NASA SC(2)-0612 AIRFOIL (sc20612-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA SC(2)-0612 AIRFOIL (sc20612-il) Reynolds number: 1,000,000 Max Cl/Cd: 79.78 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc20612-il-1000000-n5.txt Download as CSV file: xf-sc20612-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0612 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1290 0.11005 0.10708 -0.0293 1.0000 0.0141
-19.500 -1.1804 0.09663 0.09345 -0.0366 1.0000 0.0140
-19.250 -1.2201 0.08554 0.08217 -0.0428 1.0000 0.0140
-19.000 -1.2492 0.07660 0.07306 -0.0479 1.0000 0.0140
-18.750 -1.2700 0.06932 0.06562 -0.0520 1.0000 0.0140
-18.500 -1.2849 0.06332 0.05949 -0.0553 1.0000 0.0141
-18.250 -1.2949 0.05831 0.05435 -0.0579 1.0000 0.0141
-18.000 -1.3017 0.05401 0.04995 -0.0600 1.0000 0.0142
-17.750 -1.3056 0.05031 0.04615 -0.0616 1.0000 0.0143
-17.500 -1.3071 0.04707 0.04282 -0.0628 1.0000 0.0144
-17.250 -1.3067 0.04424 0.03990 -0.0637 1.0000 0.0145
-17.000 -1.3049 0.04170 0.03728 -0.0643 1.0000 0.0146
-16.750 -1.3018 0.03941 0.03491 -0.0647 1.0000 0.0147
-16.500 -1.2971 0.03735 0.03276 -0.0650 1.0000 0.0149
-16.250 -1.2912 0.03546 0.03080 -0.0651 1.0000 0.0150
-16.000 -1.2842 0.03373 0.02899 -0.0651 1.0000 0.0152
-15.750 -1.2761 0.03214 0.02734 -0.0649 1.0000 0.0153
-15.500 -1.2673 0.03068 0.02581 -0.0647 1.0000 0.0155
-15.250 -1.2581 0.02931 0.02438 -0.0643 1.0000 0.0156
-15.000 -1.2486 0.02805 0.02305 -0.0637 1.0000 0.0158
-14.750 -1.2393 0.02690 0.02185 -0.0628 1.0000 0.0159
-14.500 -1.2316 0.02585 0.02073 -0.0614 1.0000 0.0161
-14.250 -1.2271 0.02491 0.01974 -0.0593 1.0000 0.0162
-14.000 -1.2279 0.02407 0.01886 -0.0560 1.0000 0.0163
-13.750 -1.2208 0.02323 0.01797 -0.0541 1.0000 0.0164
-13.500 -1.2122 0.02230 0.01699 -0.0526 1.0000 0.0166
-13.250 -1.1870 0.02127 0.01591 -0.0542 0.9990 0.0170
-13.000 -1.1594 0.02038 0.01499 -0.0560 0.9978 0.0174
-12.750 -1.1307 0.01961 0.01418 -0.0578 0.9966 0.0178
-12.500 -1.1015 0.01890 0.01344 -0.0596 0.9956 0.0182
-12.250 -1.0714 0.01824 0.01274 -0.0613 0.9947 0.0187
-12.000 -1.0407 0.01762 0.01207 -0.0632 0.9939 0.0191
-11.750 -1.0099 0.01704 0.01145 -0.0649 0.9932 0.0195
-11.500 -0.9809 0.01651 0.01088 -0.0661 0.9917 0.0198
-11.250 -0.9515 0.01589 0.01024 -0.0675 0.9903 0.0204
-11.000 -0.9210 0.01535 0.00968 -0.0690 0.9889 0.0211
-10.750 -0.8897 0.01487 0.00918 -0.0705 0.9876 0.0217
-10.500 -0.8579 0.01442 0.00872 -0.0720 0.9865 0.0224
-10.250 -0.8261 0.01401 0.00828 -0.0735 0.9856 0.0231
-10.000 -0.7940 0.01361 0.00786 -0.0750 0.9849 0.0238
-9.750 -0.7616 0.01317 0.00743 -0.0766 0.9842 0.0250
-9.500 -0.7289 0.01279 0.00704 -0.0782 0.9835 0.0262
-9.250 -0.6961 0.01245 0.00669 -0.0798 0.9829 0.0275
-9.000 -0.6633 0.01208 0.00634 -0.0814 0.9822 0.0293
