XFOIL Version 6.96 Calculated polar for: NACA 63(3)-018 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.750 -1.2070 0.10046 0.09601 -0.0076 1.0000 0.0186 -19.500 -1.2093 0.09639 0.09186 -0.0096 1.0000 0.0195 -19.250 -1.2104 0.09255 0.08793 -0.0114 1.0000 0.0204 -19.000 -1.2117 0.08875 0.08405 -0.0131 1.0000 0.0211 -18.750 -1.2127 0.08506 0.08030 -0.0147 1.0000 0.0220 -18.500 -1.2121 0.08164 0.07681 -0.0161 1.0000 0.0227 -18.250 -1.2105 0.07841 0.07351 -0.0174 1.0000 0.0236 -18.000 -1.2075 0.07543 0.07044 -0.0185 1.0000 0.0245 -17.750 -1.2036 0.07264 0.06755 -0.0194 1.0000 0.0252 -17.500 -1.2026 0.06950 0.06436 -0.0205 1.0000 0.0258 -17.250 -1.1996 0.06665 0.06147 -0.0215 1.0000 0.0265 -17.000 -1.1954 0.06400 0.05876 -0.0223 1.0000 0.0273 -16.750 -1.1904 0.06151 0.05620 -0.0230 1.0000 0.0281 -16.500 -1.1836 0.05927 0.05390 -0.0235 1.0000 0.0291 -16.250 -1.1767 0.05708 0.05163 -0.0240 1.0000 0.0298 -16.000 -1.1701 0.05488 0.04936 -0.0245 1.0000 0.0303 -15.750 -1.1664 0.05241 0.04684 -0.0249 1.0000 0.0311 -15.500 -1.1613 0.05015 0.04453 -0.0253 1.0000 0.0317 -15.250 -1.1542 0.04813 0.04248 -0.0256 1.0000 0.0326 -15.000 -1.1471 0.04615 0.04045 -0.0258 1.0000 0.0333 -14.750 -1.1387 0.04435 0.03859 -0.0259 1.0000 0.0342 -14.500 -1.1302 0.04260 0.03678 -0.0259 1.0000 0.0349 -14.250 -1.1210 0.04093 0.03505 -0.0259 1.0000 0.0356 -14.000 -1.1103 0.03944 0.03349 -0.0259 1.0000 0.0362 -13.750 -1.1053 0.03751 0.03154 -0.0257 1.0000 0.0374 -13.500 -1.0981 0.03582 0.02983 -0.0254 1.0000 0.0384 -13.250 -1.0897 0.03426 0.02823 -0.0252 1.0000 0.0392 -13.000 -1.0793 0.03288 0.02683 -0.0249 1.0000 0.0405 -12.750 -1.0686 0.03156 0.02547 -0.0245 1.0000 0.0415 -12.500 -1.0569 0.03034 0.02420 -0.0242 1.0000 0.0425 -12.250 -1.0475 0.02912 0.02292 -0.0234 0.9639 0.0430 -12.000 -1.0179 0.02754 0.02122 -0.0272 0.9123 0.0446 -11.750 -1.0095 0.02636 0.01991 -0.0262 0.8808 0.0456 -11.500 -1.0016 0.02526 0.01871 -0.0249 0.8606 0.0465 -11.250 -0.9926 0.02423 0.01758 -0.0236 0.8450 0.0475 -11.000 -0.9823 0.02328 0.01654 -0.0224 0.8318 0.0487 -10.750 -0.9711 0.02239 0.01556 -0.0212 0.8205 0.0499 -10.500 -0.9594 0.02157 0.01464 -0.0200 0.8097 0.0510 -10.250 -0.9478 0.02074 0.01374 -0.0187 0.7996 0.0521 -10.000 -0.9381 0.01985 0.01279 -0.0171 0.7908 0.0540 -9.750 -0.9269 0.01907 0.01197 -0.0156 0.7815 0.0558 -9.500 -0.9151 0.01838 0.01121 -0.0140 0.7733 0.0579 -9.250 -0.9025 0.01776 0.01053 -0.0124 0.7650 0.0601 -9.000 -0.8910 0.01716 0.00988 -0.0105 0.7577 0.0629 -8.750 -0.8813 0.01657 0.00927 -0.0082 0.7497 0.0671 -8.500 -0.8687 0.01616 0.00881 -0.0061 0.7429 0.0715 -8.250 -0.8537 0.01565 0.00831 -0.0045 0.7358 0.0788 -8.000 -0.8364 0.01518 0.00784 -0.0032 0.7292 0.0877 -7.750 -0.8180 0.01470 0.00739 -0.0020 0.7230 0.0993 -7.500 -0.7991 0.01421 0.00694 -0.0010 0.7163 0.1142 -7.250 -0.7794 0.01373 0.00650 0.0000 0.7103 0.1316 -7.000 -0.7587 0.01325 0.00609 0.0007 0.7042 0.1515 -6.750 -0.7383 0.01271 0.00566 0.0015 0.6981 0.1767 -6.500 -0.7177 0.01216 0.00522 0.0023 0.6924 0.2078 -6.250 -0.6963 0.01159 0.00480 0.0029 0.6863 0.2432 -6.000 -0.6742 0.01108 0.00441 0.0035 0.6807 0.2782 -5.750 -0.6510 0.01061 0.00408 0.0039 0.6756 0.3131 -5.500 -0.6267 0.01021 0.00380 0.0042 0.6699 0.3464 -5.250 -0.6012 0.00992 0.00358 0.0044 0.6641 0.3746 -5.000 -0.5746 0.00971 0.00341 0.0045 0.6590 0.3968 -4.750 -0.5473 0.00954 0.00327 0.0044 0.6536 0.4149 -4.500 -0.5203 0.00936 0.00315 0.0044 0.6484 0.4378 -4.250 -0.4929 0.00924 0.00305 0.0044 0.6435 0.4568 -4.000 -0.4644 0.00915 0.00296 0.0042 0.6380 0.4682 -3.750 -0.4359 0.00908 0.00287 0.0040 0.6325 0.4770 -3.250 -0.3786 0.00898 0.00272 0.0036 0.6231 0.4967 -3.000 -0.3498 0.00891 0.00266 0.0034 0.6178 0.5027 -2.750 -0.3210 0.00888 0.00258 0.0031 0.6128 0.5084 -2.250 -0.2628 0.00880 0.00247 0.0026 0.6033 0.5191 -2.000 -0.2337 0.00877 0.00242 0.0023 0.5985 0.5247 -1.750 -0.2045 0.00877 0.00237 0.0020 0.5940 0.5296 -1.500 -0.1754 0.00872 0.00234 0.0018 0.5890 0.5342 -1.250 -0.1462 0.00870 0.00231 0.0015 0.5843 0.5389 -1.000 -0.1170 0.00870 0.00228 0.0012 0.5799 0.5438 -0.750 -0.0877 0.00869 0.00226 0.0009 0.5755 0.5481 -0.500 -0.0585 0.00866 0.00225 0.0006 0.5705 0.5524 -0.250 -0.0293 0.00866 0.00224 0.0003 0.5660 0.5572 0.000 0.0000 0.00869 0.00223 0.0000 0.5619 0.5619 0.250 0.0293 0.00866 0.00224 -0.0003 0.5572 0.5660 0.500 0.0585 0.00866 0.00225 -0.0006 0.5524 0.5705 0.750 0.0877 0.00869 0.00226 -0.0009 0.5481 0.5755 1.000 0.1170 0.00870 0.00228 -0.0012 0.5438 0.5799 1.250 0.1462 0.00870 0.00231 -0.0015 0.5389 0.5843 1.500 0.1754 0.00872 0.00234 -0.0018 0.5342 0.5890 1.750 0.2045 0.00877 0.00237 -0.0020 0.5296 0.5940 2.000 0.2337 0.00877 0.00242 -0.0023 0.5247 0.5985 2.250 0.2628 0.00880 0.00247 -0.0026 0.5191 0.6033 2.750 0.3210 0.00888 0.00258 -0.0031 0.5084 0.6128 3.000 0.3498 0.00891 0.00266 -0.0034 0.5027 0.6178 3.250 0.3786 0.00898 0.00272 -0.0036 0.4967 0.6231 3.750 0.4359 0.00908 0.00287 -0.0040 0.4770 0.6325 4.000 0.4644 0.00915 0.00296 -0.0042 0.4682 0.6380 4.250 0.4929 0.00924 0.00305 -0.0044 0.4568 0.6435 4.500 0.5203 0.00936 0.00315 -0.0044 0.4378 0.6484 4.750 0.5473 0.00954 0.00327 -0.0044 0.4148 0.6536 5.000 0.5747 0.00971 0.00341 -0.0045 0.3968 0.6590 5.250 0.6013 0.00991 0.00358 -0.0044 0.3755 0.6642 5.500 0.6267 0.01021 0.00380 -0.0042 0.3468 0.6699 5.750 0.6511 0.01061 0.00408 -0.0039 0.3132 0.6756 6.000 0.6742 0.01107 