XFOIL Version 6.96 Calculated polar for: NACA 0012-64 a=0.8 c(li)=0.2 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 ------ -------- --------- --------- -------- -------- -------- -10.750 -0.4549 0.10389 0.10219 -0.0379 1.0000 0.0049 -10.500 -0.4577 0.10045 0.09877 -0.0385 1.0000 0.0047 -10.250 -0.4593 0.09623 0.09457 -0.0403 0.9994 0.0044 -10.000 -0.4569 0.09072 0.08907 -0.0446 0.9976 0.0042 -9.750 -0.4556 0.08437 0.08272 -0.0502 0.9956 0.0040 -9.500 -0.4616 0.07503 0.07340 -0.0609 0.9906 0.0038 -9.250 -0.4873 0.06409 0.06232 -0.0697 0.9802 0.0036 -9.000 -0.4951 0.05921 0.05733 -0.0702 0.9719 0.0036 -8.750 -0.4979 0.05485 0.05282 -0.0698 0.9650 0.0036 -8.500 -0.4992 0.05100 0.04883 -0.0684 0.9575 0.0036 -8.250 -0.4957 0.04764 0.04531 -0.0669 0.9518 0.0037 -8.000 -0.4897 0.04455 0.04207 -0.0652 0.9457 0.0037 -7.750 -0.4820 0.04147 0.03880 -0.0633 0.9401 0.0038 -7.500 -0.4731 0.03823 0.03535 -0.0612 0.9354 0.0039 -7.250 -0.4632 0.03502 0.03190 -0.0588 0.9302 0.0040 -7.000 -0.4520 0.03197 0.02859 -0.0563 0.9253 0.0041 -6.750 -0.4394 0.02901 0.02535 -0.0537 0.9210 0.0042 -6.500 -0.4254 0.02618 0.02223 -0.0511 0.9161 0.0043 -6.250 -0.4096 0.02335 0.01908 -0.0485 0.9116 0.0046 -5.750 -0.3778 0.01268 0.00722 -0.0420 0.9043 0.0055 -5.500 -0.3529 0.01219 0.00667 -0.0415 0.9005 0.0057 -5.250 -0.3278 0.01178 0.00621 -0.0411 0.8967 0.0059 -5.000 -0.3029 0.01132 0.00567 -0.0406 0.8933 0.0062 -4.750 -0.2785 0.01084 0.00514 -0.0400 0.8895 0.0065 -4.500 -0.2540 0.01040 0.00464 -0.0394 0.8855 0.0069 -4.250 -0.2289 0.01007 0.00425 -0.0390 0.8817 0.0073 -4.000 -0.2042 0.00969 0.00380 -0.0384 0.8780 0.0078 -3.750 -0.1792 0.00936 0.00345 -0.0379 0.8735 0.0084 -3.500 -0.1534 0.00913 0.00320 -0.0376 0.8691 0.0089 -3.250 -0.1274 0.00891 0.00295 -0.0373 0.8652 0.0096 -3.000 -0.1014 0.00870 0.00270 -0.0370 0.8608 0.0104 -2.750 -0.0756 0.00849 0.00245 -0.0366 0.8549 0.0112 -2.500 -0.0495 0.00831 0.00226 -0.0363 0.8489 0.0128 -2.250 -0.0232 0.00817 0.00210 -0.0360 0.8414 0.0141 -2.000 0.0031 0.00805 0.00194 -0.0358 0.8341 0.0154 -1.750 0.0292 0.00790 0.00176 -0.0354 0.8259 0.0179 -1.500 0.0558 0.00780 0.00167 -0.0352 0.8189 0.0211 -1.250 0.0826 0.00772 0.00157 -0.0351 0.8118 0.0233 -1.000 0.1091 0.00762 0.00146 -0.0349 0.8053 0.0286 -0.750 0.1359 0.00756 0.00139 -0.0348 0.7979 0.0330 -0.500 0.1625 0.00750 0.00131 -0.0346 0.7908 0.0393 -0.250 0.1888 0.00743 0.00123 -0.0343 0.7805 0.0541 0.000 0.2130 0.00725 0.00120 -0.0337 0.7662 0.1368 0.250 0.2380 0.00728 0.00117 -0.0331 0.7461 0.1477 0.500 0.2628 0.00731 0.00114 -0.0326 0.7237 0.1552 0.750 0.2872 0.00734 0.00112 -0.0319 0.7018 0.1669 1.000 0.3072 0.00720 0.00114 -0.0305 0.6624 0.2826 1.250 0.3258 0.00752 0.00119 -0.0286 0.5861 0.2978 1.500 0.3442 0.00787 0.00130 -0.0268 0.5119 0.3178 1.750 0.3575 0.00743 0.00134 -0.0243 0.4653 0.5412 2.000 0.3740 0.00747 0.00144 -0.0222 0.4059 0.6310 2.250 0.3920 0.00760 0.00156 -0.0203 0.3522 0.6934 2.500 0.4109 0.00776 0.00170 -0.0186 0.3045 0.7439 2.750 0.4302 0.00788 0.00181 -0.0170 0.2644 0.7881 3.000 0.4558 0.00793 0.00220 -0.0165 0.2264 0.9297 3.250 0.4802 0.00830 0.00243 -0.0160 0.1890 0.9462 3.500 0.5035 0.00861 0.00262 -0.0153 0.1609 0.9541 