SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| 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: 80.02 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-nasasc2-0714-il-1000000-n5.txt Download as CSV file: xf-nasasc2-0714-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2630 0.06912 0.06503 -0.0699 1.0000 0.0193
-19.500 -1.2715 0.06461 0.06042 -0.0720 1.0000 0.0195
-19.250 -1.2765 0.06069 0.05641 -0.0736 1.0000 0.0196
-19.000 -1.2795 0.05718 0.05282 -0.0750 1.0000 0.0198
-18.750 -1.2806 0.05402 0.04958 -0.0762 1.0000 0.0199
-18.500 -1.2800 0.05117 0.04666 -0.0770 1.0000 0.0201
-18.250 -1.2780 0.04861 0.04402 -0.0777 1.0000 0.0203
-18.000 -1.2751 0.04626 0.04161 -0.0781 1.0000 0.0205
-17.750 -1.2714 0.04410 0.03938 -0.0783 1.0000 0.0207
-17.500 -1.2666 0.04216 0.03739 -0.0783 1.0000 0.0209
-17.250 -1.2621 0.04033 0.03549 -0.0781 1.0000 0.0211
-17.000 -1.2570 0.03869 0.03379 -0.0776 1.0000 0.0213
-16.750 -1.2517 0.03716 0.03221 -0.0769 1.0000 0.0216
-16.500 -1.2469 0.03574 0.03074 -0.0760 1.0000 0.0218
-16.250 -1.2422 0.03447 0.02942 -0.0747 1.0000 0.0219
-16.000 -1.2392 0.03327 0.02816 -0.0731 1.0000 0.0221
-15.750 -1.2382 0.03210 0.02695 -0.0710 1.0000 0.0223
-15.500 -1.2268 0.03072 0.02553 -0.0711 0.9993 0.0227
-15.250 -1.2096 0.02947 0.02424 -0.0720 0.9982 0.0231
-15.000 -1.1910 0.02832 0.02306 -0.0729 0.9970 0.0235
-14.750 -1.1717 0.02725 0.02196 -0.0738 0.9957 0.0240
-14.500 -1.1513 0.02627 0.02094 -0.0747 0.9946 0.0244
-14.250 -1.1298 0.02533 0.01996 -0.0757 0.9936 0.0248
-14.000 -1.1079 0.02443 0.01903 -0.0767 0.9925 0.0253
-13.750 -1.0892 0.02362 0.01818 -0.0769 0.9901 0.0256
-13.500 -1.0683 0.02284 0.01735 -0.0774 0.9879 0.0260
-13.250 -1.0469 0.02201 0.01649 -0.0781 0.9859 0.0264
-13.000 -1.0237 0.02121 0.01568 -0.0791 0.9843 0.0271
-12.750 -0.9977 0.02046 0.01492 -0.0805 0.9830 0.0277
-12.500 -0.9701 0.01978 0.01422 -0.0820 0.9820 0.0283
-12.250 -0.9421 0.01914 0.01357 -0.0835 0.9811 0.0290
-12.000 -0.9209 0.01858 0.01299 -0.0835 0.9778 0.0296
-11.750 -0.8952 0.01803 0.01240 -0.0844 0.9757 0.0301
-11.500 -0.8679 0.01750 0.01185 -0.0855 0.9740 0.0306
-11.250 -0.8401 0.01689 0.01124 -0.0869 0.9724 0.0316
-11.000 -0.8111 0.01636 0.01071 -0.0883 0.9711 0.0325
-10.750 -0.7813 0.01587 0.01022 -0.0898 0.9698 0.0335
-10.500 -0.7508 0.01541 0.00974 -0.0913 0.9687 0.0343
-10.250 -0.7214 0.01500 0.00931 -0.0926 0.9671 0.0351
-10.000 -0.6942 0.01460 0.00890 -0.0933 0.9648 0.0358
-9.750 -0.6654 0.01413 0.00844 -0.0945 0.9627 0.0370
-9.500 -0.6354 0.01373 0.00804 -0.0958 0.9609 0.0381
-9.250 -0.6048 0.01335 0.00766 -0.0972 0.9592 0.0392
-9.000 -0.5736 0.01299 0.00730 -0.0986 0.9578 0.0403
-8.750 -0.5420 0.01267 0.00697 -0.1000 0.9564 0.0412
-8.500 -0.5096 0.01228 0.00658 -0.1017 0.9551 0.0427
-8.250 -0.4770 0.01193 0.00624 -0.1033 0.9538 0.0442
-8.000 -0.4457 0.01162 0.00594 -0.1046 0.9520 0.0457
