SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il) Reynolds number: 500,000 Max Cl/Cd: 65.95 at α=0.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-nasasc2-0714-il-500000.txt Download as CSV file: xf-nasasc2-0714-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: SC(2)-0714 Supercritical airfoil (coordinates fr
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.9645 0.09555 0.09181 -0.0618 1.0000 0.0307
-18.250 -0.9992 0.08559 0.08162 -0.0678 1.0000 0.0307
-18.000 -1.0245 0.07796 0.07380 -0.0720 1.0000 0.0309
-17.750 -1.0403 0.07229 0.06799 -0.0747 1.0000 0.0311
-17.500 -1.0485 0.06797 0.06359 -0.0765 1.0000 0.0313
-17.250 -1.0539 0.06424 0.05977 -0.0779 1.0000 0.0315
-17.000 -1.0576 0.06094 0.05639 -0.0790 1.0000 0.0317
-16.750 -1.0605 0.05792 0.05330 -0.0798 1.0000 0.0320
-16.500 -1.0635 0.05509 0.05039 -0.0802 1.0000 0.0322
-16.250 -1.0665 0.05246 0.04767 -0.0803 1.0000 0.0325
-16.000 -1.0696 0.04998 0.04510 -0.0802 1.0000 0.0328
-15.750 -1.0729 0.04770 0.04271 -0.0796 1.0000 0.0330
-15.500 -1.0760 0.04558 0.04050 -0.0787 1.0000 0.0333
-15.250 -1.0784 0.04370 0.03852 -0.0775 1.0000 0.0337
-15.000 -1.0806 0.04198 0.03670 -0.0759 1.0000 0.0340
-14.750 -1.0831 0.04039 0.03502 -0.0740 1.0000 0.0343
-14.500 -1.0856 0.03894 0.03347 -0.0719 1.0000 0.0347
-14.250 -1.0881 0.03762 0.03205 -0.0695 1.0000 0.0350
-14.000 -1.0911 0.03643 0.03077 -0.0668 1.0000 0.0353
-13.750 -1.0945 0.03537 0.02962 -0.0639 1.0000 0.0355
-13.500 -1.0961 0.03391 0.02808 -0.0609 1.0000 0.0360
-13.250 -1.0966 0.03281 0.02695 -0.0578 1.0000 0.0364
-13.000 -1.1004 0.03196 0.02608 -0.0541 1.0000 0.0368
-12.750 -1.1081 0.03120 0.02531 -0.0498 1.0000 0.0371
-12.500 -1.1067 0.03038 0.02446 -0.0470 1.0000 0.0375
-12.250 -1.0990 0.02953 0.02357 -0.0454 0.9999 0.0380
-12.000 -1.0733 0.02856 0.02255 -0.0470 0.9985 0.0388
-11.750 -1.0465 0.02763 0.02154 -0.0486 0.9968 0.0397
-11.500 -1.0175 0.02680 0.02062 -0.0506 0.9952 0.0406
-11.250 -0.9881 0.02593 0.01965 -0.0524 0.9938 0.0415
-11.000 -0.9614 0.02487 0.01862 -0.0536 0.9929 0.0428
-10.750 -0.9366 0.02414 0.01789 -0.0544 0.9907 0.0438
-10.500 -0.9091 0.02346 0.01719 -0.0557 0.9887 0.0449
-10.250 -0.8802 0.02282 0.01650 -0.0571 0.9870 0.0461
-10.000 -0.8494 0.02226 0.01588 -0.0588 0.9855 0.0472
-9.750 -0.8197 0.02143 0.01502 -0.0603 0.9842 0.0486
-9.500 -0.7873 0.02072 0.01435 -0.0624 0.9830 0.0502
-9.250 -0.7533 0.02020 0.01382 -0.0646 0.9821 0.0518
-9.000 -0.7192 0.01972 0.01332 -0.0669 0.9814 0.0534
-8.750 -0.6925 0.01930 0.01285 -0.0675 0.9789 0.0547
-8.500 -0.6636 0.01850 0.01206 -0.0689 0.9766 0.0569
-8.250 -0.6308 0.01797 0.01156 -0.0709 0.9748 0.0590
