NASA SC(2)-0414 AIRFOIL (sc20414-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA SC(2)-0414 AIRFOIL (sc20414-il) Reynolds number: 500,000 Max Cl/Cd: 63.37 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc20414-il-500000-n5.txt Download as CSV file: xf-sc20414-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0414 AIRFOIL
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 -1.1232 0.12246 0.11854 -0.0177 1.0000 0.0232
-19.500 -1.1430 0.11474 0.11071 -0.0220 1.0000 0.0233
-19.250 -1.1620 0.10738 0.10322 -0.0260 1.0000 0.0234
-19.000 -1.1793 0.10037 0.09609 -0.0298 1.0000 0.0235
-18.750 -1.1950 0.09379 0.08939 -0.0333 1.0000 0.0237
-18.500 -1.2086 0.08770 0.08317 -0.0365 1.0000 0.0238
-18.250 -1.2196 0.08212 0.07748 -0.0394 1.0000 0.0239
-18.000 -1.2284 0.07702 0.07227 -0.0419 1.0000 0.0241
-17.750 -1.2352 0.07238 0.06750 -0.0441 1.0000 0.0242
-17.500 -1.2400 0.06813 0.06315 -0.0460 1.0000 0.0244
-17.250 -1.2430 0.06429 0.05921 -0.0476 1.0000 0.0246
-17.000 -1.2446 0.06078 0.05559 -0.0489 1.0000 0.0249
-16.750 -1.2447 0.05754 0.05225 -0.0501 1.0000 0.0251
-16.500 -1.2435 0.05456 0.04918 -0.0510 1.0000 0.0253
-16.250 -1.2412 0.05182 0.04633 -0.0517 1.0000 0.0256
-16.000 -1.2377 0.04930 0.04372 -0.0522 1.0000 0.0259
-15.750 -1.2326 0.04702 0.04134 -0.0526 1.0000 0.0261
-15.500 -1.2266 0.04491 0.03913 -0.0528 1.0000 0.0264
-15.250 -1.2215 0.04278 0.03693 -0.0530 1.0000 0.0267
-15.000 -1.2163 0.04076 0.03486 -0.0530 1.0000 0.0271
-14.750 -1.2093 0.03896 0.03300 -0.0529 1.0000 0.0275
-14.500 -1.2008 0.03733 0.03133 -0.0528 1.0000 0.0278
-14.250 -1.1910 0.03585 0.02979 -0.0526 1.0000 0.0283
-14.000 -1.1808 0.03443 0.02832 -0.0523 1.0000 0.0287
-13.750 -1.1697 0.03311 0.02694 -0.0519 1.0000 0.0291
-13.500 -1.1582 0.03185 0.02561 -0.0515 1.0000 0.0295
-13.250 -1.1461 0.03067 0.02437 -0.0510 1.0000 0.0300
-13.000 -1.1333 0.02956 0.02320 -0.0505 1.0000 0.0304
-12.750 -1.1212 0.02843 0.02202 -0.0499 1.0000 0.0309
-12.500 -1.1093 0.02733 0.02090 -0.0492 1.0000 0.0314
-12.250 -1.0966 0.02635 0.01989 -0.0484 1.0000 0.0320
-12.000 -1.0835 0.02547 0.01899 -0.0475 1.0000 0.0326
-11.750 -1.0711 0.02465 0.01814 -0.0463 1.0000 0.0333
-11.500 -1.0604 0.02390 0.01736 -0.0447 1.0000 0.0340
-11.250 -1.0538 0.02321 0.01663 -0.0422 1.0000 0.0346
-11.000 -1.0467 0.02256 0.01594 -0.0397 1.0000 0.0351
-10.750 -1.0376 0.02179 0.01516 -0.0379 1.0000 0.0358
-10.500 -1.0258 0.02110 0.01447 -0.0363 1.0000 0.0366
-10.250 -1.0121 0.02047 0.01383 -0.0351 1.0000 0.0374
-10.000 -0.9827 0.01981 0.01314 -0.0366 0.9983 0.0385
-9.750 -0.9516 0.01919 0.01248 -0.0384 0.9962 0.0397
-9.500 -0.9198 0.01853 0.01180 -0.0404 0.9942 0.0410
-9.250 -0.8874 0.01792 0.01121 -0.0425 0.9925 0.0426
-9.000 -0.8566 0.01739 0.01066 -0.0440 0.9898 0.0443
-8.750 -0.8246 0.01691 0.01014 -0.0457 0.9873 0.0458
