WORTMANN FX 2 AIRFOIL (fx2-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 2 AIRFOIL (fx2-il) Reynolds number: 200,000 Max Cl/Cd: 34.2 at α=10.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx2-il-200000.txt Download as CSV file: xf-fx2-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.750 -0.1870 0.08967 0.08510 -0.1910 0.9143 0.0431
-15.500 -0.2266 0.08110 0.07645 -0.1942 0.9141 0.0418
-15.250 -0.2744 0.07350 0.06870 -0.1962 0.9138 0.0410
-15.000 -0.4076 0.06218 0.05670 -0.1933 0.9125 0.0374
-14.750 -0.4189 0.05996 0.05444 -0.1916 0.9119 0.0379
-14.500 -0.4490 0.05784 0.05214 -0.1878 0.9113 0.0378
-14.250 -0.4690 0.05684 0.05107 -0.1835 0.9107 0.0380
-14.000 -0.5201 0.05833 0.05251 -0.1725 0.9101 0.0374
-13.750 -0.7057 0.11036 0.10694 -0.0697 0.9924 0.0369
-13.500 -0.7240 0.10395 0.10045 -0.0724 0.9897 0.0364
-13.250 -0.7527 0.09687 0.09321 -0.0753 0.9873 0.0361
-13.000 -0.7768 0.09109 0.08726 -0.0775 0.9853 0.0357
-12.750 -0.8094 0.08564 0.08160 -0.0777 0.9831 0.0357
-12.500 -0.8330 0.08079 0.07657 -0.0769 0.9777 0.0352
-12.250 -0.8606 0.07633 0.07185 -0.0763 0.9747 0.0355
-12.000 -0.8825 0.07268 0.06792 -0.0755 0.9727 0.0354
-11.750 -0.9095 0.06929 0.06435 -0.0709 0.9663 0.0353
-11.500 -0.9277 0.06632 0.06111 -0.0687 0.9621 0.0356
-11.250 -0.9437 0.06389 0.05835 -0.0664 0.9597 0.0357
-11.000 -0.9744 0.06192 0.05623 -0.0590 0.9518 0.0359
-10.750 -0.9833 0.05924 0.05317 -0.0560 0.9481 0.0363
-10.500 -0.9806 0.05716 0.05070 -0.0545 0.9460 0.0367
-10.250 -0.9908 0.05517 0.04842 -0.0495 0.9412 0.0370
-10.000 -0.9838 0.05221 0.04522 -0.0475 0.9368 0.0377
-9.750 -0.9659 0.05077 0.04374 -0.0472 0.9344 0.0387
-9.500 -0.9463 0.04996 0.04285 -0.0471 0.9325 0.0400
-9.250 -0.9240 0.04922 0.04195 -0.0474 0.9310 0.0414
-9.000 -0.9004 0.04896 0.04139 -0.0478 0.9300 0.0436
-8.750 -0.9140 0.04685 0.03912 -0.0411 0.9221 0.0442
-8.500 -0.8911 0.04536 0.03760 -0.0409 0.9200 0.0461
-8.250 -0.8677 0.04478 0.03701 -0.0410 0.9181 0.0479
-8.000 -0.8421 0.04450 0.03663 -0.0415 0.9165 0.0506
-7.750 -0.8150 0.04479 0.03666 -0.0422 0.9153 0.0533
-7.500 -0.8200 0.04276 0.03475 -0.0368 0.9101 0.0554
-7.250 -0.8030 0.04209 0.03409 -0.0356 0.9060 0.0582
-7.000 -0.7801 0.04174 0.03365 -0.0354 0.9035 0.0618
-6.750 -0.7560 0.04124 0.03316 -0.0353 0.9019 0.0664
-6.500 -0.7299 0.04127 0.03321 -0.0359 0.9006 0.0719
-6.250 -0.7031 0.04156 0.03343 -0.0365 0.8997 0.0771
-6.000 -0.7207 0.03932 0.03123 -0.0293 0.8913 0.0788
-5.750 -0.6992 0.03892 0.03085 -0.0292 0.8883 0.0850
-5.500 -0.6742 0.03870 0.03059 -0.0297 0.8864 0.0912
