WORTMANN FX 2 AIRFOIL (fx2-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 2 AIRFOIL (fx2-il) Reynolds number: 100,000 Max Cl/Cd: 22.71 at α=11° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx2-il-100000-n5.txt Download as CSV file: xf-fx2-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 2 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-16.000 -0.1599 0.11369 0.10745 -0.1659 0.8963 0.0340
-15.750 -0.3055 0.08209 0.07561 -0.1789 0.8959 0.0313
-15.500 -0.3450 0.07484 0.06811 -0.1810 0.8950 0.0310
-15.250 -0.3668 0.07051 0.06361 -0.1816 0.8941 0.0311
-15.000 -0.3841 0.06701 0.05994 -0.1814 0.8930 0.0313
-14.750 -0.3959 0.06429 0.05709 -0.1810 0.8919 0.0317
-14.500 -0.4065 0.06178 0.05443 -0.1802 0.8907 0.0322
-14.250 -0.4157 0.05958 0.05208 -0.1792 0.8897 0.0328
-14.000 -0.4248 0.05749 0.04981 -0.1778 0.8888 0.0336
-13.750 -0.4325 0.05559 0.04771 -0.1762 0.8880 0.0346
-13.500 -0.4380 0.05365 0.04552 -0.1745 0.8872 0.0356
-13.250 -0.4483 0.05234 0.04396 -0.1712 0.8861 0.0366
-13.000 -0.4620 0.05172 0.04321 -0.1664 0.8846 0.0373
-12.750 -0.4755 0.05165 0.04316 -0.1612 0.8828 0.0378
-12.500 -0.4888 0.05152 0.04303 -0.1559 0.8803 0.0384
-12.250 -0.5015 0.05138 0.04286 -0.1508 0.8786 0.0390
-12.000 -0.5117 0.05112 0.04256 -0.1460 0.8771 0.0398
-11.750 -0.5222 0.05086 0.04223 -0.1412 0.8757 0.0407
-11.500 -0.5300 0.05046 0.04172 -0.1367 0.8745 0.0423
-11.250 -0.5266 0.04968 0.04069 -0.1340 0.8734 0.0446
-11.000 -0.5154 0.04887 0.03987 -0.1327 0.8726 0.0467
-10.750 -0.5033 0.04816 0.03911 -0.1315 0.8718 0.0491
-10.500 -0.5754 0.04972 0.04073 -0.1147 0.8681 0.0469
-10.250 -0.5908 0.04959 0.04061 -0.1086 0.8661 0.0479
-10.000 -0.5938 0.04917 0.04013 -0.1046 0.8642 0.0497
-9.750 -0.5932 0.04872 0.03957 -0.1010 0.8630 0.0523
-9.500 -0.5899 0.04824 0.03897 -0.0978 0.8620 0.0551
-9.250 -0.5871 0.04772 0.03847 -0.0948 0.8609 0.0578
-9.000 -0.5769 0.04717 0.03786 -0.0929 0.8596 0.0614
-8.750 -0.5644 0.04668 0.03717 -0.0912 0.8584 0.0658
-8.500 -0.5514 0.04603 0.03662 -0.0896 0.8576 0.0703
-8.250 -0.5414 0.04558 0.03614 -0.0877 0.8568 0.0748
-8.000 -0.5621 0.04541 0.03594 -0.0804 0.8541 0.0761
-7.750 -0.5775 0.04510 0.03557 -0.0740 0.8511 0.0781
-7.500 -0.5823 0.04471 0.03511 -0.0693 0.8490 0.0807
-7.250 -0.5861 0.04402 0.03448 -0.0651 0.8465 0.0843
-7.000 -0.5834 0.04344 0.03386 -0.0619 0.8445 0.0888
-6.750 -0.5744 0.04296 0.03329 -0.0597 0.8431 0.0941
-6.500 -0.5631 0.04230 0.03267 -0.0582 0.8417 0.1000
-6.250 -0.5683 0.04175 0.03210 -0.0536 0.8381 0.1039
