NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63(3)-618 (naca633618-il) Reynolds number: 1,000,000 Max Cl/Cd: 133.17 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca633618-il-1000000.txt Download as CSV file: xf-naca633618-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(3)-618
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9337 0.09845 0.09521 -0.0633 1.0000 0.0152
-19.500 -0.9489 0.09246 0.08912 -0.0665 1.0000 0.0153
-19.250 -0.9621 0.08687 0.08345 -0.0695 1.0000 0.0154
-19.000 -0.9770 0.08114 0.07764 -0.0725 1.0000 0.0155
-18.750 -0.9868 0.07624 0.07265 -0.0751 1.0000 0.0157
-18.500 -0.9958 0.07161 0.06794 -0.0774 1.0000 0.0159
-18.250 -1.0017 0.06751 0.06376 -0.0795 1.0000 0.0160
-18.000 -1.0061 0.06370 0.05987 -0.0813 1.0000 0.0161
-17.750 -1.0082 0.06023 0.05634 -0.0829 1.0000 0.0165
-17.500 -1.0111 0.05681 0.05284 -0.0844 1.0000 0.0166
-17.250 -1.0114 0.05376 0.04972 -0.0857 1.0000 0.0169
-17.000 -1.0112 0.05086 0.04675 -0.0868 1.0000 0.0171
-16.750 -1.0062 0.04859 0.04442 -0.0876 1.0000 0.0174
-16.500 -1.0034 0.04612 0.04187 -0.0884 1.0000 0.0176
-16.250 -1.0032 0.04348 0.03916 -0.0891 1.0000 0.0179
-16.000 -1.0077 0.04047 0.03611 -0.0899 1.0000 0.0184
-15.750 -1.0052 0.03831 0.03391 -0.0902 1.0000 0.0187
-15.500 -1.0017 0.03635 0.03190 -0.0903 1.0000 0.0190
-15.250 -0.9967 0.03459 0.03011 -0.0903 1.0000 0.0194
-15.000 -0.9909 0.03299 0.02847 -0.0900 1.0000 0.0198
-14.750 -0.9846 0.03153 0.02696 -0.0896 1.0000 0.0203
-14.500 -0.9795 0.03010 0.02548 -0.0889 1.0000 0.0206
-14.250 -0.9738 0.02888 0.02422 -0.0878 1.0000 0.0210
-14.000 -0.9561 0.02679 0.02211 -0.0904 0.9899 0.0218
-13.750 -0.9282 0.02549 0.02079 -0.0934 0.9776 0.0227
-13.500 -0.8918 0.02433 0.01958 -0.0975 0.9665 0.0237
-13.250 -0.8482 0.02323 0.01840 -0.1030 0.9576 0.0246
-13.000 -0.8029 0.02174 0.01689 -0.1097 0.9454 0.0261
-12.750 -0.7587 0.02096 0.01602 -0.1147 0.9282 0.0275
-12.500 -0.7300 0.02043 0.01535 -0.1162 0.9060 0.0284
-12.250 -0.7232 0.01930 0.01409 -0.1151 0.8840 0.0292
-12.000 -0.7123 0.01854 0.01327 -0.1139 0.8682 0.0301
-11.750 -0.6989 0.01793 0.01259 -0.1128 0.8554 0.0310
-11.500 -0.6858 0.01734 0.01192 -0.1115 0.8441 0.0318
-11.250 -0.6719 0.01682 0.01132 -0.1102 0.8335 0.0326
-11.000 -0.6616 0.01622 0.01064 -0.1084 0.8239 0.0331
-10.750 -0.6580 0.01546 0.00982 -0.1060 0.8137 0.0341
-10.500 -0.6410 0.01497 0.00929 -0.1051 0.8062 0.0351
-10.250 -0.6206 0.01462 0.00889 -0.1045 0.7986 0.0362
-10.000 -0.5991 0.01432 0.00851 -0.1039 0.7916 0.0372
-9.750 -0.5759 0.01403 0.00818 -0.1036 0.7849 0.0380
-9.500 -0.5564 0.01347 0.00758 -0.1030 0.7781 0.0395
-9.250 -0.5332 0.01312 0.00719 -0.1027 0.7719 0.0407
-9.000 -0.5085 0.01283 0.00687 -0.1025 0.7656 0.0419
