SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il) Xfoil prediction polar at RE=1,000,000 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: 1,000,000 Max Cl/Cd: 83.67 at α=-0.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-nasasc2-0714-il-1000000.txt Download as CSV file: xf-nasasc2-0714-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1778 0.08108 0.07746 -0.0649 1.0000 0.0235
-19.500 -1.1876 0.07605 0.07233 -0.0674 1.0000 0.0236
-19.250 -1.1956 0.07137 0.06755 -0.0698 1.0000 0.0238
-19.000 -1.2013 0.06716 0.06326 -0.0717 1.0000 0.0239
-18.750 -1.2053 0.06332 0.05933 -0.0734 1.0000 0.0241
-18.500 -1.2077 0.05980 0.05572 -0.0749 1.0000 0.0243
-18.250 -1.2088 0.05656 0.05240 -0.0761 1.0000 0.0245
-18.000 -1.2087 0.05360 0.04936 -0.0770 1.0000 0.0247
-17.750 -1.2075 0.05089 0.04657 -0.0777 1.0000 0.0249
-17.500 -1.2051 0.04846 0.04406 -0.0782 1.0000 0.0251
-17.250 -1.2022 0.04621 0.04174 -0.0784 1.0000 0.0253
-17.000 -1.1988 0.04413 0.03959 -0.0783 1.0000 0.0255
-16.750 -1.1946 0.04229 0.03767 -0.0780 1.0000 0.0257
-16.500 -1.1898 0.04061 0.03592 -0.0775 1.0000 0.0259
-16.250 -1.1848 0.03907 0.03432 -0.0768 1.0000 0.0261
-16.000 -1.1877 0.03708 0.03227 -0.0755 1.0000 0.0264
-15.750 -1.1920 0.03525 0.03038 -0.0737 1.0000 0.0268
-15.500 -1.1937 0.03384 0.02894 -0.0716 1.0000 0.0272
-15.250 -1.1940 0.03267 0.02775 -0.0693 1.0000 0.0275
-15.000 -1.1944 0.03161 0.02666 -0.0669 1.0000 0.0277
-14.750 -1.1939 0.03067 0.02569 -0.0642 1.0000 0.0280
-14.500 -1.1947 0.02976 0.02475 -0.0614 1.0000 0.0283
-14.250 -1.1880 0.02884 0.02379 -0.0598 0.9996 0.0287
-14.000 -1.1671 0.02782 0.02272 -0.0609 0.9985 0.0292
-13.750 -1.1455 0.02685 0.02171 -0.0620 0.9971 0.0297
-13.500 -1.1223 0.02602 0.02082 -0.0632 0.9958 0.0301
-13.250 -1.0983 0.02526 0.02000 -0.0643 0.9945 0.0305
-13.000 -1.0797 0.02394 0.01864 -0.0655 0.9931 0.0312
-12.750 -1.0625 0.02293 0.01761 -0.0657 0.9904 0.0319
-12.500 -1.0380 0.02215 0.01682 -0.0669 0.9882 0.0326
-12.250 -1.0104 0.02147 0.01613 -0.0683 0.9865 0.0333
-12.000 -0.9815 0.02082 0.01545 -0.0700 0.9852 0.0340
-11.750 -0.9516 0.02021 0.01482 -0.0718 0.9841 0.0347
-11.500 -0.9208 0.01969 0.01426 -0.0736 0.9833 0.0353
-11.250 -0.8905 0.01885 0.01339 -0.0758 0.9825 0.0362
-11.000 -0.8590 0.01808 0.01262 -0.0782 0.9819 0.0374
-10.750 -0.8262 0.01757 0.01212 -0.0804 0.9814 0.0385
-10.500 -0.8033 0.01712 0.01166 -0.0804 0.9783 0.0394
-10.250 -0.7748 0.01668 0.01120 -0.0816 0.9763 0.0403
-10.000 -0.7435 0.01629 0.01078 -0.0831 0.9749 0.0410
-9.750 -0.7107 0.01556 0.01003 -0.0855 0.9738 0.0425
-9.500 -0.6768 0.01501 0.00951 -0.0878 0.9729 0.0441
-9.250 -0.6425 0.01459 0.00908 -0.0900 0.9722 0.0454
-9.000 -0.6079 0.01419 0.00868 -0.0922 0.9717 0.0467
-8.750 -0.5730 0.01387 0.00834 -0.0942 0.9712 0.0476
-8.500 -0.5365 0.01326 0.00774 -0.0972 0.9708 0.0502
-8.250 -0.5004 0.01285 0.00736 -0.0996 0.9704 0.0522
