WORTMANN FX 2 AIRFOIL (fx2-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 2 AIRFOIL (fx2-il) Reynolds number: 200,000 Max Cl/Cd: 34.15 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx2-il-200000-n5.txt Download as CSV file: xf-fx2-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.000 -0.3538 0.09274 0.08733 -0.1695 0.8568 0.0173
-17.750 -0.3830 0.08421 0.07858 -0.1739 0.8565 0.0172
-17.500 -0.4051 0.07750 0.07168 -0.1772 0.8561 0.0174
-17.250 -0.4206 0.07226 0.06626 -0.1795 0.8557 0.0176
-17.000 -0.4324 0.06784 0.06167 -0.1812 0.8553 0.0178
-16.750 -0.4423 0.06390 0.05756 -0.1823 0.8548 0.0180
-16.500 -0.4482 0.06063 0.05413 -0.1831 0.8543 0.0182
-16.250 -0.4528 0.05766 0.05097 -0.1836 0.8538 0.0186
-16.000 -0.4550 0.05505 0.04818 -0.1838 0.8533 0.0189
-15.750 -0.4559 0.05271 0.04580 -0.1838 0.8528 0.0193
-15.500 -0.4546 0.05070 0.04370 -0.1837 0.8522 0.0197
-15.250 -0.4521 0.04890 0.04184 -0.1836 0.8517 0.0202
-15.000 -0.4483 0.04722 0.04007 -0.1832 0.8511 0.0207
-14.750 -0.4434 0.04569 0.03845 -0.1828 0.8506 0.0213
-14.500 -0.4377 0.04428 0.03695 -0.1823 0.8499 0.0222
-14.250 -0.4308 0.04296 0.03550 -0.1817 0.8492 0.0231
-14.000 -0.4226 0.04173 0.03413 -0.1809 0.8483 0.0239
-13.750 -0.4166 0.04047 0.03286 -0.1801 0.8476 0.0248
-13.500 -0.4087 0.03939 0.03174 -0.1793 0.8471 0.0256
-13.250 -0.3997 0.03843 0.03070 -0.1785 0.8465 0.0267
-13.000 -0.3897 0.03753 0.02974 -0.1777 0.8459 0.0281
-12.750 -0.3782 0.03674 0.02884 -0.1768 0.8454 0.0300
-12.500 -0.3694 0.03588 0.02799 -0.1758 0.8448 0.0317
-12.250 -0.3585 0.03516 0.02723 -0.1749 0.8443 0.0335
-12.000 -0.3467 0.03450 0.02650 -0.1739 0.8438 0.0360
-11.750 -0.3356 0.03383 0.02580 -0.1729 0.8432 0.0382
-11.500 -0.3240 0.03327 0.02520 -0.1719 0.8427 0.0412
-11.250 -0.3107 0.03279 0.02463 -0.1709 0.8422 0.0445
-11.000 -0.3001 0.03221 0.02406 -0.1697 0.8418 0.0472
-10.750 -0.2877 0.03176 0.02358 -0.1686 0.8413 0.0503
-10.500 -0.2734 0.03141 0.02313 -0.1676 0.8408 0.0539
-10.250 -0.2675 0.03102 0.02277 -0.1653 0.8397 0.0564
-10.000 -0.2615 0.03075 0.02251 -0.1630 0.8386 0.0591
-9.750 -0.2547 0.03059 0.02233 -0.1606 0.8376 0.0622
-9.500 -0.2486 0.03051 0.02221 -0.1580 0.8365 0.0648
-9.250 -0.2461 0.03043 0.02211 -0.1548 0.8353 0.0672
-9.000 -0.2490 0.03030 0.02203 -0.1508 0.8338 0.0698
-8.750 -0.2517 0.03030 0.02204 -0.1467 0.8323 0.0724
-8.500 -0.2507 0.03019 0.02190 -0.1431 0.8306 0.0755
-8.250 -0.2488 0.03008 0.02175 -0.1396 0.8292 0.0785
-8.000 -0.2486 0.02995 0.02158 -0.1359 0.8280 0.0812
-7.750 -0.2517 0.02972 0.02136 -0.1317 0.8268 0.0843
-7.500 -0.4161 0.03319 0.02496 -0.0974 0.8153 0.0727
-7.250 -0.4229 0.03289 0.02462 -0.0924 0.8132 0.0752
-7.000 -0.4234 0.03248 0.02415 -0.0885 0.8117 0.0779
-6.500 -0.4882 0.03262 0.02421 -0.0700 0.8031 0.0781
-6.250 -0.4856 0.03227 0.02381 -0.0668 0.8005 0.0812
-6.000 -0.4744 0.03164 0.02317 -0.0651 0.7986 0.0861
-5.750 -0.4577 0.03118 0.02268 -0.0642 0.7974 0.0910
-5.500 -0.4381 0.03072 0.02220 -0.0638 0.7964 0.0982
