WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=200,000 Ncrit=0
| Details | Polar file |
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Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il) Reynolds number: 200,000 Max Cl/Cd: 31.68 at α=9.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx3-il-200000.txt Download as CSV file: xf-fx3-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 3 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
------ -------- --------- --------- -------- -------- --------
-12.500 -0.5093 0.11118 0.10811 -0.0739 0.9616 0.0380
-12.250 -0.5353 0.10406 0.10092 -0.0768 0.9605 0.0374
-12.000 -0.5676 0.09681 0.09357 -0.0792 0.9596 0.0369
-11.750 -0.6009 0.09009 0.08671 -0.0806 0.9586 0.0364
-11.500 -0.6334 0.08392 0.08037 -0.0808 0.9577 0.0359
-11.250 -0.6650 0.07819 0.07447 -0.0802 0.9569 0.0355
-11.000 -0.6947 0.07306 0.06913 -0.0789 0.9561 0.0352
-10.750 -0.9058 0.07020 0.06530 -0.0627 0.9580 0.0314
-10.500 -0.8876 0.07107 0.06633 -0.0632 0.9569 0.0325
-10.250 -0.9395 0.06441 0.05910 -0.0551 0.9489 0.0317
-10.000 -0.9383 0.06171 0.05617 -0.0537 0.9458 0.0321
-9.750 -0.9296 0.05932 0.05356 -0.0532 0.9438 0.0326
-9.500 -0.9157 0.05746 0.05146 -0.0532 0.9424 0.0333
-9.250 -0.8999 0.05564 0.04935 -0.0533 0.9415 0.0342
-9.000 -0.9087 0.05289 0.04643 -0.0479 0.9356 0.0347
-8.750 -0.8937 0.05086 0.04406 -0.0470 0.9324 0.0364
-8.500 -0.8741 0.04915 0.04190 -0.0467 0.9303 0.0381
-8.250 -0.8534 0.04715 0.03974 -0.0463 0.9292 0.0398
-8.000 -0.8289 0.04664 0.03919 -0.0468 0.9281 0.0416
-7.750 -0.8022 0.04640 0.03883 -0.0476 0.9271 0.0445
-7.500 -0.7744 0.04613 0.03827 -0.0483 0.9264 0.0477
-7.250 -0.7812 0.04383 0.03603 -0.0424 0.9201 0.0492
-7.000 -0.7595 0.04332 0.03550 -0.0422 0.9171 0.0523
-6.750 -0.7332 0.04313 0.03516 -0.0428 0.9150 0.0566
-6.500 -0.7106 0.04242 0.03448 -0.0421 0.9137 0.0613
-6.250 -0.6830 0.04246 0.03448 -0.0429 0.9126 0.0668
-6.000 -0.6567 0.04243 0.03437 -0.0430 0.9118 0.0725
-5.750 -0.6287 0.04278 0.03477 -0.0438 0.9111 0.0785
-5.500 -0.6357 0.04080 0.03277 -0.0382 0.9028 0.0811
-5.250 -0.6098 0.04076 0.03262 -0.0387 0.9003 0.0856
-5.000 -0.5870 0.04041 0.03239 -0.0382 0.8986 0.0918
-4.750 -0.5568 0.04063 0.03258 -0.0397 0.8972 0.0983
-4.500 -0.5260 0.04081 0.03278 -0.0413 0.8962 0.1047
-4.250 -0.4917 0.04127 0.03327 -0.0440 0.8955 0.1126
-4.000 -0.4947 0.03951 0.03148 -0.0396 0.8869 0.1160
-3.750 -0.4602 0.03917 0.03123 -0.0428 0.8846 0.1280
-3.500 -0.4178 0.03865 0.03106 -0.0484 0.8833 0.1753
-3.250 -0.4146 0.04206 0.03712 -0.0387 0.8809 0.6229
-3.000 -0.3665 0.04502 0.03982 -0.0432 0.8799 0.6723
-2.750 -0.3768 0.04442 0.03921 -0.0360 0.8700 0.6819
-2.500 -0.3617 0.04641 0.04117 -0.0311 0.8669 0.6950
-2.250 -0.3399 0.04850 0.04320 -0.0279 0.8652 0.7081
-2.000 -0.3519 0.04837 0.04310 -0.0196 0.8574 0.7121
-1.750 -0.3319 0.04926 0.04391 -0.0174 0.8534 0.7239
-1.500 -0.3056 0.05058 0.04515 -0.0165 0.8511 0.7373
-1.250 -0.2909 0.05207 0.04663 -0.0109 0.8496 0.7440
-1.000 -0.2945 0.05122 0.04576 -0.0070 0.8404 0.7540
-0.750 -0.2686 0.05231 0.04678 -0.0062 0.8373 0.7683
-0.500 -0.2598 0.05309 0.04757 0.0011 0.8353 0.7786
-0.250 -0.1594 0.05772 0.05227 0.0006 0.8368 0.8700
0.000 -0.2664 0.05438 0.04893 0.0213 0.8236 0.8496
2.000 -0.0796 0.05125 0.04538 0.0197 0.7705 0.8756
2.250 -0.0422 0.05086 0.04494 0.0170 0.7681 0.8738
2.500 -0.0067 0.05092 0.04495 0.0110 0.7596 0.8611