-7.750 -0.4146 0.01135 0.00567 -0.1059 0.9501 0.0472
-7.500 -0.3828 0.01105 0.00539 -0.1072 0.9482 0.0493
-7.250 -0.3507 0.01076 0.00512 -0.1086 0.9464 0.0518
-7.000 -0.3185 0.01051 0.00488 -0.1100 0.9446 0.0543
-6.750 -0.2861 0.01024 0.00464 -0.1113 0.9428 0.0578
-6.500 -0.2534 0.00999 0.00441 -0.1127 0.9412 0.0625
-6.250 -0.2203 0.00973 0.00420 -0.1142 0.9397 0.0690
-6.000 -0.1872 0.00950 0.00401 -0.1157 0.9382 0.0758
-5.750 -0.1554 0.00930 0.00385 -0.1168 0.9359 0.0833
-5.500 -0.1230 0.00907 0.00368 -0.1181 0.9335 0.0928
-5.250 -0.0905 0.00886 0.00352 -0.1193 0.9311 0.1019
-5.000 -0.0581 0.00867 0.00337 -0.1205 0.9285 0.1106
-4.750 -0.0250 0.00846 0.00321 -0.1218 0.9259 0.1227
-4.500 0.0091 0.00819 0.00304 -0.1235 0.9235 0.1431
-4.250 0.0439 0.00790 0.00288 -0.1253 0.9214 0.1750
-4.000 0.0789 0.00757 0.00272 -0.1273 0.9182 0.2159
-3.750 0.1138 0.00725 0.00255 -0.1292 0.9135 0.2568
-3.500 0.1527 0.00673 0.00230 -0.1322 0.9087 0.3361
-3.250 0.1942 0.00608 0.00202 -0.1359 0.9042 0.4445
-3.000 0.2312 0.00568 0.00190 -0.1383 0.8968 0.5291
-2.750 0.2623 0.00562 0.00187 -0.1388 0.8862 0.5562
-2.500 0.2917 0.00562 0.00182 -0.1389 0.8651 0.5688
-2.250 0.3203 0.00569 0.00178 -0.1388 0.8350 0.5792
-2.000 0.3484 0.00584 0.00180 -0.1385 0.7975 0.5900
-1.750 0.3725 0.00627 0.00186 -0.1375 0.7151 0.5995
-1.500 0.3951 0.00691 0.00208 -0.1363 0.6120 0.6076
-1.250 0.4198 0.00745 0.00226 -0.1356 0.5273 0.6138
-1.000 0.4446 0.00801 0.00243 -0.1350 0.4390 0.6165
-0.750 0.4707 0.00841 0.00259 -0.1347 0.3761 0.6185
-0.500 0.4965 0.00887 0.00276 -0.1343 0.3056 0.6204
-0.250 0.5230 0.00926 0.00292 -0.1340 0.2521 0.6227
0.000 0.5502 0.00956 0.00305 -0.1339 0.2143 0.6250
0.250 0.5775 0.00986 0.00319 -0.1337 0.1789 0.6271
0.500 0.6049 0.01015 0.00334 -0.1336 0.1505 0.6290
0.750 0.6326 0.01039 0.00347 -0.1335 0.1295 0.6307
1.000 0.6604 0.01062 0.00360 -0.1334 0.1134 0.6320
1.250 0.6884 0.01082 0.00373 -0.1333 0.1019 0.6330
1.500 0.7162 0.01102 0.00388 -0.1332 0.0918 0.6344
1.750 0.7438 0.01123 0.00404 -0.1330 0.0804 0.6357
2.000 0.7713 0.01145 0.00420 -0.1329 0.0712 0.6370
2.250 0.7990 0.01165 0.00436 -0.1327 0.0657 0.6382
2.500 0.8265 0.01186 0.00454 -0.1325 0.0615 0.6395
2.750 0.8541 0.01205 0.00471 -0.1324 0.0591 0.6408
3.000 0.8815 0.01226 0.00490 -0.1321 0.0567 0.6421
3.250 0.9086 0.01249 0.00511 -0.1319 0.0540 0.6434
3.500 0.9361 0.01267 0.00529 -0.1317 0.0528 0.6446
3.750 0.9634 0.01287 0.00549 -0.1314 0.0513 0.6460
4.000 0.9903 0.01309 0.00570 -0.1311 0.0496 0.6475
4.250 1.0170 0.01334 0.00593 -0.1308 0.0479 0.6489
4.500 1.0435 0.01359 0.00617 -0.1304 0.0463 0.6502
4.750 1.0703 0.01379 0.00639 -0.1301 0.0451 0.6520
5.000 1.0968 0.01401 0.00662 -0.1297 0.0435 0.6535
5.250 1.1230 0.01426 0.00686 -0.1292 0.0419 0.6550
5.500 1.1487 0.01455 0.00714 -0.1287 0.0402 0.6564
5.750 1.1747 0.01479 0.00740 -0.1282 0.0393 0.6579
