S1012 (s1012-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: S1012 (s1012-il) Reynolds number: 500,000 Max Cl/Cd: 53.5 at α=8.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s1012-il-500000.txt Download as CSV file: xf-s1012-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: S1012
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.9917 0.11846 0.11553 -0.0108 1.0000 0.0197
-18.000 -1.0230 0.10720 0.10409 -0.0180 1.0000 0.0196
-17.750 -1.0500 0.09740 0.09412 -0.0242 1.0000 0.0196
-17.500 -1.0740 0.08840 0.08494 -0.0300 1.0000 0.0196
-17.250 -1.0990 0.07974 0.07609 -0.0354 1.0000 0.0197
-17.000 -1.1188 0.07241 0.06859 -0.0398 1.0000 0.0197
-16.750 -1.1383 0.06563 0.06163 -0.0435 1.0000 0.0198
-16.500 -1.1521 0.06018 0.05603 -0.0462 1.0000 0.0200
-16.250 -1.1642 0.05534 0.05106 -0.0481 1.0000 0.0202
-16.000 -1.1721 0.05143 0.04703 -0.0493 1.0000 0.0205
-15.750 -1.1765 0.04822 0.04374 -0.0500 1.0000 0.0208
-15.500 -1.1780 0.04553 0.04097 -0.0502 1.0000 0.0211
-15.250 -1.1791 0.04302 0.03836 -0.0501 1.0000 0.0214
-15.000 -1.1780 0.04087 0.03612 -0.0497 1.0000 0.0219
-14.750 -1.1777 0.03870 0.03382 -0.0490 1.0000 0.0223
-14.500 -1.1745 0.03687 0.03188 -0.0482 1.0000 0.0228
-14.250 -1.1708 0.03514 0.03002 -0.0471 1.0000 0.0232
-14.000 -1.1655 0.03359 0.02834 -0.0460 1.0000 0.0236
-13.750 -1.1582 0.03226 0.02686 -0.0447 1.0000 0.0240
-13.500 -1.1591 0.03003 0.02453 -0.0428 1.0000 0.0247
-13.250 -1.1530 0.02862 0.02308 -0.0413 1.0000 0.0255
-13.000 -1.1432 0.02756 0.02196 -0.0399 1.0000 0.0260
-12.750 -1.1323 0.02658 0.02093 -0.0385 1.0000 0.0268
-12.500 -1.1198 0.02574 0.02002 -0.0371 1.0000 0.0277
-12.250 -1.1067 0.02490 0.01908 -0.0357 1.0000 0.0286
-12.000 -1.0924 0.02416 0.01822 -0.0344 1.0000 0.0292
-11.750 -1.0849 0.02273 0.01674 -0.0323 1.0000 0.0304
-11.500 -1.0717 0.02192 0.01592 -0.0307 1.0000 0.0315
-11.250 -1.0562 0.02129 0.01526 -0.0294 1.0000 0.0327
-11.000 -1.0397 0.02071 0.01462 -0.0281 1.0000 0.0342
-10.750 -1.0215 0.02028 0.01411 -0.0269 1.0000 0.0354
-10.500 -1.0116 0.01932 0.01314 -0.0247 1.0000 0.0373
-10.250 -0.9811 0.01870 0.01252 -0.0262 0.9844 0.0396
-10.000 -0.9488 0.01817 0.01192 -0.0278 0.9743 0.0420
-9.750 -0.9214 0.01736 0.01104 -0.0286 0.9643 0.0446
-9.500 -0.8967 0.01686 0.01052 -0.0286 0.9550 0.0472
-9.250 -0.8749 0.01656 0.01016 -0.0278 0.9462 0.0498
-9.000 -0.8543 0.01622 0.00972 -0.0267 0.9394 0.0521
-8.750 -0.8367 0.01564 0.00916 -0.0252 0.9328 0.0553
-8.500 -0.8156 0.01536 0.00882 -0.0242 0.9278 0.0582
-8.250 -0.7928 0.01514 0.00853 -0.0234 0.9235 0.0608
-8.000 -0.7735 0.01460 0.00799 -0.0221 0.9188 0.0648
-7.750 -0.7511 0.01432 0.00770 -0.0213 0.9151 0.0686