-5.250 -0.6472 0.03871 0.03064 -0.0309 0.8852 0.0989
-5.000 -0.6176 0.03905 0.03101 -0.0325 0.8843 0.1084
-4.750 -0.6305 0.03706 0.02903 -0.0263 0.8755 0.1121
-4.500 -0.6043 0.03677 0.02880 -0.0272 0.8727 0.1265
-4.250 -0.5765 0.03623 0.02856 -0.0289 0.8710 0.1713
-4.000 -0.5584 0.03400 0.02863 -0.0302 0.8699 0.5707
-3.750 -0.5257 0.03671 0.03148 -0.0297 0.8688 0.6219
-3.500 -0.5338 0.03558 0.03030 -0.0239 0.8595 0.6342
-3.250 -0.5055 0.03702 0.03163 -0.0235 0.8564 0.6497
-3.000 -0.4732 0.03843 0.03290 -0.0244 0.8546 0.6626
-2.750 -0.4436 0.04104 0.03554 -0.0229 0.8532 0.6704
-2.500 -0.4501 0.04031 0.03477 -0.0177 0.8447 0.6795
-2.250 -0.4296 0.04179 0.03628 -0.0149 0.8409 0.6856
-2.000 -0.4002 0.04312 0.03753 -0.0147 0.8388 0.6963
-1.750 -0.3712 0.04507 0.03947 -0.0134 0.8373 0.7025
-1.500 -0.3751 0.04414 0.03848 -0.0098 0.8290 0.7108
-1.250 -0.3553 0.04503 0.03939 -0.0071 0.8248 0.7148
-1.000 -0.3236 0.04606 0.04034 -0.0076 0.8225 0.7227
-0.750 -0.2901 0.04740 0.04164 -0.0080 0.8210 0.7293
-0.500 -0.3033 0.04653 0.04079 -0.0017 0.8112 0.7331
-0.250 -0.2642 0.04697 0.04110 -0.0050 0.8077 0.7419
0.000 -0.2286 0.04774 0.04184 -0.0059 0.8056 0.7442
0.250 -0.2267 0.04703 0.04113 -0.0019 0.7939 0.7469
0.500 -0.1719 0.04729 0.04128 -0.0067 0.7902 0.7483
0.750 -0.1473 0.04632 0.04025 -0.0067 0.7770 0.7505
1.000 -0.0993 0.04645 0.04030 -0.0108 0.7750 0.7525
1.250 -0.0884 0.04587 0.03968 -0.0098 0.7642 0.7547
1.500 -0.0447 0.04583 0.03955 -0.0139 0.7619 0.7568
1.750 -0.0026 0.04587 0.03954 -0.0169 0.7605 0.7584
2.000 -0.0011 0.04554 0.03924 -0.0134 0.7499 0.7601
2.250 0.0345 0.04552 0.03919 -0.0151 0.7479 0.7615
2.500 0.0740 0.04554 0.03919 -0.0175 0.7466 0.7630
2.750 0.0787 0.04547 0.03913 -0.0151 0.7362 0.7650
3.000 0.1164 0.04538 0.03903 -0.0174 0.7343 0.7668
3.250 0.1576 0.04529 0.03892 -0.0203 0.7330 0.7689
3.500 0.1662 0.04542 0.03904 -0.0189 0.7228 0.7713
3.750 0.2066 0.04533 0.03892 -0.0220 0.7208 0.7738
4.000 0.2424 0.04505 0.03868 -0.0234 0.7195 0.7755
4.250 0.2471 0.04528 0.03895 -0.0207 0.7093 0.7773
4.500 0.2825 0.04503 0.03873 -0.0222 0.7072 0.7791
4.750 0.3205 0.04470 0.03842 -0.0241 0.7057 0.7811
5.000 0.3295 0.04509 0.03885 -0.0224 0.6957 0.7833
5.250 0.3662 0.04476 0.03854 -0.0243 0.6934 0.7856
5.500 0.4061 0.04433 0.03814 -0.0268 0.6919 0.7879
5.750 0.4472 0.04393 0.03776 -0.0295 0.6905 0.7902
6.000 0.4532 0.04424 0.03813 -0.0271 0.6793 0.7918
6.250 0.4892 0.04361 0.03757 -0.0283 0.6776 0.7937
6.500 0.5268 0.04294 0.03699 -0.0298 0.6765 0.7957
6.750 0.5352 0.04335 0.03745 -0.0277 0.6649 0.7980
7.000 0.5767 0.04229 0.03647 -0.0296 0.6632 0.8005