-8.000 -0.5968 0.01753 0.01112 -0.0730 0.9734 0.0611
-7.750 -0.5623 0.01718 0.01073 -0.0750 0.9722 0.0631
-7.500 -0.5253 0.01651 0.01011 -0.0780 0.9713 0.0667
-7.250 -0.4884 0.01613 0.00975 -0.0806 0.9705 0.0702
-7.000 -0.4510 0.01575 0.00935 -0.0833 0.9698 0.0739
-6.750 -0.4129 0.01529 0.00896 -0.0862 0.9692 0.0799
-6.500 -0.3748 0.01492 0.00863 -0.0890 0.9687 0.0874
-6.250 -0.3363 0.01458 0.00834 -0.0918 0.9681 0.0975
-6.000 -0.3097 0.01425 0.00806 -0.0923 0.9642 0.1086
-5.750 -0.2740 0.01385 0.00777 -0.0946 0.9624 0.1253
-5.500 -0.2356 0.01341 0.00748 -0.0976 0.9612 0.1512
-5.250 -0.1942 0.01285 0.00717 -0.1015 0.9606 0.2006
-5.000 -0.1449 0.01193 0.00673 -0.1077 0.9612 0.3060
-4.750 -0.0821 0.01065 0.00626 -0.1173 0.9645 0.4928
-4.500 -0.0479 0.01060 0.00643 -0.1187 0.9624 0.5605
-4.250 -0.0145 0.01065 0.00649 -0.1198 0.9603 0.5832
-4.000 0.0198 0.01072 0.00655 -0.1211 0.9586 0.5990
-3.750 0.0540 0.01081 0.00667 -0.1222 0.9570 0.6096
-3.500 0.0906 0.01089 0.00675 -0.1237 0.9557 0.6202
-3.250 0.1285 0.01098 0.00684 -0.1255 0.9547 0.6301
-3.000 0.1678 0.01096 0.00683 -0.1276 0.9539 0.6358
-2.750 0.1885 0.01108 0.00699 -0.1257 0.9468 0.6397
-2.500 0.2271 0.01101 0.00693 -0.1275 0.9443 0.6458
-2.250 0.2663 0.01094 0.00688 -0.1293 0.9425 0.6526
-2.000 0.3027 0.01094 0.00696 -0.1300 0.9402 0.6577
-1.750 0.3346 0.01079 0.00683 -0.1298 0.9328 0.6635
-1.500 0.3754 0.01026 0.00624 -0.1318 0.9250 0.6678
-1.250 0.4032 0.01002 0.00603 -0.1311 0.9154 0.6695
-1.000 0.4330 0.00989 0.00593 -0.1309 0.9082 0.6712
-0.750 0.4596 0.00987 0.00593 -0.1301 0.8987 0.6730
-0.500 0.4908 0.00974 0.00579 -0.1303 0.8895 0.6746
-0.250 0.5186 0.00967 0.00574 -0.1300 0.8767 0.6764
0.000 0.5480 0.00961 0.00566 -0.1299 0.8607 0.6786
0.250 0.5785 0.00953 0.00552 -0.1301 0.8390 0.6811
0.500 0.6091 0.00949 0.00535 -0.1304 0.8044 0.6834
0.750 0.6371 0.00966 0.00519 -0.1301 0.7339 0.6852
1.000 0.6533 0.01043 0.00532 -0.1274 0.6029 0.6864
1.250 0.6677 0.01147 0.00568 -0.1247 0.4638 0.6876
1.500 0.6862 0.01235 0.00603 -0.1230 0.3497 0.6887
1.750 0.7075 0.01308 0.00633 -0.1218 0.2629 0.6898
2.000 0.7306 0.01368 0.00661 -0.1210 0.1990 0.6910
2.250 0.7550 0.01418 0.00687 -0.1204 0.1558 0.6922
2.500 0.7806 0.01458 0.00713 -0.1200 0.1284 0.6936
2.750 0.8063 0.01498 0.00739 -0.1196 0.1089 0.6952
3.000 0.8327 0.01532 0.00765 -0.1193 0.0971 0.6970
3.250 0.8598 0.01561 0.00790 -0.1191 0.0892 0.6989
3.500 0.8864 0.01598 0.00820 -0.1189 0.0826 0.7008
3.750 0.9144 0.01624 0.00844 -0.1190 0.0788 0.7026
4.000 0.9401 0.01651 0.00870 -0.1185 0.0750 0.7041
4.250 0.9638 0.01695 0.00912 -0.1176 0.0712 0.7053
4.500 0.9893 0.01722 0.00943 -0.1170 0.0686 0.7066
