FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX S 03-182 AIRFOIL (fxs03182-il) Reynolds number: 50,000 Max Cl/Cd: 16.18 at α=12° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxs03182-il-50000-n5.txt Download as CSV file: xf-fxs03182-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX S 03-182 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.3714 0.11835 0.11188 -0.0678 1.0000 0.0350
-12.500 -0.3870 0.11470 0.10839 -0.0672 1.0000 0.0345
-12.250 -0.4086 0.11091 0.10473 -0.0661 1.0000 0.0344
-12.000 -0.4183 0.10349 0.09733 -0.0707 0.9952 0.0331
-11.750 -0.4354 0.09358 0.08739 -0.0785 0.9873 0.0322
-11.500 -0.4654 0.08348 0.07707 -0.0864 0.9786 0.0307
-11.250 -0.4948 0.07517 0.06839 -0.0924 0.9691 0.0296
-11.000 -0.5089 0.06994 0.06284 -0.0956 0.9587 0.0292
-10.750 -0.5118 0.06620 0.05890 -0.0980 0.9501 0.0299
-10.500 -0.5118 0.06281 0.05529 -0.1001 0.9418 0.0308
-10.250 -0.5141 0.05980 0.05201 -0.1008 0.9323 0.0314
-10.000 -0.5085 0.05669 0.04857 -0.1023 0.9258 0.0330
-9.750 -0.5088 0.05430 0.04586 -0.1012 0.9159 0.0341
-9.500 -0.4912 0.05101 0.04201 -0.1023 0.9112 0.0360
-9.250 -0.4775 0.04860 0.03907 -0.1009 0.9033 0.0380
-9.000 -0.4362 0.04605 0.03650 -0.1029 0.9009 0.0421
-8.750 -0.3971 0.04417 0.03437 -0.1044 0.8984 0.0520
-8.500 -0.3856 0.04334 0.03326 -0.1032 0.8907 0.0611
-8.250 -0.3582 0.04218 0.03200 -0.1036 0.8863 0.0742
-8.000 -0.3219 0.04110 0.03090 -0.1045 0.8835 0.0867
-7.750 -0.3096 0.04052 0.03032 -0.1024 0.8764 0.0953
-7.500 -0.2916 0.03967 0.02943 -0.1014 0.8712 0.1068
-7.250 -0.2798 0.03889 0.02862 -0.0997 0.8658 0.1172
-7.000 -0.2812 0.03835 0.02811 -0.0962 0.8582 0.1269
-6.750 -0.2760 0.03721 0.02709 -0.0943 0.8537 0.1470
-6.500 -0.2948 0.03700 0.02700 -0.0883 0.8446 0.1596
-6.250 -0.2992 0.03551 0.02589 -0.0857 0.8397 0.2022
-6.000 -0.3215 0.03511 0.02575 -0.0793 0.8310 0.2307
-5.750 -0.2874 0.03795 0.03022 -0.0730 0.8289 0.4826
-5.500 -0.2870 0.03748 0.02945 -0.0707 0.8248 0.5329
-5.250 -0.3140 0.03744 0.02941 -0.0638 0.8165 0.5515
-5.000 -0.3000 0.03836 0.03002 -0.0611 0.8128 0.5862
-4.500 -0.2798 0.04237 0.03376 -0.0501 0.8040 0.6479
-4.250 -0.2532 0.04451 0.03571 -0.0462 0.8012 0.6744
-4.000 -0.2295 0.04525 0.03623 -0.0443 0.7987 0.6911
-3.750 -0.2061 0.04523 0.03593 -0.0438 0.7965 0.7014
-3.500 -0.2349 0.04532 0.03602 -0.0362 0.7895 0.7119
-3.250 -0.2153 0.04550 0.03601 -0.0348 0.7863 0.7178
-3.000 -0.2053 0.04517 0.03550 -0.0333 0.7835 0.7269
-2.750 -0.1786 0.04516 0.03528 -0.0333 0.7817 0.7318
-2.500 -0.1990 0.04522 0.03530 -0.0275 0.7759 0.7400
-2.250 -0.1852 0.04528 0.03522 -0.0258 0.7724 0.7448
-2.000 -0.1678 0.04521 0.03497 -0.0250 0.7698 0.7506
-1.750 -0.1489 0.04500 0.03458 -0.0248 0.7676 0.7567
-1.500 -0.1456 0.04525 0.03476 -0.0219 0.7637 0.7611
-1.250 -0.1387 0.04529 0.03470 -0.0200 0.7597 0.7663
-1.000 -0.1224 0.04523 0.03449 -0.0197 0.7567 0.7709
-0.750 -0.1002 0.04530 0.03442 -0.0195 0.7545 0.7743
-0.500 -0.0744 0.04531 0.03430 -0.0201 0.7525 0.7779
-0.250 -0.0749 0.04560 0.03453 -0.0177 0.7475 0.7829
0.000 -0.0592 0.04578 0.03463 -0.0171 0.7442 0.7863
0.250 -0.0380 0.04596 0.03470 -0.0171 0.7414 0.7895
0.500 -0.0115 0.04608 0.03473 -0.0179 0.7390 0.7926
0.750 0.0019 0.04642 0.03500 -0.0174 0.7352 0.7960
1.000 0.0163 0.04677 0.03529 -0.0172 0.7311 0.7995
1.250 0.0369 0.04706 0.03552 -0.0170 0.7278 0.8022
1.500 0.0640 0.04729 0.03570 -0.0179 0.7251 0.8049
1.750 0.0817 0.04772 0.03609 -0.0178 0.7212 0.8078
