NASA SC(2)-0412 AIRFOIL (sc20412-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA SC(2)-0412 AIRFOIL (sc20412-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.82 at α=7.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc20412-il-1000000.txt Download as CSV file: xf-sc20412-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.1059 0.12730 0.12472 -0.0058 1.0000 0.0172
-19.000 -1.1447 0.11529 0.11253 -0.0127 1.0000 0.0172
-18.750 -1.1776 0.10484 0.10192 -0.0186 1.0000 0.0172
-18.500 -1.2045 0.09572 0.09265 -0.0237 1.0000 0.0172
-18.250 -1.2275 0.08756 0.08433 -0.0284 1.0000 0.0172
-18.000 -1.2454 0.08041 0.07704 -0.0324 1.0000 0.0172
-17.750 -1.2602 0.07405 0.07053 -0.0359 1.0000 0.0173
-17.500 -1.2715 0.06847 0.06482 -0.0389 1.0000 0.0173
-17.250 -1.2798 0.06356 0.05978 -0.0413 1.0000 0.0174
-17.000 -1.2851 0.05932 0.05542 -0.0433 1.0000 0.0174
-16.750 -1.2908 0.05523 0.05121 -0.0449 1.0000 0.0175
-16.500 -1.3034 0.05058 0.04642 -0.0464 1.0000 0.0176
-16.250 -1.3115 0.04674 0.04245 -0.0473 1.0000 0.0178
-16.000 -1.3155 0.04359 0.03921 -0.0478 1.0000 0.0180
-15.750 -1.3157 0.04093 0.03647 -0.0481 1.0000 0.0182
-15.500 -1.3132 0.03861 0.03408 -0.0482 1.0000 0.0183
-15.250 -1.3084 0.03658 0.03197 -0.0482 1.0000 0.0185
-15.000 -1.3016 0.03477 0.03010 -0.0481 1.0000 0.0187
-14.750 -1.2932 0.03315 0.02841 -0.0479 1.0000 0.0189
-14.500 -1.2836 0.03166 0.02686 -0.0476 1.0000 0.0192
-14.250 -1.2729 0.03028 0.02542 -0.0473 1.0000 0.0194
-14.000 -1.2613 0.02900 0.02408 -0.0470 1.0000 0.0197
-13.750 -1.2495 0.02777 0.02277 -0.0465 1.0000 0.0200
-13.500 -1.2372 0.02660 0.02153 -0.0460 1.0000 0.0203
-13.250 -1.2241 0.02553 0.02040 -0.0454 1.0000 0.0205
-13.000 -1.2107 0.02456 0.01936 -0.0447 1.0000 0.0207
-12.750 -1.1993 0.02356 0.01830 -0.0436 1.0000 0.0209
-12.500 -1.1932 0.02209 0.01677 -0.0423 1.0000 0.0215
-12.250 -1.1776 0.02109 0.01574 -0.0420 1.0000 0.0219
-12.000 -1.1590 0.02031 0.01493 -0.0418 1.0000 0.0224
-11.750 -1.1391 0.01962 0.01421 -0.0416 1.0000 0.0229
-11.500 -1.1184 0.01897 0.01352 -0.0415 1.0000 0.0235
-11.250 -1.0968 0.01839 0.01289 -0.0413 1.0000 0.0240
-11.000 -1.0747 0.01788 0.01234 -0.0411 1.0000 0.0245
-10.750 -1.0540 0.01711 0.01153 -0.0408 1.0000 0.0253
-10.500 -1.0320 0.01648 0.01089 -0.0406 1.0000 0.0261
-10.250 -1.0089 0.01604 0.01044 -0.0404 1.0000 0.0270
-10.000 -0.9854 0.01564 0.01002 -0.0401 1.0000 0.0278
-9.750 -0.9617 0.01529 0.00965 -0.0398 1.0000 0.0286
-9.500 -0.9381 0.01476 0.00909 -0.0396 1.0000 0.0298
-9.250 -0.9141 0.01432 0.00866 -0.0395 1.0000 0.0310
-9.000 -0.8899 0.01401 0.00834 -0.0392 1.0000 0.0322
-8.750 -0.8655 0.01372 0.00803 -0.0390 1.0000 0.0332
-8.500 -0.8409 0.01338 0.00767 -0.0388 1.0000 0.0343
-8.250 -0.8116 0.01291 0.00722 -0.0397 0.9996 0.0361
