NASA SC(2)-0714 AIRFOIL (sc20714-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA SC(2)-0714 AIRFOIL (sc20714-il) Reynolds number: 500,000 Max Cl/Cd: 64.19 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc20714-il-500000-n5.txt Download as CSV file: xf-sc20714-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0714 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 -1.0323 0.10690 0.10290 -0.0508 1.0000 0.0236
-19.500 -1.0544 0.09904 0.09488 -0.0551 1.0000 0.0237
-19.250 -1.0727 0.09207 0.08776 -0.0589 1.0000 0.0238
-19.000 -1.0876 0.08579 0.08133 -0.0623 1.0000 0.0239
-18.750 -1.0997 0.08016 0.07557 -0.0652 1.0000 0.0240
-18.500 -1.1090 0.07512 0.07039 -0.0677 1.0000 0.0241
-18.250 -1.1161 0.07055 0.06569 -0.0699 1.0000 0.0242
-18.000 -1.1217 0.06639 0.06142 -0.0718 1.0000 0.0244
-17.750 -1.1271 0.06242 0.05737 -0.0734 1.0000 0.0246
-17.500 -1.1304 0.05887 0.05374 -0.0747 1.0000 0.0247
-17.250 -1.1321 0.05569 0.05048 -0.0758 1.0000 0.0249
-17.000 -1.1323 0.05283 0.04755 -0.0765 1.0000 0.0252
-16.750 -1.1314 0.05024 0.04489 -0.0769 1.0000 0.0254
-16.500 -1.1296 0.04793 0.04251 -0.0770 1.0000 0.0256
-16.250 -1.1273 0.04581 0.04032 -0.0769 1.0000 0.0258
-16.000 -1.1248 0.04385 0.03829 -0.0765 1.0000 0.0261
-15.750 -1.1218 0.04207 0.03645 -0.0759 1.0000 0.0264
-15.500 -1.1190 0.04042 0.03472 -0.0750 1.0000 0.0266
-15.250 -1.1164 0.03890 0.03315 -0.0738 1.0000 0.0269
-15.000 -1.1143 0.03752 0.03170 -0.0723 1.0000 0.0272
-14.750 -1.1125 0.03623 0.03035 -0.0706 1.0000 0.0275
-14.500 -1.1109 0.03505 0.02910 -0.0686 1.0000 0.0279
-14.250 -1.1094 0.03397 0.02796 -0.0663 1.0000 0.0281
-14.000 -1.1102 0.03285 0.02680 -0.0638 1.0000 0.0284
-13.750 -1.0963 0.03150 0.02542 -0.0642 0.9988 0.0289
-13.500 -1.0787 0.03029 0.02418 -0.0650 0.9972 0.0294
-13.250 -1.0597 0.02921 0.02305 -0.0658 0.9955 0.0299
-13.000 -1.0396 0.02819 0.02198 -0.0667 0.9940 0.0304
-12.750 -1.0190 0.02723 0.02097 -0.0675 0.9925 0.0310
-12.500 -1.0022 0.02633 0.02002 -0.0675 0.9896 0.0316
-12.250 -0.9831 0.02547 0.01910 -0.0678 0.9868 0.0322
-12.000 -0.9610 0.02460 0.01817 -0.0686 0.9847 0.0328
-11.750 -0.9361 0.02367 0.01724 -0.0700 0.9831 0.0335
-11.500 -0.9089 0.02289 0.01645 -0.0716 0.9819 0.0344
-11.250 -0.8802 0.02219 0.01571 -0.0733 0.9810 0.0354
-11.000 -0.8607 0.02157 0.01505 -0.0731 0.9772 0.0364
-10.750 -0.8350 0.02095 0.01439 -0.0740 0.9749 0.0372
-10.500 -0.8073 0.02021 0.01363 -0.0755 0.9731 0.0382
-10.250 -0.7776 0.01955 0.01298 -0.0772 0.9717 0.0393
-10.000 -0.7467 0.01897 0.01238 -0.0791 0.9707 0.0406
-9.750 -0.7152 0.01843 0.01181 -0.0809 0.9698 0.0419
-9.500 -0.6830 0.01788 0.01124 -0.0829 0.9691 0.0433
-9.250 -0.6502 0.01732 0.01069 -0.0851 0.9685 0.0450
-9.000 -0.6168 0.01683 0.01020 -0.0872 0.9680 0.0467
-8.750 -0.5933 0.01644 0.00978 -0.0871 0.9640 0.0481