-8.750 -0.6339 0.01177 0.00603 -0.0821 0.9798 0.0312
-8.500 -0.6029 0.01147 0.00574 -0.0832 0.9778 0.0332
-8.250 -0.5712 0.01117 0.00547 -0.0844 0.9759 0.0359
-8.000 -0.5390 0.01090 0.00520 -0.0856 0.9740 0.0383
-7.750 -0.5066 0.01063 0.00496 -0.0870 0.9723 0.0415
-7.500 -0.4739 0.01041 0.00474 -0.0882 0.9709 0.0437
-7.250 -0.4410 0.01014 0.00449 -0.0896 0.9695 0.0463
-7.000 -0.4110 0.00993 0.00430 -0.0903 0.9665 0.0487
-6.750 -0.3804 0.00975 0.00411 -0.0911 0.9635 0.0506
-6.500 -0.3487 0.00952 0.00389 -0.0921 0.9609 0.0533
-6.250 -0.3169 0.00931 0.00371 -0.0932 0.9587 0.0558
-6.000 -0.2850 0.00913 0.00353 -0.0942 0.9565 0.0582
-5.750 -0.2539 0.00894 0.00336 -0.0950 0.9536 0.0619
-5.500 -0.2232 0.00876 0.00321 -0.0958 0.9500 0.0659
-5.250 -0.1921 0.00859 0.00306 -0.0966 0.9468 0.0707
-5.000 -0.1606 0.00839 0.00291 -0.0975 0.9439 0.0795
-4.500 -0.0976 0.00800 0.00265 -0.0994 0.9375 0.1033
-4.250 -0.0662 0.00782 0.00252 -0.1003 0.9335 0.1187
-4.000 -0.0343 0.00759 0.00239 -0.1013 0.9296 0.1405
-3.750 -0.0021 0.00735 0.00226 -0.1024 0.9250 0.1710
-3.500 0.0304 0.00706 0.00213 -0.1037 0.9179 0.2138
-3.250 0.0635 0.00675 0.00199 -0.1050 0.9113 0.2667
-3.000 0.0969 0.00644 0.00187 -0.1065 0.9047 0.3242
-2.500 0.1635 0.00580 0.00159 -0.1093 0.8775 0.4560
-2.250 0.1961 0.00556 0.00151 -0.1105 0.8547 0.5316
-2.000 0.2261 0.00555 0.00151 -0.1108 0.8318 0.5682
-1.750 0.2546 0.00566 0.00152 -0.1107 0.7958 0.5882
-1.500 0.2822 0.00588 0.00155 -0.1105 0.7445 0.5995
-1.250 0.3094 0.00619 0.00162 -0.1102 0.6792 0.6118
-0.750 0.3598 0.00748 0.00198 -0.1093 0.4397 0.6283
-0.500 0.3868 0.00792 0.00212 -0.1092 0.3627 0.6324
-0.250 0.4142 0.00831 0.00224 -0.1091 0.2974 0.6364
0.000 0.4418 0.00866 0.00237 -0.1091 0.2419 0.6399
0.250 0.4698 0.00894 0.00250 -0.1091 0.2024 0.6428
0.500 0.4978 0.00921 0.00263 -0.1091 0.1664 0.6452
0.750 0.5258 0.00947 0.00276 -0.1091 0.1365 0.6477
1.000 0.5541 0.00969 0.00288 -0.1091 0.1177 0.6499
1.250 0.5825 0.00988 0.00301 -0.1092 0.1032 0.6518
1.500 0.6108 0.01010 0.00314 -0.1092 0.0891 0.6538
1.750 0.6390 0.01030 0.00328 -0.1092 0.0779 0.6560
2.000 0.6672 0.01049 0.00343 -0.1092 0.0698 0.6584
2.250 0.6953 0.01068 0.00359 -0.1091 0.0642 0.6606
2.500 0.7236 0.01085 0.00375 -0.1091 0.0609 0.6626
2.750 0.7518 0.01102 0.00391 -0.1091 0.0580 0.6645
3.000 0.7797 0.01123 0.00408 -0.1090 0.0547 0.6663
3.250 0.8078 0.01141 0.00425 -0.1089 0.0526 0.6681
3.500 0.8358 0.01159 0.00443 -0.1089 0.0507 0.6697
3.750 0.8635 0.01180 0.00461 -0.1087 0.0484 0.6711
4.000 0.8911 0.01201 0.00482 -0.1086 0.0460 0.6731
4.250 0.9189 0.01219 0.00502 -0.1085 0.0440 0.6750
4.500 0.9463 0.01241 0.00523 -0.1083 0.0414 0.6769
4.750 0.9736 0.01264 0.00545 -0.1081 0.0392 0.6790
5.000 1.0008 0.01286 0.00568 -0.1079 0.0368 0.6812
5.250 1.0277 0.01313 0.00592 -0.1076 0.0340 0.6833