-8.000 -0.7777 0.01260 0.00691 -0.0414 0.9988 0.0377
-7.750 -0.7436 0.01233 0.00663 -0.0430 0.9978 0.0391
-7.500 -0.7092 0.01189 0.00620 -0.0449 0.9968 0.0413
-7.250 -0.6747 0.01160 0.00593 -0.0466 0.9958 0.0435
-7.000 -0.6400 0.01138 0.00570 -0.0483 0.9948 0.0453
-6.750 -0.6047 0.01099 0.00534 -0.0503 0.9940 0.0482
-6.500 -0.5696 0.01073 0.00510 -0.0521 0.9933 0.0510
-6.250 -0.5363 0.01051 0.00488 -0.0534 0.9914 0.0532
-6.000 -0.5014 0.01014 0.00455 -0.0553 0.9897 0.0577
-5.750 -0.4663 0.00991 0.00432 -0.0570 0.9880 0.0609
-5.500 -0.4303 0.00958 0.00404 -0.0590 0.9867 0.0666
-5.250 -0.3944 0.00931 0.00381 -0.0610 0.9855 0.0728
-5.000 -0.3581 0.00904 0.00360 -0.0630 0.9845 0.0815
-4.750 -0.3215 0.00875 0.00338 -0.0651 0.9836 0.0940
-4.500 -0.2850 0.00843 0.00316 -0.0672 0.9825 0.1122
-4.250 -0.2513 0.00809 0.00296 -0.0687 0.9793 0.1397
-4.000 -0.2162 0.00767 0.00274 -0.0707 0.9763 0.1858
-3.750 -0.1802 0.00718 0.00251 -0.0729 0.9734 0.2435
-3.500 -0.1425 0.00656 0.00224 -0.0756 0.9704 0.3353
-3.250 -0.1058 0.00575 0.00193 -0.0783 0.9643 0.4647
-3.000 -0.0714 0.00533 0.00182 -0.0799 0.9574 0.5598
-2.750 -0.0415 0.00526 0.00182 -0.0802 0.9480 0.5910
-2.500 -0.0119 0.00525 0.00181 -0.0803 0.9398 0.6068
-2.250 0.0171 0.00525 0.00182 -0.0803 0.9302 0.6188
-2.000 0.0457 0.00528 0.00181 -0.0802 0.9175 0.6279
-1.750 0.0739 0.00531 0.00181 -0.0799 0.9016 0.6347
-1.500 0.1024 0.00538 0.00180 -0.0798 0.8854 0.6408
-1.250 0.1312 0.00543 0.00183 -0.0797 0.8709 0.6482
-1.000 0.1601 0.00553 0.00188 -0.0796 0.8568 0.6557
-0.750 0.1889 0.00562 0.00190 -0.0795 0.8369 0.6618
-0.500 0.2177 0.00569 0.00194 -0.0795 0.8191 0.6658
-0.250 0.2462 0.00582 0.00199 -0.0793 0.7945 0.6705
0.000 0.2749 0.00598 0.00204 -0.0792 0.7692 0.6751
0.250 0.3039 0.00607 0.00207 -0.0793 0.7443 0.6789
0.500 0.3321 0.00623 0.00212 -0.0791 0.7098 0.6824
0.750 0.3598 0.00648 0.00220 -0.0789 0.6581 0.6855
1.000 0.3860 0.00701 0.00231 -0.0786 0.5509 0.6882
1.250 0.4116 0.00774 0.00251 -0.0783 0.4206 0.6904
1.500 0.4387 0.00827 0.00267 -0.0783 0.3317 0.6920
1.750 0.4660 0.00875 0.00283 -0.0783 0.2568 0.6934
2.000 0.4936 0.00919 0.00299 -0.0784 0.1948 0.6945
2.250 0.5217 0.00946 0.00310 -0.0785 0.1566 0.6966
2.500 0.5499 0.00969 0.00324 -0.0785 0.1327 0.6983
2.750 0.5782 0.00993 0.00338 -0.0786 0.1126 0.6999
3.000 0.6065 0.01016 0.00354 -0.0786 0.0975 0.7015
3.250 0.6347 0.01038 0.00371 -0.0786 0.0852 0.7032
3.500 0.6629 0.01062 0.00389 -0.0786 0.0767 0.7050
3.750 0.6913 0.01081 0.00406 -0.0787 0.0718 0.7068
4.000 0.7193 0.01107 0.00428 -0.0786 0.0660 0.7085
4.250 0.7477 0.01125 0.00446 -0.0787 0.0632 0.7103
4.500 0.7759 0.01147 0.00465 -0.0787 0.0598 0.7119
4.750 0.8037 0.01175 0.00490 -0.0786 0.0561 0.7134
5.000 0.8319 0.01189 0.00507 -0.0786 0.0541 0.7157
