S3010-103-84 (s3010-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: S3010-103-84 (s3010-il) Reynolds number: 100,000 Max Cl/Cd: 52.82 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s3010-il-100000-n5.txt Download as CSV file: xf-s3010-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S3010-103-84
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.000 -0.4217 0.09114 0.08620 -0.0221 1.0000 0.0323
-8.750 -0.4207 0.08698 0.08209 -0.0243 1.0000 0.0318
-8.500 -0.4213 0.08263 0.07780 -0.0266 1.0000 0.0310
-8.250 -0.4251 0.07771 0.07297 -0.0297 1.0000 0.0303
-8.000 -0.4636 0.06102 0.05623 -0.0459 1.0000 0.0273
-7.750 -0.4658 0.05625 0.05137 -0.0487 1.0000 0.0271
-7.500 -0.4660 0.05186 0.04682 -0.0504 1.0000 0.0269
-7.250 -0.4663 0.04748 0.04223 -0.0513 1.0000 0.0267
-7.000 -0.4655 0.04369 0.03819 -0.0509 1.0000 0.0265
-6.750 -0.4635 0.04036 0.03456 -0.0498 1.0000 0.0264
-6.500 -0.4548 0.03694 0.03074 -0.0493 0.9978 0.0264
-6.250 -0.4239 0.03280 0.02598 -0.0526 0.9876 0.0264
-6.000 -0.3908 0.02952 0.02211 -0.0551 0.9789 0.0267
-5.750 -0.3548 0.02684 0.01888 -0.0575 0.9718 0.0271
-5.500 -0.3219 0.02492 0.01672 -0.0591 0.9625 0.0282
-5.250 -0.2875 0.02364 0.01529 -0.0609 0.9540 0.0300
-5.000 -0.2532 0.02235 0.01378 -0.0623 0.9451 0.0322
-4.750 -0.2215 0.02108 0.01228 -0.0629 0.9347 0.0336
-4.500 -0.1901 0.01991 0.01107 -0.0637 0.9250 0.0352
-4.250 -0.1597 0.01902 0.01012 -0.0641 0.9146 0.0379
-4.000 -0.1315 0.01828 0.00923 -0.0640 0.9027 0.0418
-3.750 -0.1037 0.01756 0.00849 -0.0639 0.8913 0.0500
-3.500 -0.0761 0.01675 0.00770 -0.0637 0.8804 0.0660
-3.250 -0.0498 0.01600 0.00712 -0.0633 0.8687 0.1064
-3.000 -0.0247 0.01531 0.00683 -0.0630 0.8564 0.1858
-2.750 0.0007 0.01476 0.00656 -0.0625 0.8446 0.2662
-2.500 0.0264 0.01432 0.00631 -0.0619 0.8334 0.3384
-2.250 0.0515 0.01391 0.00613 -0.0611 0.8219 0.4197
-2.000 0.0760 0.01355 0.00599 -0.0601 0.8094 0.5045
-1.750 0.1000 0.01325 0.00590 -0.0587 0.7975 0.5871
-1.500 0.1234 0.01298 0.00580 -0.0570 0.7861 0.6673
-1.250 0.1462 0.01276 0.00571 -0.0550 0.7747 0.7446
-1.000 0.1699 0.01259 0.00562 -0.0531 0.7621 0.8192
-0.750 0.2013 0.01245 0.00547 -0.0528 0.7498 0.8930
-0.500 0.2457 0.01232 0.00520 -0.0556 0.7373 0.9625
-0.250 0.2830 0.01229 0.00499 -0.0573 0.7243 1.0000
0.000 0.3079 0.01236 0.00486 -0.0566 0.7117 1.0000
0.250 0.3331 0.01245 0.00479 -0.0560 0.6981 1.0000
0.500 0.3587 0.01254 0.00475 -0.0554 0.6843 1.0000
0.750 0.3845 0.01265 0.00471 -0.0549 0.6705 1.0000
1.000 0.4105 0.01276 0.00470 -0.0544 0.6567 1.0000
1.250 0.4366 0.01289 0.00470 -0.0539 0.6429 1.0000
1.500 0.4628 0.01302 0.00472 -0.0534 0.6292 1.0000
1.750 0.4890 0.01317 0.00476 -0.0529 0.6153 1.0000
2.000 0.5153 0.01332 0.00481 -0.0525 0.6015 1.0000
2.250 0.5416 0.01349 0.00488 -0.0520 0.5873 1.0000
2.500 0.5678 0.01367 0.00497 -0.0515 0.5731 1.0000
2.750 0.5940 0.01385 0.00507 -0.0511 0.5587 1.0000
3.000 0.6202 0.01405 0.00520 -0.0507 0.5439 1.0000
3.250 0.6464 0.01427 0.00537 -0.0503 0.5291 1.0000