-8.750 -0.4832 0.01260 0.00658 -0.1023 0.7592 0.0431
-8.500 -0.4589 0.01222 0.00616 -0.1022 0.7533 0.0448
-8.250 -0.4334 0.01188 0.00582 -0.1022 0.7473 0.0467
-8.000 -0.4072 0.01165 0.00554 -0.1022 0.7412 0.0485
-7.750 -0.3806 0.01142 0.00526 -0.1022 0.7356 0.0504
-7.500 -0.3540 0.01108 0.00493 -0.1024 0.7297 0.0534
-7.250 -0.3269 0.01087 0.00468 -0.1025 0.7240 0.0562
-7.000 -0.2999 0.01058 0.00438 -0.1027 0.7184 0.0611
-6.750 -0.2722 0.01030 0.00412 -0.1029 0.7129 0.0679
-6.500 -0.2448 0.00999 0.00385 -0.1032 0.7071 0.0796
-6.250 -0.2173 0.00969 0.00359 -0.1035 0.7016 0.0977
-6.000 -0.1891 0.00933 0.00334 -0.1040 0.6967 0.1227
-5.750 -0.1609 0.00897 0.00310 -0.1044 0.6910 0.1530
-5.500 -0.1327 0.00862 0.00286 -0.1049 0.6853 0.1886
-5.250 -0.1037 0.00819 0.00261 -0.1056 0.6806 0.2369
-5.000 -0.0745 0.00777 0.00238 -0.1064 0.6754 0.2900
-4.750 -0.0452 0.00743 0.00220 -0.1071 0.6701 0.3422
-4.500 -0.0156 0.00722 0.00210 -0.1077 0.6650 0.3841
-4.250 0.0144 0.00709 0.00203 -0.1082 0.6600 0.4100
-4.000 0.0441 0.00703 0.00197 -0.1086 0.6547 0.4274
-3.750 0.0736 0.00703 0.00193 -0.1090 0.6495 0.4409
-3.500 0.1037 0.00697 0.00190 -0.1095 0.6453 0.4536
-3.250 0.1336 0.00693 0.00188 -0.1099 0.6403 0.4660
-3.000 0.1632 0.00694 0.00186 -0.1103 0.6351 0.4796
-2.750 0.1928 0.00696 0.00186 -0.1106 0.6302 0.4905
-2.500 0.2228 0.00693 0.00185 -0.1111 0.6256 0.4990
-2.250 0.2525 0.00694 0.00185 -0.1114 0.6208 0.5061
-2.000 0.2819 0.00699 0.00184 -0.1117 0.6160 0.5124
-1.750 0.3116 0.00699 0.00186 -0.1121 0.6117 0.5207
-1.500 0.3415 0.00702 0.00186 -0.1125 0.6072 0.5274
-1.250 0.3710 0.00702 0.00187 -0.1129 0.6023 0.5333
-1.000 0.4001 0.00707 0.00189 -0.1131 0.5971 0.5386
-0.750 0.4300 0.00709 0.00190 -0.1136 0.5933 0.5437
-0.500 0.4597 0.00711 0.00191 -0.1139 0.5890 0.5486
-0.250 0.4891 0.00713 0.00194 -0.1143 0.5844 0.5542
0.000 0.5180 0.00721 0.00199 -0.1145 0.5794 0.5595
0.250 0.5478 0.00723 0.00201 -0.1149 0.5756 0.5641
0.500 0.5774 0.00724 0.00204 -0.1153 0.5713 0.5695
0.750 0.6065 0.00729 0.00209 -0.1156 0.5668 0.5744
1.000 0.6352 0.00738 0.00215 -0.1158 0.5618 0.5791
1.250 0.6649 0.00741 0.00218 -0.1162 0.5580 0.5832
1.500 0.6942 0.00743 0.00224 -0.1165 0.5534 0.5889
1.750 0.7229 0.00750 0.00230 -0.1168 0.5485 0.5940
2.000 0.7516 0.00759 0.00237 -0.1170 0.5439 0.5987
2.250 0.7810 0.00762 0.00243 -0.1173 0.5399 0.6032
2.500 0.8100 0.00766 0.00250 -0.1176 0.5353 0.6084
2.750 0.8383 0.00775 0.00258 -0.1178 0.5306 0.6138
3.000 0.8669 0.00784 0.00267 -0.1180 0.5262 0.6189
3.250 0.8960 0.00787 0.00275 -0.1183 0.5220 0.6243
3.500 0.9245 0.00794 0.00284 -0.1185 0.5170 0.6296
3.750 0.9521 0.00808 0.00295 -0.1186 0.5113 0.6350
4.000 0.9809 0.00813 0.00303 -0.1189 0.5062 0.6398
4.250 1.0090 0.00820 0.00314 -0.1190 0.4997 0.6455