0.00441 -0.0035 0.2783 0.6807 6.250 0.6964 0.01159 0.00480 -0.0030 0.2434 0.6863 6.500 0.7177 0.01216 0.00522 -0.0023 0.2077 0.6924 6.750 0.7383 0.01272 0.00566 -0.0015 0.1764 0.6981 7.000 0.7587 0.01325 0.00609 -0.0007 0.1515 0.7042 7.250 0.7795 0.01374 0.00650 0.0000 0.1315 0.7103 7.500 0.7991 0.01421 0.00695 0.0010 0.1140 0.7163 7.750 0.8180 0.01471 0.00739 0.0020 0.0990 0.7230 8.000 0.8365 0.01518 0.00784 0.0031 0.0877 0.7292 8.250 0.8538 0.01565 0.00831 0.0045 0.0787 0.7357 8.500 0.8688 0.01616 0.00881 0.0061 0.0715 0.7429 8.750 0.8814 0.01657 0.00927 0.0082 0.0670 0.7499 9.000 0.8914 0.01715 0.00987 0.0105 0.0631 0.7577 9.250 0.9027 0.01776 0.01053 0.0124 0.0601 0.7650 9.500 0.9154 0.01837 0.01120 0.0140 0.0579 0.7732 9.750 0.9273 0.01906 0.01196 0.0155 0.0559 0.7815 10.000 0.9385 0.01984 0.01278 0.0171 0.0540 0.7906 10.250 0.9482 0.02072 0.01372 0.0186 0.0521 0.7997 10.500 0.9598 0.02156 0.01463 0.0199 0.0509 0.8098 10.750 0.9716 0.02237 0.01554 0.0212 0.0499 0.8204 11.000 0.9827 0.02326 0.01652 0.0224 0.0487 0.8318 11.250 0.9928 0.02422 0.01758 0.0236 0.0476 0.8451 11.500 1.0020 0.02525 0.01869 0.0249 0.0466 0.8609 11.750 1.0101 0.02633 0.01988 0.0262 0.0456 0.8811 12.000 1.0185 0.02752 0.02120 0.0272 0.0446 0.9130 12.250 1.0470 0.02920 0.02299 0.0233 0.0433 0.9655 12.750 1.0686 0.03160 0.02551 0.0245 0.0417 1.0000 13.000 1.0809 0.03279 0.02674 0.0247 0.0403 1.0000 13.250 1.0900 0.03428 0.02826 0.0251 0.0395 1.0000 13.500 1.0993 0.03577 0.02977 0.0253 0.0382 1.0000 13.750 1.1063 0.03749 0.03151 0.0256 0.0372 1.0000 14.000 1.1116 0.03940 0.03344 0.0257 0.0362 1.0000 14.250 1.1223 0.04088 0.03500 0.0258 0.0356 1.0000 14.500 1.1317 0.04252 0.03670 0.0258 0.0349 1.0000 14.750 1.1406 0.04423 0.03847 0.0258 0.0340 1.0000 15.000 1.1481 0.04613 0.04043 0.0256 0.0334 1.0000 15.250 1.1559 0.04803 0.04238 0.0254 0.0326 1.0000 15.500 1.1627 0.05007 0.04446 0.0252 0.0318 1.0000 15.750 1.1681 0.05231 0.04673 0.0248 0.0311 1.0000 16.000 1.1721 0.05474 0.04921 0.0244 0.0302 1.0000 16.250 1.1794 0.05686 0.05140 0.0239 0.0297 1.0000 16.500 1.1853 0.05917 0.05379 0.0234 0.0291 1.0000 16.750 1.1922 0.06139 0.05608 0.0228 0.0282 1.0000 17.000 1.1976 0.06385 0.05860 0.0221 0.0272 1.0000 17.250 1.2011 0.06656 0.06138 0.0213 0.0267 1.0000 17.500 1.2046 0.06935 0.06420 0.0204 0.0258 1.0000 17.750 1.2061 0.07242 0.06733 0.0193 0.0250 1.0000 18.000 1.2100 0.07523 0.07023 0.0183 0.0243 1.0000 18.250 1.2127 0.07824 0.07333 0.0172 0.0235 1.0000 18.500 1.2141 0.08148 0.07665 0.0160 0.0227 1.0000 18.750 1.2147 0.08489 0.08012 0.0145 0.0218 1.0000 19.000 1.2138 0.08857 0.08386 0.0129 0.0210 1.0000 19.250 1.2126 0.09236 0.08774 0.0113 0.0203 1.0000