5.250 0.8596 0.01210 0.00527 -0.0786 0.0514 0.7175
5.500 0.8869 0.01240 0.00557 -0.0784 0.0484 0.7192
5.750 0.9147 0.01259 0.00578 -0.0783 0.0465 0.7210
6.000 0.9422 0.01284 0.00602 -0.0782 0.0443 0.7228
6.250 0.9689 0.01320 0.00637 -0.0779 0.0418 0.7247
6.500 0.9965 0.01340 0.00660 -0.0778 0.0400 0.7265
6.750 1.0236 0.01367 0.00685 -0.0777 0.0380 0.7283
7.000 1.0500 0.01406 0.00723 -0.0774 0.0359 0.7299
7.250 1.0772 0.01429 0.00748 -0.0772 0.0344 0.7315
7.500 1.1039 0.01456 0.00777 -0.0770 0.0328 0.7340
7.750 1.1292 0.01503 0.00824 -0.0765 0.0311 0.7362
8.000 1.1557 0.01531 0.00857 -0.0762 0.0301 0.7384
8.250 1.1817 0.01563 0.00892 -0.0759 0.0290 0.7406
8.500 1.2073 0.01601 0.00931 -0.0755 0.0279 0.7429
8.750 1.2311 0.01664 0.00996 -0.0748 0.0266 0.7450
9.000 1.2567 0.01699 0.01035 -0.0743 0.0260 0.7470
9.250 1.2819 0.01740 0.01079 -0.0739 0.0253 0.7486
9.500 1.3066 0.01780 0.01124 -0.0733 0.0246 0.7510
9.750 1.3306 0.01827 0.01175 -0.0727 0.0239 0.7534
10.000 1.3530 0.01893 0.01245 -0.0718 0.0231 0.7557
10.250 1.3747 0.01965 0.01323 -0.0708 0.0225 0.7581
10.500 1.3983 0.02011 0.01375 -0.0701 0.0221 0.7606
10.750 1.4210 0.02064 0.01435 -0.0693 0.0216 0.7629
11.000 1.4432 0.02122 0.01498 -0.0684 0.0212 0.7650
11.250 1.4648 0.02180 0.01562 -0.0675 0.0208 0.7675
11.500 1.4857 0.02240 0.01629 -0.0664 0.0204 0.7702
11.750 1.5055 0.02307 0.01703 -0.0652 0.0201 0.7728
12.000 1.5235 0.02390 0.01791 -0.0638 0.0197 0.7754
12.250 1.5376 0.02503 0.01911 -0.0618 0.0193 0.7782
12.500 1.5490 0.02634 0.02054 -0.0595 0.0190 0.7808
12.750 1.5655 0.02708 0.02136 -0.0579 0.0188 0.7834
13.000 1.5796 0.02788 0.02228 -0.0559 0.0187 0.7866
13.250 1.5910 0.02874 0.02324 -0.0535 0.0185 0.7897
13.500 1.5972 0.02969 0.02430 -0.0503 0.0183 0.7929
13.750 1.6046 0.03079 0.02550 -0.0476 0.0182 0.7962
14.000 1.6113 0.03200 0.02681 -0.0451 0.0180 0.7992
14.250 1.6170 0.03333 0.02826 -0.0426 0.0178 0.8029
14.500 1.6216 0.03480 0.02985 -0.0403 0.0177 0.8066
14.750 1.6250 0.03645 0.03162 -0.0382 0.0175 0.8105
15.000 1.6274 0.03829 0.03356 -0.0363 0.0174 0.8142
15.250 1.6283 0.04035 0.03574 -0.0346 0.0173 0.8179
15.500 1.6280 0.04264 0.03815 -0.0332 0.0172 0.8216
15.750 1.6265 0.04520 0.04084 -0.0322 0.0170 0.8255
16.000 1.6238 0.04805 0.04381 -0.0316 0.0169 0.8294
16.250 1.6193 0.05130 0.04718 -0.0313 0.0168 0.8331
16.500 1.6119 0.05512 0.05113 -0.0317 0.0167 0.8369
16.750 1.6026 0.05944 0.05559 -0.0326 0.0166 0.8410
17.000 1.5887 0.06480 0.06110 -0.0344 0.0166 0.8449
17.250 1.5715 0.07117 0.06763 -0.0372 0.0165 0.8484
17.500 1.5493 0.07894 0.07559 -0.0414 0.0165 0.8515
17.750 1.5223 0.08823 0.08507 -0.0468 0.0165 0.8543
18.000 1.4878 0.09930 0.09635 -0.0533 0.0165 0.8564
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