4.500 1.0361 0.00834 0.00326 -0.1190 0.4933 0.6514
4.750 1.0647 0.00840 0.00336 -0.1192 0.4879 0.6570
5.000 1.0921 0.00850 0.00349 -0.1192 0.4812 0.6629
5.250 1.1193 0.00862 0.00363 -0.1192 0.4746 0.6688
5.500 1.1467 0.00873 0.00375 -0.1193 0.4667 0.6745
5.750 1.1730 0.00889 0.00390 -0.1191 0.4577 0.6803
6.000 1.1994 0.00902 0.00406 -0.1190 0.4477 0.6866
6.250 1.2252 0.00920 0.00422 -0.1188 0.4358 0.6930
6.500 1.2499 0.00942 0.00442 -0.1184 0.4224 0.6990
6.750 1.2741 0.00966 0.00464 -0.1179 0.4098 0.7053
7.000 1.2987 0.00988 0.00485 -0.1174 0.3968 0.7118
7.250 1.3218 0.01015 0.00510 -0.1168 0.3813 0.7182
7.500 1.3426 0.01052 0.00542 -0.1158 0.3619 0.7250
7.750 1.3613 0.01099 0.00579 -0.1144 0.3365 0.7315
8.000 1.3760 0.01158 0.00626 -0.1124 0.3087 0.7383
8.250 1.3868 0.01224 0.00679 -0.1097 0.2810 0.7458
8.500 1.3946 0.01286 0.00732 -0.1064 0.2559 0.7530
8.750 1.3999 0.01363 0.00798 -0.1028 0.2313 0.7609
9.250 1.4089 0.01536 0.00954 -0.0961 0.1868 0.7775
9.500 1.4135 0.01633 0.01043 -0.0931 0.1670 0.7865
9.750 1.4171 0.01740 0.01145 -0.0901 0.1486 0.7961
10.000 1.4205 0.01858 0.01258 -0.0873 0.1322 0.8059
10.250 1.4233 0.01987 0.01382 -0.0846 0.1167 0.8168
10.500 1.4258 0.02127 0.01518 -0.0822 0.1016 0.8286
10.750 1.4297 0.02265 0.01656 -0.0800 0.0899 0.8419
11.000 1.4332 0.02412 0.01803 -0.0779 0.0792 0.8573
11.250 1.4358 0.02565 0.01958 -0.0758 0.0697 0.8773
11.500 1.4364 0.02717 0.02117 -0.0734 0.0617 0.9126
12.000 1.4433 0.03047 0.02453 -0.0702 0.0491 1.0000
12.250 1.4494 0.03222 0.02628 -0.0692 0.0448 1.0000
12.500 1.4541 0.03414 0.02820 -0.0681 0.0411 1.0000
12.750 1.4621 0.03582 0.02991 -0.0674 0.0389 1.0000
13.000 1.4671 0.03781 0.03192 -0.0666 0.0367 1.0000
13.250 1.4738 0.03973 0.03387 -0.0660 0.0351 1.0000
13.500 1.4814 0.04159 0.03577 -0.0654 0.0337 1.0000
13.750 1.4866 0.04374 0.03795 -0.0649 0.0323 1.0000
14.000 1.4900 0.04613 0.04037 -0.0644 0.0309 1.0000
14.250 1.4984 0.04805 0.04235 -0.0642 0.0301 1.0000
14.500 1.5052 0.05019 0.04454 -0.0640 0.0293 1.0000
14.750 1.5110 0.05246 0.04685 -0.0638 0.0283 1.0000
15.000 1.5145 0.05504 0.04947 -0.0637 0.0275 1.0000
15.250 1.5160 0.05793 0.05240 -0.0636 0.0265 1.0000
15.500 1.5235 0.06015 0.05469 -0.0637 0.0259 1.0000
15.750 1.5294 0.06260 0.05720 -0.0638 0.0252 1.0000
16.000 1.5343 0.06519 0.05984 -0.0640 0.0245 1.0000
16.250 1.5369 0.06813 0.06283 -0.0643 0.0238 1.0000
16.500 1.5369 0.07146 0.06621 -0.0647 0.0230 1.0000
16.750 1.5404 0.07438 0.06920 -0.0651 0.0224 1.0000
17.000 1.5458 0.07708 0.07197 -0.0656 0.0218 1.0000
17.250 1.5495 0.08004 0.07498 -0.0661 0.0211 1.0000
17.500 1.5513 0.08331 0.07831 -0.0668 0.0204 1.0000
17.750 1.5504 0.08701 0.08206 -0.0676 0.0197 1.0000
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