-8.500 -0.7917 0.01633 0.00959 -0.0477 0.9850 0.0475
-8.250 -0.7577 0.01586 0.00911 -0.0497 0.9831 0.0495
-8.000 -0.7231 0.01544 0.00867 -0.0517 0.9816 0.0516
-7.750 -0.6908 0.01497 0.00822 -0.0533 0.9791 0.0539
-7.500 -0.6596 0.01457 0.00784 -0.0546 0.9755 0.0564
-7.250 -0.6269 0.01422 0.00746 -0.0561 0.9726 0.0587
-7.000 -0.5933 0.01378 0.00706 -0.0578 0.9700 0.0617
-6.500 -0.5288 0.01306 0.00637 -0.0606 0.9622 0.0688
-6.250 -0.4963 0.01273 0.00606 -0.0619 0.9581 0.0733
-6.000 -0.4627 0.01238 0.00574 -0.0635 0.9548 0.0785
-5.750 -0.4311 0.01209 0.00548 -0.0646 0.9503 0.0843
-5.500 -0.3994 0.01176 0.00520 -0.0657 0.9452 0.0917
-5.250 -0.3669 0.01145 0.00493 -0.0670 0.9408 0.0999
-5.000 -0.3350 0.01117 0.00468 -0.0681 0.9358 0.1092
-4.750 -0.3036 0.01085 0.00445 -0.0692 0.9297 0.1225
-4.500 -0.2715 0.01056 0.00421 -0.0703 0.9245 0.1392
-4.250 -0.2395 0.01023 0.00398 -0.0715 0.9193 0.1591
-4.000 -0.2072 0.00986 0.00375 -0.0729 0.9132 0.1903
-3.500 -0.1394 0.00892 0.00323 -0.0765 0.9021 0.2915
-3.250 -0.1027 0.00825 0.00291 -0.0792 0.8963 0.3788
-3.000 -0.0641 0.00753 0.00264 -0.0824 0.8909 0.4890
-2.750 -0.0313 0.00735 0.00264 -0.0834 0.8841 0.5440
-2.500 -0.0004 0.00733 0.00265 -0.0839 0.8764 0.5678
-2.250 0.0301 0.00734 0.00266 -0.0843 0.8693 0.5834
-2.000 0.0603 0.00735 0.00268 -0.0846 0.8597 0.5966
-1.750 0.0902 0.00740 0.00267 -0.0847 0.8468 0.6087
-1.500 0.1192 0.00747 0.00271 -0.0846 0.8315 0.6169
-1.250 0.1488 0.00755 0.00271 -0.0847 0.8139 0.6261
-1.000 0.1773 0.00766 0.00279 -0.0844 0.7930 0.6341
-0.750 0.2065 0.00779 0.00282 -0.0844 0.7691 0.6417
-0.500 0.2360 0.00789 0.00282 -0.0845 0.7477 0.6463
-0.250 0.2645 0.00800 0.00288 -0.0844 0.7247 0.6498
0.000 0.2933 0.00813 0.00293 -0.0843 0.6985 0.6532
0.250 0.3220 0.00829 0.00296 -0.0843 0.6658 0.6561
0.500 0.3499 0.00853 0.00298 -0.0842 0.6126 0.6582
0.750 0.3753 0.00910 0.00308 -0.0837 0.5093 0.6602
1.000 0.4008 0.00977 0.00327 -0.0834 0.4045 0.6622
1.250 0.4272 0.01031 0.00346 -0.0833 0.3269 0.6638
1.500 0.4541 0.01073 0.00363 -0.0832 0.2668 0.6653
1.750 0.4814 0.01111 0.00381 -0.0831 0.2186 0.6668
2.000 0.5091 0.01143 0.00398 -0.0831 0.1854 0.6683
2.250 0.5370 0.01172 0.00415 -0.0831 0.1594 0.6698
2.750 0.5933 0.01223 0.00448 -0.0832 0.1255 0.6731
3.000 0.6216 0.01247 0.00465 -0.0832 0.1135 0.6749
3.250 0.6500 0.01268 0.00483 -0.0833 0.1043 0.6766
3.500 0.6782 0.01292 0.00501 -0.0833 0.0962 0.6784
3.750 0.7063 0.01317 0.00520 -0.0834 0.0893 0.6804
4.000 0.7343 0.01339 0.00541 -0.0833 0.0844 0.6823
4.250 0.7617 0.01365 0.00565 -0.0832 0.0795 0.6841
4.500 0.7894 0.01388 0.00589 -0.0831 0.0755 0.6858
4.750 0.8169 0.01413 0.00613 -0.0829 0.0713 0.6874
5.000 0.8442 0.01439 0.00639 -0.0828 0.0677 0.6890
5.250 0.8716 0.01465 0.00664 -0.0826 0.0644 0.6907
5.500 0.8985 0.01495 0.00691 -0.0824 0.0612 0.6925