-8.500 -0.5629 0.01596 0.00932 -0.0886 0.9620 0.0498
-8.250 -0.5308 0.01553 0.00890 -0.0903 0.9606 0.0520
-8.000 -0.4979 0.01514 0.00851 -0.0921 0.9594 0.0544
-7.750 -0.4644 0.01472 0.00811 -0.0941 0.9583 0.0569
-7.500 -0.4303 0.01433 0.00773 -0.0960 0.9574 0.0599
-7.250 -0.3961 0.01400 0.00739 -0.0980 0.9566 0.0629
-7.000 -0.3612 0.01359 0.00703 -0.1002 0.9558 0.0672
-6.750 -0.3262 0.01326 0.00671 -0.1022 0.9551 0.0717
-6.500 -0.2905 0.01289 0.00639 -0.1045 0.9543 0.0778
-6.250 -0.2546 0.01254 0.00610 -0.1067 0.9536 0.0854
-6.000 -0.2248 0.01230 0.00588 -0.1076 0.9507 0.0929
-5.750 -0.1931 0.01202 0.00565 -0.1088 0.9483 0.1024
-5.500 -0.1593 0.01171 0.00542 -0.1106 0.9466 0.1148
-5.250 -0.1243 0.01138 0.00519 -0.1126 0.9451 0.1333
-5.000 -0.0883 0.01102 0.00495 -0.1149 0.9438 0.1579
-4.750 -0.0509 0.01062 0.00470 -0.1175 0.9427 0.1930
-4.500 -0.0118 0.01014 0.00444 -0.1207 0.9418 0.2404
-4.250 0.0316 0.00947 0.00410 -0.1251 0.9413 0.3213
-4.000 0.0792 0.00864 0.00372 -0.1307 0.9412 0.4346
-3.750 0.1210 0.00820 0.00368 -0.1343 0.9405 0.5349
-3.500 0.1547 0.00816 0.00373 -0.1354 0.9391 0.5664
-3.250 0.1874 0.00816 0.00373 -0.1363 0.9375 0.5805
-3.000 0.2149 0.00820 0.00381 -0.1361 0.9328 0.5894
-2.750 0.2465 0.00815 0.00374 -0.1366 0.9279 0.6003
-2.500 0.2790 0.00807 0.00368 -0.1371 0.9224 0.6101
-2.250 0.3074 0.00804 0.00363 -0.1368 0.9111 0.6190
-2.000 0.3365 0.00801 0.00360 -0.1365 0.8982 0.6247
-1.750 0.3667 0.00800 0.00355 -0.1366 0.8847 0.6311
-1.500 0.3965 0.00800 0.00349 -0.1366 0.8661 0.6363
-1.250 0.4252 0.00801 0.00345 -0.1363 0.8411 0.6386
-1.000 0.4540 0.00807 0.00342 -0.1362 0.8143 0.6405
-0.750 0.4808 0.00827 0.00338 -0.1355 0.7583 0.6422
-0.500 0.5004 0.00899 0.00350 -0.1334 0.6361 0.6441
-0.250 0.5196 0.00987 0.00379 -0.1317 0.5100 0.6466
0.000 0.5421 0.01061 0.00405 -0.1307 0.4111 0.6490
0.250 0.5670 0.01116 0.00424 -0.1302 0.3343 0.6507
0.500 0.5927 0.01165 0.00442 -0.1299 0.2707 0.6519
0.750 0.6189 0.01206 0.00460 -0.1296 0.2215 0.6531
1.000 0.6449 0.01244 0.00480 -0.1292 0.1806 0.6542
1.250 0.6715 0.01276 0.00499 -0.1290 0.1521 0.6552
1.500 0.6983 0.01305 0.00518 -0.1287 0.1322 0.6563
1.750 0.7252 0.01334 0.00539 -0.1284 0.1148 0.6576
2.000 0.7522 0.01362 0.00559 -0.1282 0.1022 0.6590
2.250 0.7794 0.01386 0.00579 -0.1280 0.0936 0.6602
2.500 0.8066 0.01411 0.00600 -0.1278 0.0865 0.6614
3.000 0.8607 0.01463 0.00644 -0.1273 0.0736 0.6639
3.250 0.8874 0.01491 0.00668 -0.1270 0.0688 0.6652
3.500 0.9144 0.01516 0.00692 -0.1268 0.0651 0.6665
3.750 0.9409 0.01546 0.00718 -0.1264 0.0619 0.6678
4.000 0.9677 0.01572 0.00745 -0.1261 0.0595 0.6690
4.250 0.9942 0.01600 0.00771 -0.1258 0.0569 0.6702
4.500 1.0201 0.01632 0.00801 -0.1253 0.0546 0.6715
4.750 1.0458 0.01661 0.00833 -0.1248 0.0528 0.6728
5.000 1.0714 0.01690 0.00864 -0.1243 0.0511 0.6741