2.750 0.0290 0.05056 0.04456 0.0086 0.7570 0.8603
3.000 0.0689 0.05039 0.04436 0.0055 0.7554 0.8600
3.250 0.0836 0.04990 0.04388 0.0060 0.7463 0.8575
3.500 0.1240 0.04964 0.04361 0.0027 0.7445 0.8559
3.750 0.1446 0.04954 0.04353 0.0018 0.7360 0.8539
4.000 0.1833 0.04930 0.04328 -0.0012 0.7337 0.8537
4.250 0.2263 0.04907 0.04306 -0.0051 0.7323 0.8527
4.500 0.2539 0.04934 0.04335 -0.0080 0.7232 0.8495
4.750 0.3070 0.04956 0.04360 -0.0146 0.7213 0.8473
5.000 0.3510 0.04930 0.04336 -0.0184 0.7199 0.8471
5.250 0.3647 0.04921 0.04332 -0.0175 0.7103 0.8463
5.500 0.4023 0.04863 0.04278 -0.0197 0.7082 0.8454
5.750 0.4424 0.04798 0.04218 -0.0224 0.7067 0.8445
6.000 0.4595 0.04808 0.04235 -0.0223 0.6965 0.8432
6.250 0.4998 0.04744 0.04177 -0.0250 0.6942 0.8430
6.500 0.5426 0.04663 0.04103 -0.0281 0.6927 0.8426
6.750 0.5620 0.04679 0.04127 -0.0283 0.6820 0.8412
7.000 0.6041 0.04597 0.04053 -0.0313 0.6797 0.8401
7.250 0.6470 0.04501 0.03967 -0.0342 0.6780 0.8398
7.500 0.6743 0.04455 0.03930 -0.0351 0.6672 0.8390
7.750 0.7345 0.04136 0.03621 -0.0391 0.6635 0.8378
8.000 0.7858 0.03948 0.03443 -0.0430 0.6612 0.8364
8.250 0.8171 0.03945 0.03452 -0.0452 0.6491 0.8344
8.500 0.8680 0.03777 0.03296 -0.0490 0.6453 0.8338
8.750 0.9016 0.03742 0.03271 -0.0509 0.6321 0.8331
9.000 0.9501 0.03598 0.03136 -0.0544 0.6159 0.8319
9.250 0.9926 0.03432 0.02967 -0.0563 0.5859 0.8312
9.500 1.0314 0.03305 0.02820 -0.0577 0.5373 0.8305
9.750 1.0502 0.03315 0.02798 -0.0567 0.4771 0.8296
10.000 1.0533 0.03439 0.02884 -0.0540 0.4125 0.8284
10.250 1.0506 0.03620 0.03028 -0.0509 0.3483 0.8273
10.500 1.0464 0.03833 0.03203 -0.0480 0.2834 0.8260
10.750 1.0438 0.04056 0.03388 -0.0456 0.2223 0.8249
11.000 1.0455 0.04265 0.03567 -0.0439 0.1750 0.8237
11.250 1.0525 0.04446 0.03729 -0.0428 0.1438 0.8229
11.500 1.0616 0.04613 0.03885 -0.0421 0.1200 0.8224
11.750 1.0708 0.04786 0.04048 -0.0413 0.0980 0.8218
12.000 1.0756 0.05008 0.04254 -0.0403 0.0743 0.8208
12.250 1.0829 0.05226 0.04467 -0.0396 0.0575 0.8197
12.500 1.0917 0.05441 0.04678 -0.0393 0.0495 0.8187
12.750 1.1039 0.05635 0.04872 -0.0394 0.0442 0.8177
13.000 1.1135 0.05852 0.05092 -0.0391 0.0410 0.8169
13.250 1.1234 0.06015 0.05264 -0.0383 0.0383 0.8164
13.500 1.1318 0.06194 0.05445 -0.0376 0.0361 0.8160
13.750 1.1401 0.06374 0.05626 -0.0366 0.0342 0.8155
14.000 1.1529 0.06523 0.05791 -0.0361 0.0326 0.8151
14.250 1.1660 0.06669 0.05947 -0.0356 0.0312 0.8146
14.500 1.1796 0.06816 0.06100 -0.0351 0.0300 0.8142
14.750 1.1938 0.06958 0.06247 -0.0348 0.0289 0.8138
15.000 1.2151 0.07055 0.06344 -0.0343 0.0275 0.8134
15.250 1.2304 0.07222 0.06531 -0.0339 0.0267 0.8130
15.500 1.2405 0.07426 0.06756 -0.0334 0.0260 0.8126
15.750 1.2510 0.07643 0.06997 -0.0330 0.0255 0.8122
16.000 1.2589 0.07893 0.07271 -0.0325 0.0250 0.8118
16.250 1.2633 0.08183 0.07586 -0.0320 0.0246 0.8113
16.500 1.2641 0.08513 0.07942 -0.0315 0.0244 0.8109
16.750 1.2607 0.08890 0.08346 -0.0311 0.0243 0.8105
17.000 1.2536 0.09308 0.08793 -0.0309 0.0241 0.8101
17.250 1.2431 0.09778 0.09291 -0.0311 0.0240 0.8098
17.500 1.2300 0.10290 0.09831 -0.0317 0.0240 0.8095
17.750 1.2150 0.10846 0.10413 -0.0330 0.0238 0.8092
18.000 1.1949 0.11509 0.11106 -0.0351 0.0240 0.8088
18.250 1.1735 0.12229 0.11854 -0.0382 0.0241 0.8083
18.500 1.1479 0.13081 0.12734 -0.0426 0.0244 0.8077
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