NASA SC(2)-0412 AIRFOIL (sc20412-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA SC(2)-0412 AIRFOIL (sc20412-il) Reynolds number: 1,000,000 Max Cl/Cd: 78.16 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc20412-il-1000000-n5.txt Download as CSV file: xf-sc20412-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0412 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 -1.1477 0.12904 0.12627 -0.0043 1.0000 0.0136
-19.500 -1.2094 0.11306 0.11008 -0.0133 1.0000 0.0135
-19.250 -1.2648 0.09872 0.09552 -0.0212 1.0000 0.0134
-19.000 -1.3053 0.08743 0.08403 -0.0274 1.0000 0.0134
-18.750 -1.3333 0.07863 0.07505 -0.0323 1.0000 0.0134
-18.500 -1.3533 0.07152 0.06780 -0.0362 1.0000 0.0135
-18.250 -1.3673 0.06564 0.06177 -0.0393 1.0000 0.0135
-18.000 -1.3771 0.06070 0.05671 -0.0416 1.0000 0.0136
-17.750 -1.3839 0.05639 0.05228 -0.0435 1.0000 0.0136
-17.500 -1.3878 0.05268 0.04846 -0.0449 1.0000 0.0137
-17.250 -1.3901 0.04935 0.04503 -0.0460 1.0000 0.0138
-17.000 -1.3903 0.04641 0.04199 -0.0467 1.0000 0.0139
-16.750 -1.3893 0.04378 0.03926 -0.0472 1.0000 0.0140
-16.500 -1.3868 0.04139 0.03679 -0.0475 1.0000 0.0141
-16.250 -1.3826 0.03925 0.03455 -0.0476 1.0000 0.0142
-16.000 -1.3770 0.03730 0.03252 -0.0476 1.0000 0.0143
-15.750 -1.3696 0.03554 0.03068 -0.0476 1.0000 0.0144
-15.500 -1.3637 0.03368 0.02874 -0.0474 1.0000 0.0145
-15.250 -1.3570 0.03191 0.02691 -0.0472 1.0000 0.0148
-15.000 -1.3482 0.03038 0.02531 -0.0469 1.0000 0.0150
-14.750 -1.3379 0.02899 0.02386 -0.0465 1.0000 0.0152
-14.500 -1.3264 0.02773 0.02255 -0.0461 1.0000 0.0154
-14.250 -1.3139 0.02656 0.02134 -0.0457 1.0000 0.0157
-14.000 -1.3010 0.02547 0.02020 -0.0452 1.0000 0.0159
-13.750 -1.2875 0.02447 0.01914 -0.0446 1.0000 0.0161
-13.500 -1.2742 0.02352 0.01814 -0.0438 1.0000 0.0164
-13.250 -1.2616 0.02264 0.01721 -0.0428 1.0000 0.0166
-13.000 -1.2468 0.02181 0.01633 -0.0421 1.0000 0.0169
-12.750 -1.2289 0.02103 0.01550 -0.0419 1.0000 0.0171
-12.500 -1.2097 0.02030 0.01472 -0.0417 1.0000 0.0174
-12.250 -1.1903 0.01952 0.01390 -0.0417 1.0000 0.0178
-12.000 -1.1698 0.01881 0.01317 -0.0416 1.0000 0.0182
-11.750 -1.1484 0.01818 0.01251 -0.0416 1.0000 0.0187
-11.500 -1.1263 0.01761 0.01193 -0.0415 1.0000 0.0192
-11.250 -1.1038 0.01710 0.01138 -0.0413 1.0000 0.0198
-11.000 -1.0809 0.01662 0.01088 -0.0411 1.0000 0.0203
-10.750 -1.0577 0.01618 0.01040 -0.0409 1.0000 0.0207
-10.500 -1.0343 0.01571 0.00991 -0.0407 1.0000 0.0214
-10.250 -1.0107 0.01527 0.00947 -0.0406 1.0000 0.0222
-10.000 -0.9851 0.01486 0.00905 -0.0407 0.9998 0.0230
-9.750 -0.9538 0.01446 0.00864 -0.0420 0.9989 0.0240
-9.500 -0.9224 0.01408 0.00823 -0.0433 0.9979 0.0248
-9.250 -0.8909 0.01365 0.00782 -0.0446 0.9967 0.0260
-9.000 -0.8588 0.01328 0.00745 -0.0460 0.9956 0.0271
-8.750 -0.8262 0.01294 0.00709 -0.0474 0.9944 0.0283