-8.000 -0.4645 0.01252 0.00702 -0.1019 0.9701 0.0540
-7.750 -0.4284 0.01216 0.00665 -0.1043 0.9696 0.0560
-7.500 -0.3917 0.01174 0.00628 -0.1068 0.9692 0.0598
-7.250 -0.3556 0.01144 0.00599 -0.1091 0.9687 0.0629
-7.000 -0.3190 0.01107 0.00566 -0.1115 0.9682 0.0686
-6.750 -0.2892 0.01082 0.00545 -0.1123 0.9659 0.0743
-6.500 -0.2576 0.01053 0.00522 -0.1136 0.9637 0.0833
-6.250 -0.2234 0.01022 0.00498 -0.1154 0.9621 0.0949
-6.000 -0.1885 0.00992 0.00475 -0.1173 0.9609 0.1068
-5.750 -0.1534 0.00963 0.00452 -0.1192 0.9597 0.1201
-5.500 -0.1176 0.00931 0.00429 -0.1213 0.9586 0.1391
-5.250 -0.0798 0.00888 0.00403 -0.1240 0.9578 0.1747
-5.000 -0.0402 0.00835 0.00374 -0.1273 0.9569 0.2297
-4.750 0.0025 0.00766 0.00339 -0.1315 0.9563 0.3146
-4.500 0.0490 0.00678 0.00299 -0.1367 0.9561 0.4414
-4.250 0.0891 0.00631 0.00282 -0.1399 0.9552 0.5287
-4.000 0.1220 0.00622 0.00280 -0.1409 0.9530 0.5607
-3.750 0.1507 0.00616 0.00277 -0.1409 0.9486 0.5764
-3.500 0.1811 0.00610 0.00272 -0.1412 0.9446 0.5879
-3.250 0.2121 0.00606 0.00265 -0.1416 0.9411 0.5988
-3.000 0.2419 0.00604 0.00266 -0.1416 0.9368 0.6068
-2.750 0.2702 0.00599 0.00260 -0.1414 0.9295 0.6127
-2.500 0.2994 0.00591 0.00247 -0.1412 0.9205 0.6173
-2.250 0.3275 0.00586 0.00243 -0.1409 0.9101 0.6216
-2.000 0.3564 0.00591 0.00246 -0.1407 0.9006 0.6275
-1.750 0.3860 0.00598 0.00247 -0.1407 0.8900 0.6326
-1.500 0.4143 0.00600 0.00254 -0.1405 0.8792 0.6383
-1.250 0.4430 0.00609 0.00261 -0.1403 0.8684 0.6425
-1.000 0.4721 0.00613 0.00261 -0.1403 0.8526 0.6448
-0.750 0.5011 0.00618 0.00259 -0.1403 0.8320 0.6463
-0.500 0.5288 0.00632 0.00258 -0.1399 0.7970 0.6480
-0.250 0.5539 0.00666 0.00264 -0.1391 0.7340 0.6498
0.000 0.5747 0.00730 0.00279 -0.1375 0.6254 0.6521
0.250 0.5949 0.00812 0.00307 -0.1359 0.5009 0.6538
0.500 0.6172 0.00883 0.00333 -0.1349 0.3987 0.6553
0.750 0.6406 0.00946 0.00357 -0.1340 0.3086 0.6567
1.000 0.6652 0.00999 0.00380 -0.1334 0.2403 0.6582
1.250 0.6909 0.01042 0.00400 -0.1330 0.1906 0.6596
1.500 0.7171 0.01081 0.00419 -0.1326 0.1537 0.6611
1.750 0.7440 0.01110 0.00437 -0.1324 0.1296 0.6626
2.000 0.7710 0.01140 0.00455 -0.1321 0.1108 0.6639
2.250 0.7981 0.01168 0.00473 -0.1319 0.0953 0.6651
2.500 0.8253 0.01194 0.00492 -0.1317 0.0831 0.6662
2.750 0.8527 0.01218 0.00509 -0.1315 0.0761 0.6672
3.000 0.8800 0.01241 0.00528 -0.1313 0.0706 0.6683
3.250 0.9073 0.01259 0.00546 -0.1311 0.0673 0.6700
3.500 0.9339 0.01286 0.00570 -0.1307 0.0635 0.6714
3.750 0.9608 0.01309 0.00593 -0.1304 0.0613 0.6727
4.000 0.9877 0.01330 0.00616 -0.1301 0.0595 0.6740
4.250 1.0140 0.01357 0.00642 -0.1296 0.0573 0.6754
4.500 1.0393 0.01396 0.00679 -0.1290 0.0543 0.6770
4.750 1.0658 0.01418 0.00704 -0.1286 0.0530 0.6788
5.000 1.0923 0.01441 0.00728 -0.1282 0.0514 0.6805
5.250 1.1183 0.01468 0.00754 -0.1278 0.0497 0.6820
5.500 1.1433 0.01506 0.00790 -0.1271 0.0476 0.6832