2.000 0.0967 0.04822 0.03655 -0.0177 0.7163 0.8111
2.250 0.1225 0.04859 0.03689 -0.0187 0.7127 0.8143
2.500 0.1509 0.04891 0.03719 -0.0196 0.7100 0.8169
2.750 0.1604 0.04956 0.03785 -0.0185 0.7043 0.8199
3.000 0.1817 0.05008 0.03837 -0.0190 0.6998 0.8228
3.250 0.2114 0.05051 0.03880 -0.0205 0.6965 0.8261
3.500 0.2289 0.05117 0.03948 -0.0205 0.6916 0.8295
3.750 0.2445 0.05180 0.04015 -0.0201 0.6861 0.8327
4.000 0.2731 0.05222 0.04061 -0.0211 0.6823 0.8360
4.250 0.2905 0.05297 0.04139 -0.0213 0.6765 0.8395
4.500 0.3122 0.05364 0.04212 -0.0219 0.6706 0.8430
4.750 0.3416 0.05399 0.04254 -0.0227 0.6669 0.8464
5.000 0.3506 0.05488 0.04351 -0.0218 0.6589 0.8505
5.250 0.3779 0.05543 0.04413 -0.0228 0.6541 0.8549
5.500 0.3970 0.05617 0.04497 -0.0229 0.6480 0.8590
5.750 0.4148 0.05687 0.04577 -0.0227 0.6413 0.8633
6.000 0.4483 0.05721 0.04621 -0.0241 0.6375 0.8678
6.250 0.4566 0.05824 0.04734 -0.0233 0.6275 0.8728
6.500 0.4893 0.05835 0.04761 -0.0241 0.6232 0.8780
6.750 0.4976 0.05939 0.04876 -0.0233 0.6128 0.8842
7.000 0.5305 0.05949 0.04902 -0.0241 0.6086 0.8905
7.250 0.5369 0.06066 0.05034 -0.0231 0.5979 0.8978
7.750 0.5797 0.06165 0.05167 -0.0232 0.5820 0.9140
8.000 0.5937 0.06235 0.05254 -0.0227 0.5713 0.9240
8.250 0.6302 0.06205 0.05248 -0.0238 0.5656 0.9368
8.500 0.6447 0.06298 0.05361 -0.0241 0.5534 0.9550
8.750 0.6620 0.06352 0.05434 -0.0246 0.5411 1.0000
9.000 0.6854 0.06410 0.05509 -0.0256 0.5292 1.0000
9.500 0.7488 0.06387 0.05529 -0.0279 0.5088 1.0000
9.750 0.7715 0.06412 0.05572 -0.0284 0.4949 1.0000
10.000 0.7948 0.06425 0.05606 -0.0287 0.4809 1.0000
10.250 0.8204 0.06396 0.05597 -0.0289 0.4663 1.0000
10.500 0.8475 0.06332 0.05559 -0.0289 0.4513 1.0000
10.750 0.8607 0.06398 0.05643 -0.0285 0.4308 1.0000
11.000 0.8869 0.06313 0.05579 -0.0281 0.4126 1.0000
11.250 0.9171 0.06178 0.05462 -0.0275 0.3920 1.0000
11.500 0.9386 0.06133 0.05426 -0.0267 0.3605 1.0000
11.750 0.9648 0.06028 0.05308 -0.0256 0.3193 1.0000
12.000 0.9814 0.06066 0.05325 -0.0247 0.2779 1.0000
12.250 0.9878 0.06256 0.05496 -0.0241 0.2418 1.0000
12.500 0.9920 0.06485 0.05705 -0.0236 0.2118 1.0000
12.750 0.9945 0.06750 0.05954 -0.0233 0.1860 1.0000
13.000 0.9970 0.07024 0.06213 -0.0231 0.1655 1.0000
13.250 1.0004 0.07302 0.06482 -0.0230 0.1473 1.0000
13.500 1.0044 0.07579 0.06751 -0.0230 0.1319 1.0000
13.750 1.0083 0.07864 0.07032 -0.0231 0.1181 1.0000
14.000 1.0115 0.08165 0.07332 -0.0235 0.1057 1.0000
14.250 1.0142 0.08470 0.07631 -0.0241 0.0959 1.0000
14.500 1.0204 0.08750 0.07929 -0.0245 0.0868 1.0000
14.750 1.0282 0.08999 0.08179 -0.0247 0.0808 1.0000
15.000 1.0379 0.09244 0.08447 -0.0249 0.0747 1.0000
15.250 1.0462 0.09485 0.08687 -0.0252 0.0702 1.0000
15.500 1.0535 0.09778 0.09008 -0.0258 0.0654 1.0000
15.750 1.0584 0.10082 0.09325 -0.0266 0.0613 1.0000
16.000 1.0631 0.10380 0.09621 -0.0275 0.0576 1.0000
16.250 1.0639 0.10788 0.10067 -0.0287 0.0542 1.0000
16.500 1.0631 0.11204 0.10506 -0.0303 0.0512 1.0000
16.750 1.0633 0.11586 0.10897 -0.0320 0.0483 1.0000
17.000 1.0652 0.11951 0.11265 -0.0334 0.0460 1.0000
17.250 1.0570 0.12552 0.11905 -0.0362 0.0445 1.0000
17.500 1.0469 0.13205 0.12590 -0.0395 0.0434 1.0000
17.750 1.0332 0.13961 0.13373 -0.0438 0.0425 1.0000
18.000 1.0155 0.14851 0.14288 -0.0490 0.0424 1.0000
18.250 0.9922 0.15973 0.15429 -0.0558 0.0433 1.0000
18.500 0.9700 0.17179 0.16642 -0.0630 0.0446 1.0000
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