-8.500 -0.7933 0.01261 0.00675 -0.0489 0.9935 0.0292
-8.250 -0.7619 0.01226 0.00641 -0.0501 0.9916 0.0307
-8.000 -0.7301 0.01194 0.00610 -0.0513 0.9897 0.0321
-7.750 -0.6979 0.01166 0.00581 -0.0525 0.9880 0.0334
-7.500 -0.6653 0.01136 0.00552 -0.0539 0.9864 0.0351
-7.250 -0.6324 0.01106 0.00525 -0.0553 0.9849 0.0371
-7.000 -0.5994 0.01081 0.00499 -0.0566 0.9834 0.0388
-6.750 -0.5666 0.01054 0.00474 -0.0580 0.9816 0.0409
-6.500 -0.5356 0.01028 0.00451 -0.0589 0.9781 0.0434
-6.250 -0.5035 0.01007 0.00430 -0.0600 0.9751 0.0455
-6.000 -0.4706 0.00981 0.00407 -0.0613 0.9723 0.0487
-5.750 -0.4377 0.00959 0.00386 -0.0625 0.9691 0.0516
-5.500 -0.4070 0.00938 0.00367 -0.0633 0.9632 0.0547
-5.250 -0.3753 0.00916 0.00348 -0.0642 0.9578 0.0588
-5.000 -0.3445 0.00899 0.00331 -0.0649 0.9523 0.0621
-4.750 -0.3138 0.00878 0.00314 -0.0656 0.9458 0.0678
-4.500 -0.2831 0.00858 0.00298 -0.0664 0.9398 0.0762
-4.250 -0.2527 0.00840 0.00283 -0.0670 0.9331 0.0849
-4.000 -0.2223 0.00824 0.00270 -0.0676 0.9268 0.0946
-3.750 -0.1917 0.00805 0.00256 -0.0682 0.9196 0.1075
-3.250 -0.1305 0.00762 0.00229 -0.0696 0.8995 0.1541
-3.000 -0.0995 0.00738 0.00215 -0.0705 0.8882 0.1894
-2.500 -0.0355 0.00678 0.00187 -0.0727 0.8655 0.2910
-2.250 -0.0023 0.00640 0.00172 -0.0742 0.8564 0.3637
-2.000 0.0320 0.00592 0.00153 -0.0761 0.8405 0.4626
-1.750 0.0644 0.00567 0.00145 -0.0772 0.8159 0.5396
-1.500 0.0942 0.00568 0.00144 -0.0775 0.7880 0.5681
-1.250 0.1240 0.00572 0.00146 -0.0778 0.7650 0.5945
-1.000 0.1535 0.00580 0.00148 -0.0780 0.7407 0.6109
-0.750 0.1822 0.00598 0.00152 -0.0780 0.6983 0.6231
-0.500 0.2107 0.00619 0.00155 -0.0781 0.6459 0.6291
-0.250 0.2373 0.00675 0.00167 -0.0779 0.5294 0.6366
0.000 0.2638 0.00744 0.00184 -0.0778 0.3981 0.6434
0.250 0.2921 0.00776 0.00196 -0.0779 0.3385 0.6482
0.500 0.3204 0.00808 0.00208 -0.0780 0.2820 0.6524
0.750 0.3487 0.00841 0.00219 -0.0782 0.2287 0.6561
1.000 0.3773 0.00869 0.00229 -0.0783 0.1903 0.6588
1.250 0.4058 0.00893 0.00240 -0.0784 0.1587 0.6610
1.500 0.4347 0.00910 0.00250 -0.0786 0.1406 0.6627
1.750 0.4635 0.00928 0.00261 -0.0787 0.1233 0.6642
2.000 0.4922 0.00946 0.00273 -0.0788 0.1089 0.6658
2.250 0.5210 0.00963 0.00285 -0.0789 0.0979 0.6674
2.500 0.5497 0.00982 0.00297 -0.0790 0.0862 0.6690
2.750 0.5782 0.01001 0.00310 -0.0791 0.0768 0.6707
3.000 0.6069 0.01018 0.00324 -0.0792 0.0704 0.6724
3.250 0.6354 0.01037 0.00339 -0.0793 0.0646 0.6740
3.500 0.6640 0.01054 0.00354 -0.0793 0.0609 0.6755
3.750 0.6923 0.01074 0.00370 -0.0794 0.0568 0.6770
4.000 0.7208 0.01090 0.00387 -0.0794 0.0541 0.6790
4.250 0.7490 0.01109 0.00404 -0.0794 0.0512 0.6808
4.500 0.7771 0.01130 0.00424 -0.0794 0.0485 0.6825
4.750 0.8053 0.01148 0.00443 -0.0794 0.0465 0.6842
5.000 0.8333 0.01169 0.00463 -0.0793 0.0441 0.6859
5.250 0.8611 0.01192 0.00485 -0.0793 0.0418 0.6876