3.750 0.5284 0.00894 0.00282 -0.0149 0.1327 0.9597 4.000 0.5486 0.00920 0.00299 -0.0134 0.1117 0.9651 4.250 0.5786 0.00953 0.00324 -0.0142 0.0935 0.9678 4.500 0.6077 0.00983 0.00347 -0.0148 0.0808 0.9711 4.750 0.6317 0.01005 0.00366 -0.0142 0.0721 0.9747 5.000 0.6574 0.01031 0.00388 -0.0140 0.0608 0.9769 5.250 0.6889 0.01072 0.00417 -0.0153 0.0428 0.9780 5.500 0.7210 0.01102 0.00444 -0.0167 0.0377 0.9790 5.750 0.7504 0.01130 0.00471 -0.0174 0.0334 0.9800 6.000 0.7793 0.01154 0.00496 -0.0181 0.0325 0.9812 6.250 0.8086 0.01180 0.00524 -0.0188 0.0319 0.9829 6.500 0.8332 0.01205 0.00553 -0.0184 0.0314 0.9852 6.750 0.8613 0.01233 0.00584 -0.0188 0.0309 0.9867 7.000 0.8974 0.01268 0.00621 -0.0212 0.0305 0.9877 7.250 0.9313 0.01302 0.00658 -0.0230 0.0299 0.9889 7.500 0.9609 0.01335 0.00696 -0.0239 0.0295 0.9900 7.750 0.9875 0.01368 0.00734 -0.0241 0.0293 0.9910 8.000 1.0116 0.01400 0.00769 -0.0238 0.0287 0.9919 8.250 1.0353 0.01433 0.00803 -0.0234 0.0273 0.9929 8.500 1.0581 0.01471 0.00844 -0.0228 0.0262 0.9940 8.750 1.0794 0.01517 0.00895 -0.0220 0.0249 0.9949 9.000 1.1029 0.01564 0.00949 -0.0217 0.0240 0.9954 9.250 1.1283 0.01587 0.00975 -0.0218 0.0238 0.9959 9.500 1.1530 0.01607 0.00998 -0.0217 0.0234 0.9964 9.750 1.1770 0.01627 0.01021 -0.0214 0.0224 0.9969 10.000 1.1995 0.01654 0.01051 -0.0209 0.0207 0.9975 10.250 1.2203 0.01686 0.01083 -0.0201 0.0169 0.9981 10.500 1.2369 0.01746 0.01133 -0.0186 0.0105 0.9989 10.750 1.2524 0.01815 0.01204 -0.0169 0.0077 0.9997 11.000 1.2644 0.01873 0.01267 -0.0144 0.0066 1.0000 11.250 1.2694 0.01931 0.01331 -0.0105 0.0057 1.0000 11.500 1.2765 0.01983 0.01389 -0.0070 0.0052 1.0000 11.750 1.2836 0.02040 0.01452 -0.0036 0.0047 1.0000 12.000 1.2904 0.02103 0.01522 -0.0003 0.0043 1.0000 12.250 1.2967 0.02174 0.01600 0.0030 0.0039 1.0000 12.500 1.3034 0.02248 0.01682 0.0061 0.0036 1.0000 12.750 1.3116 0.02318 0.01760 0.0088 0.0035 1.0000 13.000 1.3196 0.02394 0.01845 0.0115 0.0033 1.0000 13.250 1.3272 0.02479 0.01938 0.0140 0.0031 1.0000 13.500 1.3344 0.02573 0.02041 0.0165 0.0030 1.0000 13.750 1.3413 0.02676 0.02153 0.0188 0.0028 1.0000 14.000 1.3475 0.02791 0.02277 0.0210 0.0027 1.0000 14.250 1.3526 0.02922 0.02418 0.0232 0.0025 1.0000 14.500 1.3559 0.03074 0.02581 0.0253 0.0024 1.0000 14.750 1.3595 0.03229 0.02747 0.0272 0.0023 1.0000 15.000 1.3636 0.03385 0.02914 0.0288 0.0023 1.0000 15.250 1.3666 0.03556 0.03098 0.0303 0.0022 1.0000 15.500 1.3678 0.03750 0.03304 0.0317 0.0021 1.0000 15.750 1.3684 0.03960 0.03526 0.0329 0.0021 1.0000 16.000 1.3668 0.04199 0.03777 0.0339 0.0020 1.0000 16.250 1.3638 0.04465 0.04056 0.0347 0.0020 1.0000 16.500 1.3593 0.04765 0.04369 0.0351 0.0019 1.0000 16.750 1.3530 0.05102 0.04720 0.0351 0.0019 1.0000 17.000 1.3445 0.05488 0.05120 0.0347 0.0019 1.0000 17.250 1.3337 0.05936 0.05582 0.0336 0.0018 1.0000 17.500 1.3201 0.06458 0.06119 0.0319 0.0018 1.0000 17.750 1.3023 0.07084 0.06761 0.0294 0.0018 1.0000 18.000 1.2792 0.07847 0.07542 0.0257 0.0018 1.0000 18.250 1.2470 0.08836 0.08549 0.0206 0.0018 1.0000 18.500 1.1995 0.10190 0.09926 0.0136 0.0019 1.0000 18.750 1.1255 0.12125 0.11885 0.0043 0.0021 1.0000 19.000 1.0381 0.14416 0.14195 -0.0067 0.0023 1.0000