-7.500 -0.7274 0.01415 0.00745 -0.0206 0.9121 0.0719
-7.250 -0.7065 0.01368 0.00701 -0.0196 0.9091 0.0769
-7.000 -0.6824 0.01342 0.00675 -0.0192 0.9063 0.0817
-6.750 -0.6585 0.01316 0.00644 -0.0186 0.9036 0.0862
-6.500 -0.6358 0.01281 0.00613 -0.0179 0.9010 0.0926
-6.250 -0.6107 0.01265 0.00592 -0.0174 0.8988 0.0978
-6.000 -0.5886 0.01229 0.00562 -0.0165 0.8964 0.1060
-5.750 -0.5639 0.01209 0.00539 -0.0161 0.8942 0.1136
-5.500 -0.5394 0.01181 0.00517 -0.0156 0.8921 0.1236
-5.250 -0.5149 0.01154 0.00496 -0.0152 0.8900 0.1344
-5.000 -0.4902 0.01130 0.00477 -0.0148 0.8880 0.1475
-4.750 -0.4657 0.01105 0.00458 -0.0143 0.8861 0.1634
-4.500 -0.4413 0.01080 0.00441 -0.0138 0.8841 0.1827
-4.250 -0.4175 0.01052 0.00424 -0.0132 0.8822 0.2077
-4.000 -0.3941 0.01022 0.00409 -0.0126 0.8805 0.2421
-3.750 -0.3711 0.00989 0.00395 -0.0119 0.8789 0.2877
-3.500 -0.3490 0.00944 0.00379 -0.0112 0.8768 0.3509
-3.250 -0.3291 0.00889 0.00361 -0.0100 0.8744 0.4366
-3.000 -0.3113 0.00824 0.00343 -0.0084 0.8721 0.5426
-2.750 -0.2943 0.00770 0.00347 -0.0062 0.8697 0.6689
-2.500 -0.2690 0.00776 0.00366 -0.0054 0.8679 0.7240
-2.250 -0.2419 0.00786 0.00376 -0.0050 0.8662 0.7456
-2.000 -0.2148 0.00800 0.00389 -0.0046 0.8645 0.7611
-1.750 -0.1873 0.00813 0.00401 -0.0044 0.8625 0.7728
-1.500 -0.1598 0.00825 0.00412 -0.0042 0.8600 0.7833
-1.250 -0.1321 0.00832 0.00422 -0.0040 0.8568 0.7904
-1.000 -0.1053 0.00836 0.00422 -0.0034 0.8524 0.7983
-0.750 -0.0793 0.00834 0.00418 -0.0024 0.8456 0.8046
-0.500 -0.0535 0.00822 0.00404 -0.0013 0.8356 0.8106
-0.250 -0.0272 0.00819 0.00395 -0.0006 0.8279 0.8167
0.000 0.0000 0.00816 0.00396 0.0000 0.8217 0.8217
0.250 0.0272 0.00819 0.00396 0.0006 0.8168 0.8279
0.500 0.0535 0.00822 0.00404 0.0013 0.8106 0.8356
0.750 0.0793 0.00833 0.00418 0.0024 0.8045 0.8456
1.000 0.1054 0.00836 0.00422 0.0034 0.7984 0.8524
1.250 0.1321 0.00833 0.00422 0.0040 0.7905 0.8568
1.500 0.1598 0.00825 0.00412 0.0042 0.7833 0.8600
1.750 0.1872 0.00813 0.00401 0.0044 0.7728 0.8625
2.000 0.2147 0.00800 0.00388 0.0046 0.7609 0.8645
2.250 0.2419 0.00786 0.00376 0.0050 0.7457 0.8662
2.500 0.2690 0.00776 0.00366 0.0054 0.7240 0.8679
2.750 0.2944 0.00770 0.00347 0.0062 0.6701 0.8697
3.000 0.3113 0.00824 0.00343 0.0084 0.5431 0.8721
3.250 0.3290 0.00889 0.00361 0.0100 0.4363 0.8744
3.500 0.3490 0.00944 0.00379 0.0112 0.3502 0.8768
3.750 0.3711 0.00988 0.00395 0.0119 0.2878 0.8789
4.000 0.3941 0.01022 0.00409 0.0126 0.2423 0.8805
4.250 0.4175 0.01052 0.00424 0.0132 0.2078 0.8822
4.500 0.4413 0.01080 0.00441 0.0138 0.1827 0.8841
4.750 0.4657 0.01105 0.00458 0.0143 0.1633 0.8861
5.000 0.4902 0.01130 0.00477 0.0148 0.1474 0.8880
5.250 0.5149 0.01154 0.00496 0.0152 0.1344 0.8900