5.500 0.8890 0.01212 0.00505 -0.0792 0.0400 0.6893
5.750 0.9166 0.01235 0.00527 -0.0791 0.0379 0.6909
6.000 0.9441 0.01260 0.00551 -0.0790 0.0360 0.6924
6.250 0.9716 0.01283 0.00575 -0.0789 0.0345 0.6938
6.500 0.9989 0.01308 0.00600 -0.0787 0.0326 0.6953
6.750 1.0259 0.01336 0.00627 -0.0786 0.0309 0.6971
7.000 1.0530 0.01361 0.00655 -0.0784 0.0294 0.6991
7.250 1.0797 0.01390 0.00685 -0.0781 0.0277 0.7011
7.500 1.1062 0.01422 0.00717 -0.0779 0.0264 0.7032
7.750 1.1328 0.01451 0.00749 -0.0776 0.0254 0.7054
8.000 1.1591 0.01483 0.00783 -0.0773 0.0243 0.7075
8.250 1.1850 0.01519 0.00819 -0.0769 0.0233 0.7094
8.500 1.2107 0.01557 0.00858 -0.0765 0.0225 0.7111
8.750 1.2365 0.01591 0.00895 -0.0762 0.0219 0.7125
9.000 1.2620 0.01626 0.00934 -0.0757 0.0212 0.7145
9.250 1.2872 0.01665 0.00976 -0.0753 0.0205 0.7165
9.500 1.3120 0.01706 0.01021 -0.0748 0.0199 0.7188
9.750 1.3363 0.01753 0.01071 -0.0742 0.0193 0.7211
10.000 1.3605 0.01799 0.01120 -0.0736 0.0189 0.7233
10.250 1.3848 0.01841 0.01168 -0.0730 0.0185 0.7255
10.500 1.4086 0.01885 0.01217 -0.0723 0.0181 0.7276
10.750 1.4321 0.01932 0.01268 -0.0716 0.0177 0.7295
11.250 1.4778 0.02032 0.01377 -0.0700 0.0168 0.7335
11.500 1.4997 0.02088 0.01438 -0.0691 0.0165 0.7359
11.750 1.5208 0.02150 0.01505 -0.0681 0.0161 0.7383
12.000 1.5407 0.02220 0.01581 -0.0669 0.0158 0.7407
12.250 1.5613 0.02279 0.01647 -0.0658 0.0156 0.7432
12.500 1.5812 0.02340 0.01715 -0.0646 0.0155 0.7457
12.750 1.6002 0.02405 0.01787 -0.0633 0.0153 0.7479
13.000 1.6183 0.02472 0.01862 -0.0619 0.0151 0.7503
13.250 1.6354 0.02543 0.01941 -0.0604 0.0149 0.7529
13.500 1.6511 0.02617 0.02024 -0.0586 0.0147 0.7557
13.750 1.6648 0.02695 0.02109 -0.0566 0.0146 0.7587
14.000 1.6754 0.02775 0.02198 -0.0540 0.0144 0.7618
14.250 1.6836 0.02863 0.02293 -0.0512 0.0143 0.7648
14.500 1.6924 0.02961 0.02400 -0.0486 0.0141 0.7677
14.750 1.7004 0.03069 0.02518 -0.0462 0.0140 0.7710
15.000 1.7077 0.03189 0.02647 -0.0439 0.0138 0.7743
15.250 1.7136 0.03323 0.02790 -0.0416 0.0137 0.7776
15.500 1.7184 0.03472 0.02949 -0.0395 0.0136 0.7806
15.750 1.7216 0.03641 0.03128 -0.0375 0.0135 0.7836
16.000 1.7232 0.03834 0.03332 -0.0357 0.0134 0.7869
16.250 1.7223 0.04058 0.03569 -0.0341 0.0132 0.7906
16.500 1.7193 0.04320 0.03842 -0.0328 0.0131 0.7943
16.750 1.7136 0.04626 0.04161 -0.0319 0.0130 0.7979
17.000 1.7053 0.04982 0.04532 -0.0315 0.0129 0.8014
17.250 1.6965 0.05373 0.04938 -0.0316 0.0129 0.8052
17.500 1.6861 0.05811 0.05391 -0.0324 0.0129 0.8090
17.750 1.6727 0.06328 0.05923 -0.0340 0.0128 0.8123
18.000 1.6529 0.06997 0.06610 -0.0369 0.0128 0.8150
18.250 1.6249 0.07877 0.07510 -0.0417 0.0128 0.8172
18.500 1.5772 0.09229 0.08888 -0.0498 0.0129 0.8182
18.750 1.4947 0.11308 0.11000 -0.0620 0.0129 0.8169
19.000 1.4090 0.13471 0.13192 -0.0748 0.0131 0.8151
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