S1014 (s1014-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1014 (s1014-il) Reynolds number: 200,000 Max Cl/Cd: 30.33 at α=9.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1014-il-200000-n5.txt Download as CSV file: xf-s1014-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1014
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.8752 0.13774 0.13360 -0.0204 1.0000 0.0281
-19.500 -0.9217 0.12346 0.11904 -0.0290 1.0000 0.0282
-19.250 -0.9478 0.11401 0.10938 -0.0347 1.0000 0.0284
-19.000 -0.9677 0.10612 0.10129 -0.0394 1.0000 0.0286
-18.750 -0.9824 0.09943 0.09445 -0.0434 1.0000 0.0289
-18.500 -0.9918 0.09394 0.08888 -0.0465 1.0000 0.0293
-18.250 -1.0010 0.08854 0.08337 -0.0495 1.0000 0.0296
-18.000 -1.0095 0.08339 0.07811 -0.0523 1.0000 0.0301
-17.750 -1.0166 0.07862 0.07322 -0.0548 1.0000 0.0306
-17.500 -1.0226 0.07415 0.06863 -0.0570 1.0000 0.0310
-17.250 -1.0274 0.07000 0.06435 -0.0588 1.0000 0.0316
-16.750 -1.0335 0.06272 0.05674 -0.0618 0.9473 0.0330
-16.500 -1.0294 0.05930 0.05305 -0.0641 0.9293 0.0339
-16.250 -1.0270 0.05636 0.04999 -0.0652 0.9174 0.0346
-16.000 -1.0248 0.05374 0.04726 -0.0659 0.9085 0.0354
-15.750 -1.0220 0.05136 0.04475 -0.0661 0.9016 0.0363
-15.500 -1.0180 0.04922 0.04247 -0.0661 0.8958 0.0374
-15.250 -1.0128 0.04723 0.04032 -0.0660 0.8911 0.0385
-15.000 -1.0060 0.04542 0.03833 -0.0657 0.8870 0.0397
-14.750 -1.0004 0.04360 0.03643 -0.0652 0.8833 0.0408
-14.500 -0.9944 0.04192 0.03468 -0.0647 0.8802 0.0419
-14.000 -0.9763 0.03910 0.03164 -0.0636 0.8750 0.0449
-13.750 -0.9649 0.03787 0.03026 -0.0630 0.8726 0.0468
-13.500 -0.9562 0.03651 0.02887 -0.0622 0.8702 0.0483
-13.250 -0.9458 0.03534 0.02765 -0.0614 0.8679 0.0499
-13.000 -0.9341 0.03430 0.02651 -0.0606 0.8658 0.0519
-12.750 -0.9206 0.03338 0.02546 -0.0598 0.8640 0.0542
-12.500 -0.9089 0.03237 0.02439 -0.0588 0.8622 0.0562
-12.250 -0.8967 0.03142 0.02340 -0.0579 0.8606 0.0584
-12.000 -0.8819 0.03059 0.02251 -0.0572 0.8590 0.0611
-11.750 -0.8652 0.02986 0.02165 -0.0565 0.8573 0.0638
-11.500 -0.8521 0.02894 0.02074 -0.0556 0.8557 0.0664
-11.250 -0.8367 0.02819 0.01996 -0.0548 0.8541 0.0695
-11.000 -0.8198 0.02754 0.01923 -0.0540 0.8524 0.0729
-10.750 -0.8043 0.02682 0.01847 -0.0531 0.8507 0.0760
-10.500 -0.7889 0.02613 0.01777 -0.0521 0.8492 0.0797
-10.250 -0.7714 0.02557 0.01713 -0.0513 0.8479 0.0837
-10.000 -0.7545 0.02497 0.01649 -0.0504 0.8467 0.0875
-9.750 -0.7385 0.02436 0.01588 -0.0494 0.8456 0.0920
-9.500 -0.7200 0.02387 0.01532 -0.0486 0.8446 0.0970
-9.250 -0.7027 0.02328 0.01475 -0.0478 0.8434 0.1018
-9.000 -0.6845 0.02277 0.01423 -0.0470 0.8422 0.1077
-8.750 -0.6659 0.02229 0.01373 -0.0462 0.8411 0.1137
-8.500 -0.6483 0.02177 0.01324 -0.0454 0.8399 0.1206