3.500 0.6724 0.01449 0.00554 -0.0499 0.5143 1.0000
3.750 0.6984 0.01473 0.00573 -0.0495 0.4994 1.0000
4.000 0.7243 0.01498 0.00595 -0.0490 0.4845 1.0000
4.250 0.7501 0.01525 0.00618 -0.0486 0.4695 1.0000
4.500 0.7757 0.01553 0.00643 -0.0482 0.4543 1.0000
4.750 0.8012 0.01583 0.00670 -0.0477 0.4390 1.0000
5.000 0.8265 0.01614 0.00700 -0.0473 0.4234 1.0000
5.250 0.8516 0.01647 0.00731 -0.0468 0.4076 1.0000
5.500 0.8764 0.01682 0.00764 -0.0463 0.3918 1.0000
5.750 0.9011 0.01719 0.00802 -0.0458 0.3756 1.0000
6.000 0.9255 0.01758 0.00842 -0.0453 0.3593 1.0000
6.250 0.9496 0.01799 0.00884 -0.0448 0.3429 1.0000
6.500 0.9734 0.01843 0.00929 -0.0443 0.3265 1.0000
6.750 0.9968 0.01889 0.00978 -0.0437 0.3101 1.0000
7.000 1.0199 0.01939 0.01029 -0.0431 0.2939 1.0000
7.250 1.0425 0.01993 0.01084 -0.0424 0.2780 1.0000
7.500 1.0645 0.02050 0.01144 -0.0417 0.2622 1.0000
7.750 1.0862 0.02111 0.01206 -0.0410 0.2472 1.0000
8.000 1.1072 0.02176 0.01273 -0.0402 0.2322 1.0000
8.250 1.1278 0.02244 0.01345 -0.0394 0.2181 1.0000
8.500 1.1476 0.02317 0.01423 -0.0386 0.2041 1.0000
8.750 1.1668 0.02394 0.01504 -0.0376 0.1910 1.0000
9.000 1.1852 0.02476 0.01590 -0.0367 0.1785 1.0000
9.250 1.2025 0.02563 0.01681 -0.0356 0.1668 1.0000
9.500 1.2184 0.02658 0.01779 -0.0344 0.1562 1.0000
9.750 1.2340 0.02753 0.01883 -0.0332 0.1454 1.0000
10.000 1.2488 0.02853 0.01993 -0.0319 0.1358 1.0000
10.250 1.2608 0.02966 0.02108 -0.0304 0.1276 1.0000
10.500 1.2717 0.03078 0.02231 -0.0288 0.1195 1.0000
10.750 1.2800 0.03201 0.02361 -0.0269 0.1129 1.0000
11.000 1.2869 0.03333 0.02505 -0.0252 0.1065 1.0000
11.250 1.2929 0.03483 0.02662 -0.0235 0.1010 1.0000
11.500 1.2988 0.03639 0.02831 -0.0221 0.0954 1.0000
11.750 1.3012 0.03826 0.03018 -0.0208 0.0913 1.0000
12.000 1.3072 0.04008 0.03221 -0.0198 0.0864 1.0000
12.250 1.3096 0.04215 0.03439 -0.0190 0.0821 1.0000
12.500 1.3104 0.04449 0.03675 -0.0183 0.0786 1.0000
12.750 1.3129 0.04686 0.03936 -0.0179 0.0745 1.0000
13.000 1.3126 0.04951 0.04215 -0.0178 0.0709 1.0000
13.250 1.3096 0.05251 0.04514 -0.0179 0.0678 1.0000
13.500 1.3076 0.05572 0.04862 -0.0184 0.0639 1.0000
13.750 1.3031 0.05925 0.05230 -0.0193 0.0606 1.0000
14.000 1.2963 0.06316 0.05626 -0.0205 0.0579 1.0000
14.250 1.2900 0.06736 0.06065 -0.0219 0.0550 1.0000
14.500 1.2820 0.07192 0.06541 -0.0237 0.0521 1.0000
14.750 1.2730 0.07681 0.07042 -0.0258 0.0499 1.0000
15.000 1.2637 0.08184 0.07553 -0.0281 0.0482 1.0000
15.250 1.2537 0.08733 0.08118 -0.0306 0.0463 1.0000
15.500 1.2427 0.09326 0.08732 -0.0334 0.0445 1.0000
15.750 1.2313 0.09940 0.09364 -0.0365 0.0429 1.0000
16.000 1.2196 0.10579 0.10016 -0.0399 0.0414 1.0000
16.250 1.2089 0.11209 0.10653 -0.0434 0.0400 1.0000
16.500 1.1996 0.11816 0.11266 -0.0466 0.0388 1.0000
16.750 1.1837 0.12613 0.12086 -0.0510 0.0378 1.0000
17.000 1.1665 0.13471 0.12964 -0.0560 0.0370 1.0000
17.250 1.1461 0.14445 0.13956 -0.0617 0.0363 1.0000
17.500 1.1161 0.15735 0.15264 -0.0695 0.0362 1.0000
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