5.750 0.9258 0.01521 0.00718 -0.0823 0.0585 0.6944
6.000 0.9527 0.01551 0.00746 -0.0821 0.0558 0.6962
6.250 0.9792 0.01584 0.00778 -0.0818 0.0536 0.6981
6.500 1.0060 0.01614 0.00810 -0.0816 0.0516 0.7000
6.750 1.0321 0.01646 0.00843 -0.0812 0.0497 0.7017
7.000 1.0575 0.01684 0.00882 -0.0808 0.0478 0.7034
7.250 1.0833 0.01716 0.00918 -0.0804 0.0462 0.7051
7.500 1.1089 0.01750 0.00955 -0.0799 0.0445 0.7068
7.750 1.1339 0.01790 0.00995 -0.0794 0.0430 0.7086
8.000 1.1584 0.01834 0.01040 -0.0788 0.0418 0.7104
8.250 1.1833 0.01872 0.01083 -0.0783 0.0406 0.7123
8.500 1.2078 0.01912 0.01127 -0.0777 0.0394 0.7143
8.750 1.2319 0.01956 0.01173 -0.0771 0.0383 0.7162
9.000 1.2552 0.02006 0.01223 -0.0764 0.0372 0.7180
9.250 1.2785 0.02053 0.01273 -0.0756 0.0362 0.7198
9.500 1.3015 0.02097 0.01325 -0.0748 0.0352 0.7217
9.750 1.3238 0.02145 0.01379 -0.0739 0.0344 0.7237
10.000 1.3455 0.02197 0.01435 -0.0729 0.0336 0.7258
10.250 1.3664 0.02254 0.01495 -0.0718 0.0328 0.7278
10.500 1.3860 0.02319 0.01563 -0.0705 0.0322 0.7299
10.750 1.4062 0.02376 0.01628 -0.0693 0.0316 0.7320
11.000 1.4254 0.02436 0.01695 -0.0680 0.0310 0.7341
11.250 1.4437 0.02499 0.01764 -0.0665 0.0304 0.7362
11.500 1.4609 0.02562 0.01833 -0.0649 0.0298 0.7381
11.750 1.4755 0.02626 0.01903 -0.0629 0.0292 0.7400
12.000 1.4873 0.02697 0.01980 -0.0604 0.0288 0.7420
12.250 1.4997 0.02782 0.02071 -0.0582 0.0283 0.7441
12.500 1.5112 0.02878 0.02174 -0.0561 0.0279 0.7463
12.750 1.5239 0.02968 0.02274 -0.0542 0.0275 0.7486
13.000 1.5358 0.03066 0.02382 -0.0523 0.0272 0.7509
13.250 1.5469 0.03173 0.02498 -0.0504 0.0268 0.7533
13.500 1.5571 0.03289 0.02622 -0.0486 0.0265 0.7558
13.750 1.5665 0.03411 0.02755 -0.0468 0.0261 0.7583
14.000 1.5750 0.03543 0.02898 -0.0450 0.0258 0.7608
14.250 1.5827 0.03686 0.03052 -0.0434 0.0255 0.7634
14.500 1.5894 0.03844 0.03219 -0.0419 0.0253 0.7660
14.750 1.5949 0.04018 0.03402 -0.0405 0.0250 0.7684
15.000 1.5989 0.04212 0.03605 -0.0392 0.0248 0.7707
15.250 1.6009 0.04433 0.03835 -0.0380 0.0245 0.7729
15.500 1.6008 0.04683 0.04095 -0.0371 0.0243 0.7749
15.750 1.5980 0.04971 0.04394 -0.0363 0.0241 0.7769
16.000 1.5978 0.05247 0.04685 -0.0359 0.0239 0.7791
16.250 1.5956 0.05557 0.05011 -0.0357 0.0238 0.7814
16.500 1.5918 0.05901 0.05369 -0.0359 0.0236 0.7836
16.750 1.5857 0.06291 0.05775 -0.0365 0.0234 0.7859
17.000 1.5782 0.06728 0.06227 -0.0376 0.0232 0.7880
17.250 1.5681 0.07226 0.06740 -0.0392 0.0231 0.7900
17.500 1.5548 0.07802 0.07334 -0.0416 0.0229 0.7917
17.750 1.5391 0.08455 0.08005 -0.0447 0.0228 0.7933
18.000 1.5193 0.09207 0.08775 -0.0486 0.0227 0.7949
18.250 1.4956 0.10056 0.09644 -0.0532 0.0226 0.7963
18.500 1.4676 0.11009 0.10616 -0.0586 0.0226 0.7975
18.750 1.4360 0.12046 0.11672 -0.0647 0.0225 0.7984
19.000 1.4023 0.13150 0.12795 -0.0715 0.0225 0.7992
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