-6.000 -0.5707 0.04127 0.03157 -0.0495 0.8351 0.1084
-5.750 -0.5642 0.04067 0.03102 -0.0469 0.8323 0.1153
-5.500 -0.5508 0.04010 0.03047 -0.0454 0.8298 0.1273
-5.250 -0.5346 0.03946 0.02992 -0.0445 0.8279 0.1493
-5.000 -0.5188 0.03859 0.02931 -0.0439 0.8265 0.1953
-4.750 -0.5070 0.03664 0.02824 -0.0438 0.8252 0.3392
-4.500 -0.5183 0.03618 0.02871 -0.0372 0.8194 0.4600
-4.250 -0.5039 0.03742 0.03024 -0.0332 0.8164 0.5588
-4.000 -0.4818 0.03838 0.03115 -0.0315 0.8142 0.5852
-3.750 -0.4545 0.03906 0.03167 -0.0315 0.8122 0.6085
-3.500 -0.4251 0.04046 0.03294 -0.0308 0.8105 0.6299
-3.250 -0.4109 0.04125 0.03361 -0.0285 0.8067 0.6475
-3.000 -0.4002 0.04215 0.03446 -0.0251 0.8025 0.6591
-2.750 -0.3791 0.04278 0.03497 -0.0238 0.7995 0.6693
-2.500 -0.3532 0.04322 0.03525 -0.0238 0.7972 0.6809
-2.250 -0.3286 0.04416 0.03614 -0.0220 0.7955 0.6870
-1.750 -0.3029 0.04472 0.03656 -0.0174 0.7871 0.7010
-1.500 -0.2801 0.04484 0.03657 -0.0171 0.7841 0.7070
-1.250 -0.2521 0.04471 0.03631 -0.0185 0.7821 0.7122
-1.000 -0.2237 0.04479 0.03629 -0.0190 0.7805 0.7140
-0.750 -0.2140 0.04477 0.03623 -0.0168 0.7750 0.7163
-0.500 -0.1932 0.04472 0.03610 -0.0167 0.7713 0.7185
-0.250 -0.1659 0.04468 0.03596 -0.0176 0.7688 0.7212
0.000 -0.1339 0.04458 0.03575 -0.0196 0.7670 0.7242
0.250 -0.0985 0.04446 0.03551 -0.0224 0.7656 0.7269
0.500 -0.0965 0.04455 0.03561 -0.0191 0.7580 0.7285
0.750 -0.0704 0.04460 0.03562 -0.0194 0.7552 0.7302
1.000 -0.0403 0.04463 0.03559 -0.0204 0.7533 0.7321
1.500 -0.0029 0.04479 0.03570 -0.0196 0.7436 0.7364
1.750 0.0280 0.04479 0.03563 -0.0212 0.7411 0.7387
2.000 0.0623 0.04477 0.03555 -0.0234 0.7393 0.7411
2.250 0.0727 0.04498 0.03576 -0.0219 0.7320 0.7432
2.500 0.0990 0.04501 0.03579 -0.0222 0.7286 0.7448
2.750 0.1294 0.04501 0.03580 -0.0232 0.7265 0.7466
3.000 0.1421 0.04526 0.03607 -0.0217 0.7196 0.7488
3.250 0.1681 0.04533 0.03614 -0.0223 0.7157 0.7509
3.500 0.2001 0.04527 0.03608 -0.0237 0.7132 0.7529
4.000 0.2444 0.04561 0.03643 -0.0243 0.7020 0.7576
4.250 0.2745 0.04551 0.03637 -0.0252 0.6993 0.7591
4.750 0.3137 0.04584 0.03680 -0.0241 0.6874 0.7624
5.000 0.3450 0.04568 0.03669 -0.0251 0.6847 0.7643
5.500 0.3864 0.04607 0.03720 -0.0247 0.6721 0.7689
5.750 0.4197 0.04586 0.03704 -0.0261 0.6695 0.7713
6.000 0.4337 0.04642 0.03765 -0.0254 0.6600 0.7735
6.250 0.4629 0.04623 0.03754 -0.0260 0.6562 0.7750
6.500 0.4955 0.04585 0.03727 -0.0269 0.6538 0.7766
6.750 0.5054 0.04651 0.03802 -0.0253 0.6430 0.7782
7.000 0.5372 0.04614 0.03775 -0.0262 0.6397 0.7799