5.250 1.0966 0.01722 0.00897 -0.1237 0.0494 0.6753
5.500 1.1212 0.01759 0.00934 -0.1230 0.0476 0.6765
5.750 1.1463 0.01792 0.00970 -0.1223 0.0462 0.6777
6.000 1.1710 0.01825 0.01006 -0.1217 0.0446 0.6790
6.250 1.1953 0.01862 0.01044 -0.1209 0.0432 0.6804
6.500 1.2188 0.01906 0.01087 -0.1201 0.0419 0.6818
6.750 1.2427 0.01944 0.01129 -0.1192 0.0408 0.6832
7.000 1.2663 0.01983 0.01171 -0.1184 0.0396 0.6847
7.250 1.2895 0.02024 0.01215 -0.1174 0.0384 0.6861
7.500 1.3121 0.02068 0.01260 -0.1164 0.0372 0.6876
7.750 1.3338 0.02119 0.01311 -0.1153 0.0361 0.6890
8.000 1.3558 0.02160 0.01359 -0.1141 0.0351 0.6905
8.250 1.3770 0.02204 0.01409 -0.1128 0.0341 0.6921
8.500 1.3974 0.02251 0.01460 -0.1114 0.0331 0.6935
8.750 1.4169 0.02302 0.01515 -0.1099 0.0323 0.6949
9.000 1.4350 0.02361 0.01576 -0.1081 0.0316 0.6964
9.250 1.4521 0.02414 0.01637 -0.1061 0.0310 0.6979
9.500 1.4676 0.02470 0.01700 -0.1039 0.0304 0.6995
9.750 1.4842 0.02531 0.01767 -0.1019 0.0298 0.7011
10.000 1.5010 0.02595 0.01836 -0.1000 0.0292 0.7028
10.250 1.5175 0.02662 0.01908 -0.0981 0.0286 0.7045
10.500 1.5334 0.02733 0.01984 -0.0962 0.0281 0.7062
10.750 1.5481 0.02814 0.02068 -0.0942 0.0276 0.7078
11.000 1.5622 0.02899 0.02158 -0.0921 0.0271 0.7094
11.250 1.5763 0.02981 0.02251 -0.0901 0.0267 0.7112
11.500 1.5897 0.03069 0.02348 -0.0880 0.0263 0.7129
11.750 1.6024 0.03162 0.02451 -0.0859 0.0259 0.7147
12.000 1.6142 0.03262 0.02560 -0.0837 0.0255 0.7165
12.250 1.6256 0.03367 0.02674 -0.0816 0.0252 0.7183
12.500 1.6360 0.03480 0.02795 -0.0794 0.0249 0.7201
12.750 1.6455 0.03601 0.02924 -0.0773 0.0246 0.7219
13.000 1.6539 0.03732 0.03063 -0.0751 0.0243 0.7238
13.250 1.6609 0.03879 0.03218 -0.0730 0.0240 0.7257
13.500 1.6658 0.04046 0.03392 -0.0708 0.0237 0.7274
13.750 1.6686 0.04235 0.03589 -0.0685 0.0235 0.7290
14.000 1.6734 0.04412 0.03779 -0.0666 0.0233 0.7305
14.250 1.6771 0.04605 0.03986 -0.0648 0.0232 0.7322
14.500 1.6794 0.04816 0.04211 -0.0631 0.0230 0.7338
14.750 1.6803 0.05047 0.04456 -0.0615 0.0228 0.7356
15.000 1.6799 0.05303 0.04726 -0.0602 0.0226 0.7376
15.250 1.6780 0.05586 0.05022 -0.0591 0.0225 0.7396
15.500 1.6750 0.05896 0.05345 -0.0583 0.0223 0.7415
15.750 1.6705 0.06242 0.05706 -0.0579 0.0222 0.7434
16.000 1.6649 0.06625 0.06102 -0.0579 0.0220 0.7452
16.250 1.6576 0.07054 0.06545 -0.0585 0.0219 0.7467
16.500 1.6485 0.07532 0.07039 -0.0596 0.0217 0.7480
16.750 1.6373 0.08069 0.07593 -0.0613 0.0216 0.7492
17.000 1.6234 0.08679 0.08219 -0.0638 0.0215 0.7504
17.250 1.6071 0.09361 0.08919 -0.0670 0.0214 0.7515
17.500 1.5873 0.10133 0.09709 -0.0710 0.0213 0.7525
17.750 1.5639 0.10993 0.10588 -0.0758 0.0212 0.7534
18.000 1.5379 0.11932 0.11546 -0.0813 0.0212 0.7541
18.250 1.5083 0.12971 0.12605 -0.0878 0.0211 0.7547
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