7.250 0.6234 0.04051 0.03475 -0.0319 0.6604 0.8029
7.500 0.6498 0.03970 0.03400 -0.0318 0.6500 0.8051
7.750 0.6956 0.03806 0.03243 -0.0341 0.6481 0.8070
8.000 0.7360 0.03651 0.03100 -0.0354 0.6467 0.8087
8.250 0.7497 0.03650 0.03107 -0.0336 0.6351 0.8105
8.500 0.7902 0.03491 0.02959 -0.0348 0.6327 0.8124
8.750 0.8113 0.03460 0.02937 -0.0340 0.6220 0.8143
9.000 0.8535 0.03302 0.02789 -0.0357 0.6169 0.8163
9.250 0.8792 0.03258 0.02754 -0.0355 0.6037 0.8182
9.500 0.9145 0.03159 0.02661 -0.0364 0.5884 0.8203
9.750 0.9553 0.03030 0.02529 -0.0380 0.5634 0.8224
10.000 0.9906 0.02919 0.02399 -0.0386 0.5182 0.8240
10.250 1.0051 0.02939 0.02391 -0.0367 0.4647 0.8258
10.500 1.0076 0.03045 0.02467 -0.0336 0.4127 0.8273
10.750 1.0042 0.03200 0.02594 -0.0301 0.3626 0.8287
11.000 0.9992 0.03382 0.02748 -0.0267 0.3119 0.8300
11.250 0.9917 0.03594 0.02928 -0.0233 0.2599 0.8313
11.750 0.9837 0.04022 0.03300 -0.0180 0.1699 0.8339
12.000 0.9856 0.04212 0.03472 -0.0162 0.1398 0.8354
12.250 0.9902 0.04392 0.03638 -0.0148 0.1176 0.8369
12.500 0.9964 0.04567 0.03803 -0.0136 0.1005 0.8383
12.750 1.0003 0.04745 0.03977 -0.0120 0.0885 0.8401
13.000 1.0021 0.04946 0.04175 -0.0104 0.0769 0.8418
13.250 1.0030 0.05166 0.04391 -0.0087 0.0676 0.8435
13.500 1.0110 0.05334 0.04564 -0.0078 0.0599 0.8453
13.750 1.0179 0.05519 0.04752 -0.0068 0.0545 0.8468
14.000 1.0277 0.05685 0.04920 -0.0063 0.0504 0.8482
14.250 1.0370 0.05859 0.05091 -0.0056 0.0474 0.8492
14.500 1.0496 0.06009 0.05253 -0.0053 0.0444 0.8503
14.750 1.0612 0.06168 0.05416 -0.0051 0.0422 0.8514
15.000 1.0751 0.06315 0.05556 -0.0049 0.0398 0.8524
15.250 1.0889 0.06469 0.05724 -0.0048 0.0382 0.8535
15.500 1.1037 0.06605 0.05871 -0.0046 0.0367 0.8548
15.750 1.1171 0.06750 0.06023 -0.0044 0.0353 0.8563
16.000 1.1329 0.06882 0.06156 -0.0043 0.0342 0.8579
16.250 1.1537 0.07001 0.06282 -0.0044 0.0328 0.8593
16.500 1.1638 0.07203 0.06505 -0.0042 0.0319 0.8606
16.750 1.1736 0.07410 0.06729 -0.0042 0.0309 0.8620
17.000 1.1841 0.07620 0.06955 -0.0042 0.0301 0.8634
17.250 1.1934 0.07847 0.07197 -0.0042 0.0294 0.8649
17.500 1.2021 0.08079 0.07440 -0.0044 0.0288 0.8663
17.750 1.2122 0.08314 0.07687 -0.0046 0.0283 0.8678
18.000 1.2249 0.08574 0.07959 -0.0050 0.0277 0.8692
18.250 1.2227 0.08966 0.08376 -0.0051 0.0274 0.8705
18.500 1.2126 0.09391 0.08830 -0.0052 0.0273 0.8719
18.750 1.1978 0.09872 0.09340 -0.0057 0.0272 0.8734
19.000 1.1829 0.10383 0.09878 -0.0067 0.0271 0.8749
19.250 1.1664 0.10936 0.10459 -0.0081 0.0270 0.8766
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