150 0.3481 1.0000 6.000 0.9023 0.00774 0.00287 -0.0148 0.3159 1.0000 6.250 0.9252 0.00867 0.00342 -0.0148 0.2412 1.0000 6.500 0.9484 0.00942 0.00394 -0.0147 0.1956 1.0000 6.750 0.9714 0.01014 0.00446 -0.0145 0.1562 1.0000 7.000 0.9938 0.01085 0.00499 -0.0143 0.1213 1.0000 7.250 1.0162 0.01148 0.00550 -0.0140 0.0951 1.0000 7.500 1.0383 0.01209 0.00599 -0.0136 0.0737 1.0000 7.750 1.0598 0.01270 0.00652 -0.0131 0.0564 1.0000 8.000 1.0815 0.01323 0.00699 -0.0126 0.0460 1.0000 8.250 1.1027 0.01375 0.00749 -0.0120 0.0375 1.0000 8.500 1.1230 0.01433 0.00802 -0.0114 0.0297 1.0000 8.750 1.1428 0.01488 0.00856 -0.0107 0.0247 1.0000 9.000 1.1620 0.01545 0.00913 -0.0099 0.0215 1.0000 9.250 1.1810 0.01598 0.00968 -0.0091 0.0197 1.0000 9.500 1.1985 0.01658 0.01029 -0.0082 0.0182 1.0000 9.750 1.2139 0.01728 0.01101 -0.0071 0.0169 1.0000 10.000 1.2289 0.01800 0.01178 -0.0062 0.0164 1.0000 10.250 1.2405 0.01892 0.01275 -0.0052 0.0160 1.0000 10.500 1.2410 0.01998 0.01385 -0.0024 0.0156 1.0000 10.750 1.2462 0.02114 0.01506 -0.0008 0.0151 1.0000 11.000 1.2536 0.02239 0.01635 0.0004 0.0149 1.0000 11.250 1.2607 0.02380 0.01780 0.0013 0.0144 1.0000 11.500 1.2674 0.02534 0.01939 0.0020 0.0141 1.0000 11.750 1.2733 0.02701 0.02111 0.0026 0.0137 1.0000 12.000 1.2784 0.02881 0.02297 0.0032 0.0133 1.0000 12.250 1.2844 0.03057 0.02479 0.0036 0.0133 1.0000 12.500 1.2918 0.03222 0.02649 0.0040 0.0131 1.0000 12.750 1.2970 0.03412 0.02845 0.0043 0.0130 1.0000 13.000 1.3021 0.03605 0.03045 0.0046 0.0128 1.0000 13.250 1.3072 0.03800 0.03245 0.0048 0.0127 1.0000 13.500 1.3111 0.04009 0.03461 0.0049 0.0125 1.0000 13.750 1.3143 0.04228 0.03686 0.0051 0.0124 1.0000 14.000 1.3175 0.04457 0.03921 0.0051 0.0122 1.0000 14.250 1.3209 0.04687 0.04157 0.0050 0.0121 1.0000 14.500 1.3232 0.04933 0.04410 0.0049 0.0120 1.0000 14.750 1.3262 0.05178 0.04660 0.0047 0.0118 1.0000 15.000 1.3286 0.05432 0.04922 0.0045 0.0117 1.0000 15.250 1.3303 0.05697 0.05193 0.0042 0.0115 1.0000 15.500 1.3314 0.05974 0.05475 0.0038 0.0115 1.0000 15.750 1.3325 0.06254 0.05762 0.0034 0.0113 1.0000 16.000 1.3335 0.06539 0.06052 0.0029 0.0111 1.0000 16.250 1.3325 0.06852 0.06371 0.0023 0.0109 1.0000 16.500 1.3317 0.07167 0.06693 0.0017 0.0108 1.0000 16.750 1.3276 0.07528 0.07061 0.0009 0.0106 1.0000 17.000 1.3260 0.07859 0.07399 0.0002 0.0105 1.0000 17.250 1.3228 0.08219 0.07767 -0.0007 0.0104 1.0000 17.500 1.3235 0.08531 0.08087 -0.0015 0.0103 1.0000 17.750 1.3262 0.08813 0.08375 -0.0022 0.0102 1.0000 18.000 1.3245 0.09161 0.08731 -0.0032 0.0102 1.0000 18.250 1.3212 0.09534 0.09113 -0.0042 0.0101 1.0000 18.500 1.3199 0.09886 0.09472 -0.0053 0.0100 1.0000 18.750 1.3189 0.10231 0.09824 -0.0064 0.0099 1.0000 19.000 1.3160 0.10611 0.10212 -0.0077 0.0098 1.0000 19.250 1.3133 0.10990 0.10599 -0.0090 0.0097 1.0000