4.750 1.0142 0.01755 0.00977 -0.1164 0.0659 0.7077
5.000 1.0371 0.01811 0.01030 -0.1154 0.0630 0.7090
5.250 1.0614 0.01853 0.01076 -0.1146 0.0610 0.7103
5.500 1.0863 0.01887 0.01113 -0.1140 0.0589 0.7118
5.750 1.1108 0.01926 0.01152 -0.1134 0.0568 0.7134
6.000 1.1325 0.01997 0.01219 -0.1123 0.0545 0.7151
6.250 1.1560 0.02050 0.01276 -0.1115 0.0531 0.7168
6.500 1.1806 0.02090 0.01320 -0.1108 0.0516 0.7186
6.750 1.2047 0.02137 0.01368 -0.1102 0.0501 0.7203
7.000 1.2270 0.02180 0.01413 -0.1091 0.0487 0.7217
7.250 1.2467 0.02258 0.01491 -0.1077 0.0472 0.7230
7.500 1.2675 0.02326 0.01565 -0.1064 0.0460 0.7242
7.750 1.2894 0.02370 0.01617 -0.1052 0.0450 0.7256
8.000 1.3105 0.02422 0.01676 -0.1040 0.0439 0.7270
8.250 1.3310 0.02476 0.01733 -0.1026 0.0429 0.7286
8.500 1.3507 0.02532 0.01791 -0.1012 0.0420 0.7303
8.750 1.3693 0.02601 0.01861 -0.0997 0.0412 0.7321
9.000 1.3870 0.02733 0.01994 -0.0982 0.0402 0.7339
9.250 1.4032 0.02784 0.02054 -0.0961 0.0397 0.7357
9.500 1.4189 0.02844 0.02123 -0.0940 0.0390 0.7373
9.750 1.4353 0.02910 0.02198 -0.0921 0.0382 0.7388
10.000 1.4511 0.02979 0.02276 -0.0901 0.0375 0.7402
10.250 1.4664 0.03054 0.02358 -0.0881 0.0369 0.7417
10.500 1.4811 0.03134 0.02443 -0.0861 0.0363 0.7432
10.750 1.4951 0.03221 0.02535 -0.0841 0.0358 0.7449
11.000 1.5083 0.03335 0.02652 -0.0821 0.0353 0.7467
11.250 1.5200 0.03523 0.02849 -0.0801 0.0346 0.7486
11.500 1.5312 0.03628 0.02967 -0.0778 0.0344 0.7508
11.750 1.5417 0.03746 0.03099 -0.0756 0.0340 0.7528
12.000 1.5512 0.03878 0.03244 -0.0734 0.0336 0.7545
12.250 1.5592 0.04017 0.03397 -0.0711 0.0332 0.7560
12.500 1.5658 0.04166 0.03560 -0.0687 0.0329 0.7575
12.750 1.5710 0.04327 0.03735 -0.0663 0.0325 0.7590
13.000 1.5751 0.04498 0.03919 -0.0640 0.0322 0.7605
13.250 1.5784 0.04678 0.04112 -0.0618 0.0319 0.7622
13.500 1.5811 0.04866 0.04312 -0.0597 0.0316 0.7640
13.750 1.5833 0.05062 0.04518 -0.0579 0.0313 0.7658
14.000 1.5850 0.05268 0.04733 -0.0562 0.0310 0.7678
14.250 1.5852 0.05502 0.04976 -0.0547 0.0308 0.7697
14.500 1.5849 0.05751 0.05232 -0.0534 0.0305 0.7715
14.750 1.5807 0.06049 0.05542 -0.0522 0.0303 0.7730
15.000 1.5714 0.06424 0.05933 -0.0512 0.0301 0.7744
15.250 1.5536 0.06927 0.06456 -0.0506 0.0299 0.7755
15.500 1.5350 0.07459 0.07011 -0.0509 0.0297 0.7767
15.750 1.5193 0.07989 0.07563 -0.0521 0.0297 0.7781
16.000 1.5005 0.08612 0.08208 -0.0543 0.0296 0.7793
16.250 1.4778 0.09351 0.08970 -0.0578 0.0296 0.7804
16.500 1.4504 0.10240 0.09882 -0.0629 0.0296 0.7814
16.750 1.4161 0.11345 0.11013 -0.0702 0.0296 0.7820
17.000 1.3645 0.12934 0.12634 -0.0818 0.0296 0.7819
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