6.000 1.2004 0.01505 0.00767 -0.1277 0.0380 0.6593
6.250 1.2257 0.01533 0.00795 -0.1271 0.0367 0.6607
6.500 1.2507 0.01565 0.00825 -0.1264 0.0352 0.6620
6.750 1.2756 0.01595 0.00856 -0.1258 0.0342 0.6633
7.000 1.3003 0.01625 0.00888 -0.1251 0.0332 0.6646
7.250 1.3247 0.01657 0.00920 -0.1243 0.0323 0.6658
7.500 1.3487 0.01691 0.00954 -0.1235 0.0314 0.6669
7.750 1.3722 0.01728 0.00991 -0.1226 0.0305 0.6680
8.000 1.3954 0.01766 0.01032 -0.1216 0.0297 0.6696
8.250 1.4186 0.01800 0.01071 -0.1206 0.0292 0.6711
8.500 1.4414 0.01836 0.01110 -0.1196 0.0286 0.6726
8.750 1.4637 0.01874 0.01151 -0.1185 0.0279 0.6741
9.000 1.4853 0.01914 0.01193 -0.1173 0.0272 0.6756
9.250 1.5062 0.01957 0.01238 -0.1159 0.0266 0.6772
9.500 1.5262 0.02003 0.01287 -0.1144 0.0260 0.6787
9.750 1.5450 0.02055 0.01341 -0.1127 0.0254 0.6803
10.000 1.5641 0.02098 0.01389 -0.1110 0.0251 0.6818
10.250 1.5805 0.02143 0.01438 -0.1088 0.0248 0.6833
10.500 1.5970 0.02191 0.01491 -0.1067 0.0245 0.6846
10.750 1.6141 0.02243 0.01548 -0.1048 0.0242 0.6861
11.000 1.6311 0.02298 0.01609 -0.1029 0.0238 0.6880
11.250 1.6477 0.02356 0.01672 -0.1009 0.0235 0.6899
11.500 1.6638 0.02418 0.01738 -0.0990 0.0231 0.6918
11.750 1.6793 0.02483 0.01808 -0.0969 0.0228 0.6937
12.000 1.6940 0.02554 0.01884 -0.0949 0.0225 0.6956
12.250 1.7082 0.02630 0.01965 -0.0927 0.0221 0.6974
12.500 1.7209 0.02715 0.02055 -0.0905 0.0218 0.6991
12.750 1.7327 0.02807 0.02153 -0.0882 0.0215 0.7008
13.000 1.7457 0.02891 0.02243 -0.0860 0.0214 0.7023
13.250 1.7584 0.02977 0.02336 -0.0840 0.0212 0.7039
13.500 1.7701 0.03070 0.02437 -0.0818 0.0210 0.7058
13.750 1.7815 0.03167 0.02542 -0.0797 0.0208 0.7076
14.000 1.7920 0.03272 0.02656 -0.0776 0.0206 0.7095
14.250 1.8016 0.03385 0.02776 -0.0755 0.0204 0.7116
14.500 1.8107 0.03504 0.02903 -0.0734 0.0202 0.7138
14.750 1.8187 0.03635 0.03042 -0.0713 0.0200 0.7159
15.000 1.8261 0.03774 0.03188 -0.0693 0.0198 0.7178
15.250 1.8320 0.03926 0.03348 -0.0672 0.0196 0.7195
15.500 1.8370 0.04092 0.03522 -0.0653 0.0195 0.7211
15.750 1.8414 0.04269 0.03708 -0.0635 0.0193 0.7229
16.000 1.8446 0.04462 0.03911 -0.0617 0.0192 0.7248
16.250 1.8460 0.04676 0.04134 -0.0601 0.0190 0.7268
16.500 1.8462 0.04912 0.04380 -0.0586 0.0189 0.7289
16.750 1.8451 0.05175 0.04652 -0.0574 0.0188 0.7309
17.000 1.8424 0.05469 0.04957 -0.0564 0.0186 0.7327
17.250 1.8377 0.05802 0.05301 -0.0558 0.0185 0.7344
17.500 1.8305 0.06183 0.05694 -0.0556 0.0184 0.7358
17.750 1.8209 0.06621 0.06144 -0.0559 0.0182 0.7372
18.000 1.8086 0.07123 0.06659 -0.0568 0.0181 0.7386
18.250 1.7930 0.07702 0.07254 -0.0584 0.0181 0.7401
18.500 1.7786 0.08290 0.07857 -0.0604 0.0180 0.7415
18.750 1.7594 0.08985 0.08569 -0.0634 0.0180 0.7428
19.000 1.7349 0.09800 0.09402 -0.0673 0.0180 0.7438
19.250 1.7033 0.10769 0.10390 -0.0725 0.0180 0.7445
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