-8.250 -0.6293 0.02134 0.01278 -0.0446 0.8388 0.1275
-8.000 -0.6116 0.02086 0.01234 -0.0436 0.8376 0.1357
-7.750 -0.5933 0.02042 0.01191 -0.0427 0.8365 0.1446
-7.500 -0.5750 0.02000 0.01151 -0.0418 0.8353 0.1551
-7.250 -0.5579 0.01955 0.01110 -0.0407 0.8340 0.1665
-7.000 -0.5408 0.01912 0.01071 -0.0395 0.8327 0.1793
-6.750 -0.5239 0.01869 0.01033 -0.0382 0.8316 0.1946
-6.500 -0.5078 0.01825 0.00996 -0.0369 0.8306 0.2122
-6.250 -0.4925 0.01781 0.00960 -0.0353 0.8297 0.2334
-6.000 -0.4788 0.01734 0.00924 -0.0335 0.8288 0.2574
-5.500 -0.4575 0.01641 0.00862 -0.0290 0.8262 0.3202
-5.250 -0.4529 0.01600 0.00841 -0.0255 0.8244 0.3576
-5.000 -0.4503 0.01561 0.00825 -0.0215 0.8222 0.4007
-4.750 -0.4460 0.01517 0.00809 -0.0177 0.8205 0.4545
-4.500 -0.4392 0.01475 0.00804 -0.0141 0.8190 0.5214
-4.250 -0.4093 0.01505 0.00891 -0.0136 0.8183 0.6091
-4.000 -0.3512 0.01643 0.01048 -0.0173 0.8185 0.6550
-3.750 -0.3353 0.01664 0.01066 -0.0151 0.8170 0.6781
-3.250 -0.3139 0.01656 0.01043 -0.0095 0.8139 0.7113
-3.000 -0.2889 0.01689 0.01071 -0.0088 0.8131 0.7198
-2.750 -0.2724 0.01694 0.01068 -0.0069 0.8119 0.7305
-2.500 -0.2437 0.01748 0.01124 -0.0070 0.8100 0.7359
-2.250 -0.2307 0.01762 0.01132 -0.0048 0.8075 0.7459
-2.000 -0.1980 0.01823 0.01196 -0.0052 0.8059 0.7501
-1.750 -0.1743 0.01865 0.01237 -0.0043 0.8040 0.7582
-1.500 -0.1469 0.01915 0.01288 -0.0038 0.8024 0.7653
-1.250 -0.1140 0.01971 0.01345 -0.0041 0.8010 0.7704
-1.000 -0.1001 0.01963 0.01333 -0.0019 0.7989 0.7792
-0.750 -0.0683 0.01988 0.01357 -0.0023 0.7977 0.7811
-0.500 -0.0386 0.02000 0.01370 -0.0025 0.7966 0.7831
-0.250 -0.0104 0.02005 0.01373 -0.0024 0.7954 0.7854
0.000 0.0000 0.02033 0.01405 0.0000 0.7894 0.7894
0.250 0.0104 0.02005 0.01373 0.0024 0.7854 0.7954
0.500 0.0386 0.02000 0.01370 0.0025 0.7831 0.7966
0.750 0.0683 0.01988 0.01357 0.0023 0.7811 0.7977
1.000 0.1001 0.01963 0.01332 0.0019 0.7792 0.7989
1.250 0.1140 0.01971 0.01345 0.0041 0.7704 0.8010
1.500 0.1469 0.01915 0.01288 0.0038 0.7653 0.8024
1.750 0.1744 0.01865 0.01237 0.0043 0.7583 0.8040
2.000 0.1979 0.01823 0.01196 0.0052 0.7502 0.8059
2.250 0.2307 0.01761 0.01132 0.0048 0.7459 0.8075
2.500 0.2437 0.01749 0.01124 0.0070 0.7360 0.8100
2.750 0.2724 0.01694 0.01068 0.0069 0.7305 0.8119
3.000 0.2889 0.01689 0.01072 0.0088 0.7198 0.8131
3.250 0.3134 0.01657 0.01045 0.0096 0.7110 0.8139
3.750 0.3351 0.01664 0.01066 0.0152 0.6779 0.8170
4.000 0.3514 0.01643 0.01048 0.0173 0.6549 0.8185
4.250 0.4094 0.01505 0.00890 0.0135 0.6088 0.8183
4.500 0.4394 0.01475 0.00804 0.0141 0.5224 0.8190
4.750 0.4461 0.01517 0.00808 0.0177 0.4547 0.8205
5.000 0.4504 0.01561 0.00824 0.0215 0.4009 0.8222
5.250 0.4530 0.01600 0.00841 0.0255 0.3575 0.8244
5.500 0.4576 0.01640 0.00862 0.0290 0.3206 0.8262
