XFOIL Version 6.94 Calculated polar for: SD7003-085-88 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.1825 0.00652 0.00223 -0.0354 0.8095 0.9623 0.500 0.2655 0.00666 0.00203 -0.0404 0.7458 1.0000 1.000 0.3103 0.00694 0.00198 -0.0380 0.6859 1.0000 1.500 0.3595 0.00728 0.00200 -0.0364 0.6274 1.0000 2.000 0.4107 0.00765 0.00210 -0.0352 0.5689 1.0000 2.500 0.4627 0.00808 0.00226 -0.0342 0.5116 1.0000 3.000 0.5150 0.00855 0.00248 -0.0334 0.4562 1.0000 3.500 0.5677 0.00904 0.00277 -0.0327 0.4021 1.0000 4.000 0.6203 0.00958 0.00313 -0.0320 0.3504 1.0000 4.500 0.6727 0.01019 0.00358 -0.0313 0.3009 1.0000 5.000 0.7247 0.01089 0.00410 -0.0306 0.2557 1.0000 5.500 0.7768 0.01159 0.00472 -0.0300 0.2143 1.0000 6.000 0.8282 0.01241 0.00544 -0.0293 0.1789 1.0000 6.500 0.8790 0.01329 0.00629 -0.0285 0.1477 1.0000 7.000 0.9293 0.01422 0.00719 -0.0276 0.1189 1.0000 7.500 0.9782 0.01532 0.00824 -0.0267 0.0941 1.0000 8.000 1.0268 0.01641 0.00940 -0.0257 0.0727 1.0000 8.500 1.0718 0.01802 0.01103 -0.0243 0.0526 1.0000 9.000 1.1132 0.02006 0.01320 -0.0224 0.0385 1.0000 9.500 1.1478 0.02295 0.01623 -0.0198 0.0316 1.0000 10.000 1.1862 0.02508 0.01866 -0.0176 0.0280 1.0000 10.500 1.2179 0.02787 0.02165 -0.0151 0.0255 1.0000 11.000 1.2342 0.03311 0.02731 -0.0115 0.0234 1.0000 11.500 1.2526 0.03612 0.03074 -0.0080 0.0221 1.0000 12.000 1.2502 0.04040 0.03543 -0.0033 0.0211 1.0000 12.500 1.2380 0.04592 0.04134 -0.0009 0.0204 1.0000 13.000 1.2180 0.05352 0.04932 -0.0022 0.0199 1.0000 13.500 1.1924 0.06357 0.05975 -0.0073 0.0195 1.0000 14.000 1.1494 0.07876 0.07536 -0.0171 0.0198 1.0000 14.500 1.0753 0.10338 0.10044 -0.0340 0.0210 1.0000 15.000 0.9349 0.15389 0.15117 -0.0638 0.0245 1.0000 17.000 0.7206 0.19662 0.19430 -0.0859 0.0349 1.0000 19.000 0.9747 0.25041 0.24759 -0.1098 0.0236 1.0000 19.500 0.9826 0.25828 0.25542 -0.1180 0.0226 1.0000 20.000 0.9973 0.26622 0.26336 -0.1233 0.0197 1.0000 20.500 1.0140 0.27260 0.26975 -0.1271 0.0182 1.0000 21.000 1.0338 0.28121 0.27840 -0.1286 0.0172 1.0000 21.500 1.0469 0.28866 0.28584 -0.1343 0.0170 1.0000 22.000 1.0589 0.29599 0.29313 -0.1417 0.0160 1.0000 22.500 1.0747 0.30324 0.30040 -0.1466 0.0145 1.0000 23.000 1.0901 0.30973 0.30690 -0.1510 0.0135 1.0000 23.500 1.1058 0.31547 0.31265 -0.1548 0.0127 1.0000 24.000 1.1218 0.32388 0.32107 -0.1579 0.0122 1.0000 24.500 1.1348 0.33016 0.32734 -0.1648 0.0118 1.0000 25.000 1.1503 0.33732 0.33452 -0.1700 0.0104 1.0000 25.500 1.1650 0.34360 0.34081 -0.1747 0.0097 1.0000 26.000 1.1793 0.34942 0.34664 -0.1792 0.0091 1.0000 26.500 1.1929 0.35498 0.35223 -0.1833 0.0087 1.0000 27.000 1.2073 0.36299 0.36025 -0.1867 0.0085 1.0000 27.500 1.2201 0.36795 0.36521 -0.1924 0.0084 1.0000 28.000 1.2338 0.37305 0.37030 -0.1982 0.0083 1.0000 28.500 1.2479 0.37876 0.37603 -0.2034 0.0078 1.0000 29.000 1.2610 0.38402 0.38131 -0.2083 0.0073 1.0000 29.500 1.2738 0.38906 0.38637 -0.2132 0.0069 1.0000 30.000 1.2859 0.39389 0.39122 -0.2181 0.0065 1.0000 30.500 1.2975 0.39851 0.39586 -0.2229 0.0062 1.0000 31.000 1.3085 0.40294 0.40031 -0.2277 0.0060 1.0000 31.500 1.3185 0.40719 0.40458 -0.2323 0.0058 1.0000 32.500 1.3389 0.41726 0.41469 -0.2419 0.0056 1.0000 33.000 1.3496 0.42182 0.41927 -0.2474 0.0055 1.0000 33.500 1.3604 0.42689 0.42436 -0.2525 0.0053 1.0000 34.000 1.3702 0.43171 0.42919 -0.2575 0.0048 1.0000 34.500 1.3790 0.43611 0.43362 -0.2625 0.0044 1.0000 35.000 1.3871 0.44028 0.43782 -0.2674 0.0042 1.0000 35.500 1.3946 0.44442 0.44198 -0.2724 0.0040 1.0000 36.000 1.4017 0.44835 0.44594 -0.2774 0.0038 1.0000 36.500 1.4079 0.45206 0.44968 -0.2823 0.0037 1.0000 37.000 1.4130 0.45581 0.45346 -0.2870 0.0036 1.0000 38.500 1.4302 0.46814 0.46585 -0.3022 0.0035 1.0000 39.000 1.4349 0.47183 0.46958 -0.3072 0.0035 1.0000 39.500 1.4397 0.47563 0.47340 -0.3123 0.0035 1.0000 40.000 1.4443 0.47957 0.47736 -0.3174 0.0035 1.0000 40.500 1.4479 0.48331 0.48114 -0.3223 0.0034 1.0000 41.000 1.4514 0.48709 0.48494 -0.3273 0.0033 1.0000 41.500 1.4541 0.49068 0.48857 -0.3322 0.0031 1.0000 42.000 1.4565 0.49418 0.49210 -0.3372 0.0029 1.0000 42.500 1.4577 0.49741 0.49536 -0.3421 0.0027 1.0000 43.000 1.4589 0.50065 0.49863 -0.3471 0.0026 1.0000 43.500 1.4593 0.50362 0.50163 -0.3520 0.0025 1.0000 44.000 1.4595 0.50669 0.50473 -0.3570 0.0023 1.0000 44.500 1.4586 0.50939 0.50746 -0.3619 0.0022 1.0000 45.000 1.4572 0.51196 0.51007 -0.3669 0.0021 1.0000 45.500 1.4548 0.51427 0.51242 -0.3718 0.0021 1.0000