5.500 0.5394 0.01181 0.00517 0.0156 0.1235 0.8921
5.750 0.5639 0.01209 0.00539 0.0161 0.1136 0.8942
6.000 0.5885 0.01229 0.00562 0.0165 0.1059 0.8964
6.250 0.6108 0.01265 0.00592 0.0174 0.0978 0.8988
6.500 0.6358 0.01281 0.00613 0.0179 0.0926 0.9010
6.750 0.6586 0.01315 0.00644 0.0186 0.0863 0.9036
7.000 0.6823 0.01343 0.00675 0.0192 0.0817 0.9063
7.250 0.7065 0.01368 0.00700 0.0197 0.0768 0.9091
7.500 0.7275 0.01414 0.00745 0.0206 0.0719 0.9121
7.750 0.7511 0.01432 0.00770 0.0213 0.0686 0.9151
8.000 0.7735 0.01460 0.00799 0.0222 0.0649 0.9188
8.250 0.7926 0.01515 0.00854 0.0234 0.0609 0.9235
8.500 0.8157 0.01536 0.00883 0.0241 0.0582 0.9278
8.750 0.8367 0.01564 0.00916 0.0252 0.0554 0.9328
9.000 0.8544 0.01621 0.00972 0.0267 0.0521 0.9393
9.250 0.8753 0.01655 0.01014 0.0278 0.0497 0.9461
9.500 0.8970 0.01685 0.01051 0.0286 0.0472 0.9549
9.750 0.9217 0.01735 0.01103 0.0286 0.0445 0.9643
10.000 0.9490 0.01817 0.01191 0.0278 0.0420 0.9743
10.250 0.9813 0.01871 0.01252 0.0262 0.0396 0.9844
10.500 1.0117 0.01932 0.01315 0.0247 0.0374 1.0000
10.750 1.0214 0.02031 0.01414 0.0269 0.0354 1.0000
11.000 1.0398 0.02072 0.01463 0.0281 0.0342 1.0000
11.250 1.0563 0.02130 0.01527 0.0293 0.0328 1.0000
11.500 1.0719 0.02193 0.01593 0.0307 0.0316 1.0000
11.750 1.0852 0.02272 0.01674 0.0322 0.0305 1.0000
12.000 1.0925 0.02418 0.01823 0.0344 0.0293 1.0000
12.250 1.1071 0.02490 0.01908 0.0357 0.0285 1.0000
12.500 1.1203 0.02571 0.01999 0.0371 0.0276 1.0000
12.750 1.1322 0.02664 0.02099 0.0385 0.0269 1.0000
13.000 1.1440 0.02752 0.02192 0.0398 0.0260 1.0000
13.250 1.1533 0.02863 0.02308 0.0412 0.0254 1.0000
13.500 1.1592 0.03006 0.02456 0.0428 0.0247 1.0000
13.750 1.1592 0.03220 0.02680 0.0446 0.0240 1.0000
14.000 1.1663 0.03357 0.02831 0.0459 0.0237 1.0000
14.250 1.1712 0.03518 0.03006 0.0470 0.0233 1.0000
14.500 1.1754 0.03684 0.03185 0.0481 0.0227 1.0000
14.750 1.1781 0.03872 0.03384 0.0489 0.0223 1.0000
15.000 1.1799 0.04073 0.03596 0.0496 0.0218 1.0000
15.250 1.1796 0.04304 0.03838 0.0500 0.0215 1.0000
15.500 1.1804 0.04532 0.04073 0.0501 0.0210 1.0000
15.750 1.1785 0.04804 0.04354 0.0499 0.0207 1.0000
16.000 1.1740 0.05128 0.04687 0.0493 0.0204 1.0000
16.250 1.1650 0.05531 0.05103 0.0480 0.0202 1.0000
16.500 1.1531 0.06011 0.05595 0.0461 0.0199 1.0000
16.750 1.1383 0.06573 0.06174 0.0434 0.0198 1.0000
17.000 1.1193 0.07244 0.06862 0.0397 0.0197 1.0000
17.250 1.0978 0.08009 0.07645 0.0350 0.0196 1.0000
17.500 1.0764 0.08817 0.08471 0.0299 0.0196 1.0000
17.750 1.0516 0.09720 0.09391 0.0242 0.0196 1.0000
18.000 1.0200 0.10799 0.10489 0.0173 0.0196 1.0000
18.250 0.9916 0.11867 0.11574 0.0106 0.0197 1.0000
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