5.750 0.4666 0.01686 0.00890 0.0315 0.2869 0.8276
6.000 0.4789 0.01734 0.00924 0.0335 0.2575 0.8288
6.250 0.4926 0.01781 0.00960 0.0353 0.2331 0.8297
6.500 0.5080 0.01824 0.00996 0.0369 0.2125 0.8307
6.750 0.5240 0.01869 0.01033 0.0382 0.1943 0.8316
7.000 0.5409 0.01911 0.01071 0.0395 0.1791 0.8327
7.250 0.5581 0.01954 0.01110 0.0406 0.1664 0.8340
7.500 0.5752 0.02000 0.01150 0.0418 0.1550 0.8354
7.750 0.5935 0.02042 0.01190 0.0427 0.1446 0.8365
8.000 0.6119 0.02085 0.01233 0.0436 0.1359 0.8376
8.250 0.6295 0.02134 0.01278 0.0445 0.1275 0.8388
8.500 0.6486 0.02177 0.01323 0.0453 0.1203 0.8399
8.750 0.6661 0.02228 0.01372 0.0462 0.1136 0.8411
9.000 0.6849 0.02276 0.01422 0.0469 0.1077 0.8423
9.250 0.7030 0.02328 0.01474 0.0477 0.1018 0.8434
9.500 0.7203 0.02386 0.01531 0.0485 0.0969 0.8446
9.750 0.7388 0.02436 0.01587 0.0493 0.0920 0.8456
10.000 0.7550 0.02496 0.01648 0.0503 0.0876 0.8467
10.250 0.7719 0.02555 0.01711 0.0512 0.0836 0.8479
10.500 0.7893 0.02613 0.01776 0.0521 0.0795 0.8492
10.750 0.8047 0.02682 0.01846 0.0530 0.0759 0.8507
11.000 0.8204 0.02752 0.01920 0.0539 0.0727 0.8525
11.250 0.8373 0.02817 0.01994 0.0547 0.0694 0.8541
11.500 0.8525 0.02893 0.02073 0.0555 0.0664 0.8558
11.750 0.8661 0.02982 0.02162 0.0564 0.0636 0.8574
12.000 0.8825 0.03057 0.02249 0.0571 0.0609 0.8590
12.250 0.8974 0.03139 0.02338 0.0578 0.0583 0.8607
12.500 0.9096 0.03235 0.02437 0.0587 0.0561 0.8623
12.750 0.9215 0.03335 0.02543 0.0597 0.0540 0.8640
13.000 0.9348 0.03428 0.02649 0.0605 0.0519 0.8659
13.250 0.9466 0.03531 0.02762 0.0613 0.0499 0.8680
13.500 0.9567 0.03650 0.02885 0.0622 0.0481 0.8702
13.750 0.9658 0.03783 0.03023 0.0629 0.0467 0.8727
14.000 0.9774 0.03905 0.03159 0.0635 0.0448 0.8752
14.500 0.9954 0.04188 0.03463 0.0646 0.0418 0.8804
14.750 1.0015 0.04354 0.03637 0.0651 0.0408 0.8835
15.000 1.0072 0.04536 0.03827 0.0655 0.0397 0.8872
15.250 1.0140 0.04717 0.04027 0.0658 0.0385 0.8914
15.500 1.0193 0.04916 0.04240 0.0660 0.0374 0.8961
15.750 1.0233 0.05131 0.04470 0.0660 0.0363 0.9019
16.000 1.0265 0.05365 0.04716 0.0658 0.0355 0.9090
16.250 1.0286 0.05629 0.04991 0.0651 0.0345 0.9182
16.500 1.0313 0.05927 0.05304 0.0638 0.0338 0.9306
16.750 1.0359 0.06266 0.05669 0.0615 0.0330 0.9495
17.250 1.0293 0.06990 0.06424 0.0586 0.0315 1.0000
17.500 1.0248 0.07400 0.06847 0.0568 0.0311 1.0000
17.750 1.0188 0.07848 0.07307 0.0546 0.0305 1.0000
18.000 1.0117 0.08325 0.07796 0.0522 0.0300 1.0000
18.250 1.0031 0.08841 0.08323 0.0494 0.0296 1.0000
18.500 0.9939 0.09379 0.08873 0.0464 0.0293 1.0000
18.750 0.9848 0.09923 0.09423 0.0432 0.0289 1.0000
19.000 0.9706 0.10581 0.10096 0.0394 0.0286 1.0000
19.250 0.9490 0.11410 0.10947 0.0344 0.0283 1.0000
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