5.500 1.0546 0.01338 0.00617 -0.1074 0.0318 0.6853
5.750 1.0811 0.01368 0.00644 -0.1070 0.0295 0.6870
6.000 1.1077 0.01395 0.00672 -0.1067 0.0281 0.6886
6.250 1.1340 0.01424 0.00702 -0.1063 0.0268 0.6906
6.500 1.1600 0.01457 0.00735 -0.1059 0.0254 0.6927
6.750 1.1860 0.01488 0.00769 -0.1055 0.0245 0.6947
7.000 1.2118 0.01519 0.00804 -0.1050 0.0238 0.6966
7.250 1.2374 0.01553 0.00839 -0.1045 0.0230 0.6986
7.500 1.2626 0.01590 0.00877 -0.1040 0.0222 0.7006
7.750 1.2874 0.01631 0.00920 -0.1034 0.0214 0.7026
8.000 1.3123 0.01669 0.00960 -0.1028 0.0208 0.7044
8.250 1.3371 0.01705 0.00999 -0.1022 0.0203 0.7061
8.750 1.3858 0.01784 0.01086 -0.1008 0.0194 0.7098
9.000 1.4095 0.01826 0.01133 -0.1000 0.0189 0.7119
9.250 1.4329 0.01872 0.01182 -0.0992 0.0185 0.7142
9.500 1.4556 0.01923 0.01236 -0.0983 0.0180 0.7166
9.750 1.4774 0.01981 0.01299 -0.0972 0.0176 0.7190
10.000 1.5000 0.02028 0.01351 -0.0962 0.0174 0.7214
10.250 1.5220 0.02076 0.01405 -0.0952 0.0171 0.7236
10.500 1.5435 0.02128 0.01462 -0.0941 0.0169 0.7257
10.750 1.5645 0.02181 0.01521 -0.0929 0.0166 0.7280
11.000 1.5848 0.02236 0.01583 -0.0916 0.0164 0.7303
11.250 1.6045 0.02294 0.01647 -0.0902 0.0161 0.7327
11.500 1.6235 0.02355 0.01714 -0.0887 0.0159 0.7351
11.750 1.6415 0.02418 0.01783 -0.0871 0.0156 0.7376
12.000 1.6581 0.02484 0.01856 -0.0853 0.0154 0.7400
12.250 1.6732 0.02555 0.01932 -0.0832 0.0152 0.7424
12.500 1.6865 0.02631 0.02014 -0.0809 0.0150 0.7445
12.750 1.6953 0.02712 0.02104 -0.0777 0.0148 0.7469
13.000 1.7036 0.02813 0.02213 -0.0748 0.0145 0.7494
13.250 1.7137 0.02906 0.02314 -0.0721 0.0144 0.7520
13.500 1.7242 0.02998 0.02415 -0.0697 0.0143 0.7548
13.750 1.7337 0.03099 0.02526 -0.0673 0.0142 0.7575
14.000 1.7422 0.03210 0.02647 -0.0648 0.0141 0.7600
14.250 1.7499 0.03331 0.02776 -0.0624 0.0140 0.7623
14.500 1.7566 0.03462 0.02917 -0.0601 0.0139 0.7646
14.750 1.7622 0.03605 0.03072 -0.0578 0.0138 0.7671
15.000 1.7666 0.03763 0.03240 -0.0556 0.0137 0.7697
15.250 1.7701 0.03935 0.03423 -0.0535 0.0136 0.7724
15.500 1.7724 0.04124 0.03623 -0.0516 0.0135 0.7751
15.750 1.7732 0.04335 0.03844 -0.0498 0.0134 0.7776
16.000 1.7727 0.04569 0.04090 -0.0482 0.0133 0.7799
16.250 1.7707 0.04831 0.04365 -0.0469 0.0132 0.7823
16.500 1.7666 0.05128 0.04674 -0.0460 0.0131 0.7849
16.750 1.7605 0.05466 0.05026 -0.0454 0.0130 0.7875
17.000 1.7525 0.05851 0.05424 -0.0453 0.0130 0.7901
17.250 1.7415 0.06304 0.05892 -0.0459 0.0129 0.7924
17.500 1.7268 0.06850 0.06454 -0.0474 0.0129 0.7945
17.750 1.7077 0.07522 0.07142 -0.0502 0.0128 0.7963
18.250 1.6394 0.09612 0.09277 -0.0617 0.0128 0.7985
18.500 1.5687 0.11482 0.11178 -0.0730 0.0129 0.7978
18.750 1.4601 0.14186 0.13918 -0.0899 0.0131 0.7953
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