7.500 0.5819 0.04632 0.03814 -0.0259 0.6255 0.7836
7.750 0.6167 0.04571 0.03764 -0.0270 0.6227 0.7858
8.000 0.6307 0.04624 0.03827 -0.0260 0.6108 0.7879
8.250 0.6697 0.04499 0.03713 -0.0273 0.6068 0.7901
8.500 0.6870 0.04480 0.03706 -0.0260 0.5932 0.7918
8.750 0.7075 0.04446 0.03683 -0.0249 0.5801 0.7935
9.000 0.7332 0.04392 0.03640 -0.0246 0.5690 0.7952
9.250 0.7638 0.04309 0.03570 -0.0247 0.5585 0.7969
9.500 0.7855 0.04306 0.03578 -0.0242 0.5433 0.7987
9.750 0.8117 0.04268 0.03549 -0.0241 0.5267 0.8007
10.000 0.8367 0.04244 0.03533 -0.0239 0.5064 0.8028
10.250 0.8659 0.04190 0.03481 -0.0240 0.4816 0.8050
10.500 0.8958 0.04141 0.03431 -0.0243 0.4553 0.8072
10.750 0.9209 0.04112 0.03396 -0.0238 0.4233 0.8093
11.000 0.9397 0.04137 0.03410 -0.0228 0.3848 0.8115
11.250 0.9514 0.04222 0.03474 -0.0213 0.3391 0.8137
11.500 0.9567 0.04365 0.03591 -0.0195 0.2904 0.8155
11.750 0.9583 0.04550 0.03747 -0.0176 0.2434 0.8172
12.000 0.9590 0.04757 0.03924 -0.0159 0.2004 0.8188
12.250 0.9619 0.04959 0.04104 -0.0145 0.1661 0.8204
12.500 0.9676 0.05147 0.04277 -0.0135 0.1402 0.8219
12.750 0.9756 0.05320 0.04447 -0.0127 0.1195 0.8233
13.000 0.9825 0.05500 0.04621 -0.0119 0.1035 0.8244
13.250 0.9897 0.05683 0.04803 -0.0111 0.0920 0.8256
13.500 0.9963 0.05875 0.04996 -0.0104 0.0819 0.8268
14.000 1.0088 0.06284 0.05415 -0.0091 0.0646 0.8296
14.250 1.0141 0.06505 0.05642 -0.0085 0.0572 0.8312
14.500 1.0195 0.06732 0.05876 -0.0081 0.0515 0.8330
14.750 1.0263 0.06951 0.06105 -0.0078 0.0460 0.8347
15.000 1.0308 0.07198 0.06355 -0.0076 0.0427 0.8363
15.250 1.0379 0.07423 0.06592 -0.0075 0.0398 0.8377
15.500 1.0432 0.07663 0.06842 -0.0073 0.0369 0.8390
15.750 1.0460 0.07932 0.07113 -0.0073 0.0351 0.8404
16.000 1.0531 0.08158 0.07358 -0.0072 0.0332 0.8419
16.250 1.0594 0.08397 0.07611 -0.0072 0.0318 0.8435
16.500 1.0648 0.08650 0.07875 -0.0074 0.0305 0.8452
16.750 1.0691 0.08919 0.08155 -0.0077 0.0293 0.8471
17.000 1.0731 0.09192 0.08433 -0.0081 0.0283 0.8489
17.250 1.0789 0.09457 0.08716 -0.0085 0.0272 0.8509
17.500 1.0842 0.09730 0.09009 -0.0089 0.0262 0.8528
17.750 1.0878 0.10017 0.09316 -0.0094 0.0254 0.8548
18.000 1.0906 0.10318 0.09636 -0.0100 0.0248 0.8570
18.250 1.0922 0.10638 0.09973 -0.0107 0.0242 0.8596
18.500 1.0927 0.10979 0.10330 -0.0117 0.0237 0.8625
18.750 1.0922 0.11337 0.10703 -0.0129 0.0232 0.8656
19.000 1.0910 0.11700 0.11080 -0.0142 0.0228 0.8690
19.250 1.0892 0.12068 0.11463 -0.0156 0.0223 0.8728
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