5.750 1.1684 0.01542 0.00827 -0.1265 0.0461 0.6844
6.000 1.1944 0.01565 0.00851 -0.1260 0.0450 0.6854
6.250 1.2202 0.01587 0.00875 -0.1255 0.0436 0.6875
6.500 1.2452 0.01615 0.00903 -0.1249 0.0421 0.6891
6.750 1.2679 0.01668 0.00956 -0.1238 0.0403 0.6906
7.000 1.2929 0.01693 0.00984 -0.1231 0.0396 0.6920
7.250 1.3174 0.01722 0.01017 -0.1224 0.0387 0.6934
7.500 1.3415 0.01754 0.01050 -0.1215 0.0377 0.6949
7.750 1.3650 0.01789 0.01086 -0.1206 0.0367 0.6964
8.000 1.3874 0.01834 0.01131 -0.1195 0.0356 0.6979
8.250 1.4077 0.01895 0.01194 -0.1181 0.0346 0.6994
8.500 1.4308 0.01927 0.01230 -0.1171 0.0340 0.7008
8.750 1.4529 0.01965 0.01270 -0.1160 0.0333 0.7020
9.000 1.4743 0.02005 0.01314 -0.1147 0.0326 0.7033
9.250 1.4949 0.02046 0.01358 -0.1133 0.0320 0.7052
9.500 1.5142 0.02092 0.01408 -0.1117 0.0314 0.7069
9.750 1.5314 0.02150 0.01468 -0.1097 0.0307 0.7084
10.000 1.5418 0.02231 0.01554 -0.1065 0.0300 0.7100
10.250 1.5564 0.02295 0.01625 -0.1041 0.0296 0.7116
10.500 1.5737 0.02347 0.01683 -0.1022 0.0293 0.7133
10.750 1.5907 0.02403 0.01745 -0.1003 0.0289 0.7150
11.000 1.6067 0.02467 0.01814 -0.0983 0.0286 0.7167
11.250 1.6224 0.02532 0.01885 -0.0963 0.0282 0.7183
11.500 1.6372 0.02603 0.01960 -0.0942 0.0278 0.7197
11.750 1.6520 0.02674 0.02037 -0.0922 0.0274 0.7217
12.000 1.6657 0.02751 0.02120 -0.0900 0.0270 0.7238
12.250 1.6784 0.02836 0.02212 -0.0878 0.0267 0.7256
12.500 1.6894 0.02935 0.02316 -0.0854 0.0263 0.7274
12.750 1.6968 0.03060 0.02448 -0.0827 0.0259 0.7292
13.000 1.6971 0.03245 0.02642 -0.0792 0.0254 0.7309
13.250 1.7080 0.03349 0.02755 -0.0771 0.0253 0.7328
13.500 1.7187 0.03455 0.02869 -0.0751 0.0251 0.7346
13.750 1.7280 0.03575 0.02998 -0.0730 0.0249 0.7362
14.000 1.7362 0.03708 0.03139 -0.0710 0.0247 0.7376
14.250 1.7432 0.03851 0.03292 -0.0689 0.0245 0.7400
14.500 1.7489 0.04008 0.03460 -0.0669 0.0243 0.7419
14.750 1.7534 0.04180 0.03641 -0.0649 0.0241 0.7438
15.000 1.7574 0.04363 0.03834 -0.0630 0.0239 0.7457
15.250 1.7600 0.04564 0.04045 -0.0613 0.0237 0.7477
15.500 1.7610 0.04786 0.04277 -0.0597 0.0236 0.7497
15.750 1.7615 0.05023 0.04524 -0.0583 0.0234 0.7516
16.000 1.7610 0.05284 0.04794 -0.0571 0.0232 0.7533
16.250 1.7592 0.05573 0.05093 -0.0562 0.0231 0.7546
16.500 1.7562 0.05890 0.05420 -0.0557 0.0230 0.7567
16.750 1.7513 0.06246 0.05789 -0.0555 0.0228 0.7585
17.000 1.7451 0.06640 0.06195 -0.0557 0.0227 0.7602
17.250 1.7366 0.07088 0.06654 -0.0564 0.0226 0.7619
17.500 1.7259 0.07589 0.07168 -0.0576 0.0225 0.7635
17.750 1.7128 0.08150 0.07742 -0.0595 0.0224 0.7650
18.000 1.6966 0.08787 0.08394 -0.0620 0.0223 0.7664
18.250 1.6779 0.09489 0.09111 -0.0652 0.0223 0.7676
18.500 1.6566 0.10258 0.09894 -0.0690 0.0222 0.7687
18.750 1.6326 0.11090 0.10741 -0.0735 0.0221 0.7695
19.000 1.6078 0.11958 0.11625 -0.0784 0.0221 0.7702
19.250 1.5817 0.12873 0.12555 -0.0840 0.0220 0.7709
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