-5.250 -0.4163 0.03013 0.02168 -0.0638 0.7955 0.1134
-5.000 -0.3934 0.02940 0.02111 -0.0642 0.7948 0.1527
-4.750 -0.4104 0.02962 0.02141 -0.0577 0.7882 0.1707
-4.500 -0.3949 0.02863 0.02082 -0.0573 0.7857 0.2519
-4.250 -0.3758 0.02695 0.01998 -0.0583 0.7842 0.4209
-4.000 -0.3544 0.02682 0.02047 -0.0574 0.7829 0.5499
-3.750 -0.3281 0.02720 0.02093 -0.0569 0.7819 0.5824
-3.500 -0.2997 0.02774 0.02149 -0.0567 0.7810 0.6072
-3.250 -0.2695 0.02824 0.02194 -0.0569 0.7803 0.6233
-3.000 -0.2734 0.02906 0.02276 -0.0520 0.7735 0.6320
-2.750 -0.2501 0.02955 0.02317 -0.0513 0.7711 0.6414
-2.500 -0.2221 0.02985 0.02335 -0.0517 0.7694 0.6517
-2.250 -0.1953 0.03037 0.02385 -0.0512 0.7682 0.6568
-2.000 -0.1641 0.03041 0.02375 -0.0526 0.7673 0.6646
-1.750 -0.1355 0.03068 0.02399 -0.0527 0.7664 0.6671
-1.500 -0.1353 0.03133 0.02464 -0.0485 0.7593 0.6700
-1.250 -0.1115 0.03158 0.02485 -0.0481 0.7570 0.6744
-1.000 -0.0813 0.03150 0.02463 -0.0496 0.7555 0.6800
-0.750 -0.0533 0.03160 0.02471 -0.0498 0.7543 0.6815
-0.500 -0.0232 0.03157 0.02463 -0.0506 0.7533 0.6827
-0.250 -0.0149 0.03198 0.02504 -0.0480 0.7474 0.6844
0.000 0.0070 0.03211 0.02514 -0.0476 0.7441 0.6862
0.250 0.0350 0.03209 0.02507 -0.0482 0.7423 0.6881
0.500 0.0650 0.03202 0.02495 -0.0492 0.7409 0.6902
0.750 0.0962 0.03193 0.02480 -0.0505 0.7399 0.6926
1.000 0.1293 0.03180 0.02459 -0.0522 0.7391 0.6955
1.500 0.1579 0.03237 0.02519 -0.0489 0.7285 0.6979
1.750 0.1876 0.03230 0.02512 -0.0497 0.7271 0.6992
2.000 0.2183 0.03220 0.02502 -0.0505 0.7260 0.7007
2.500 0.2515 0.03275 0.02557 -0.0482 0.7153 0.7049
2.750 0.2818 0.03263 0.02545 -0.0492 0.7137 0.7071
3.000 0.3140 0.03245 0.02525 -0.0504 0.7125 0.7094
3.500 0.3498 0.03290 0.02573 -0.0486 0.7012 0.7127
3.750 0.3798 0.03271 0.02558 -0.0492 0.6995 0.7139
4.000 0.4111 0.03247 0.02538 -0.0501 0.6983 0.7153
4.500 0.4473 0.03295 0.02594 -0.0482 0.6864 0.7185
4.750 0.4786 0.03268 0.02571 -0.0491 0.6847 0.7203
5.000 0.5110 0.03236 0.02542 -0.0502 0.6835 0.7221
5.250 0.5191 0.03308 0.02617 -0.0480 0.6732 0.7241
5.500 0.5499 0.03283 0.02596 -0.0489 0.6710 0.7260
5.750 0.5815 0.03244 0.02562 -0.0498 0.6694 0.7275
6.250 0.6206 0.03277 0.02611 -0.0481 0.6569 0.7303
6.500 0.6544 0.03194 0.02535 -0.0489 0.6540 0.7317
6.750 0.6690 0.03225 0.02573 -0.0474 0.6427 0.7332
7.000 0.7064 0.03117 0.02469 -0.0486 0.6380 0.7347
7.250 0.7270 0.03115 0.02472 -0.0478 0.6247 0.7362
7.500 0.7535 0.03086 0.02448 -0.0477 0.6124 0.7378
7.750 0.7867 0.03023 0.02387 -0.0486 0.6019 0.7393
8.000 0.8251 0.02931 0.02297 -0.0501 0.5901 0.7407
8.250 0.8581 0.02876 0.02243 -0.0510 0.5725 0.7421
8.500 0.8902 0.02823 0.02189 -0.0517 0.5509 0.7431
8.750 0.9231 0.02764 0.02122 -0.0524 0.5233 0.7442
9.000 0.9449 0.02767 0.02109 -0.0517 0.4853 0.7454
9.250 0.9565 0.02830 0.02151 -0.0497 0.4454 0.7467
9.500 0.9605 0.02940 0.02239 -0.0468 0.4022 0.7480
9.750 0.9615 0.03076 0.02353 -0.0438 0.3600 0.7493
10.000 0.9622 0.03226 0.02481 -0.0409 0.3170 0.7506
10.250 0.9606 0.03398 0.02627 -0.0379 0.2706 0.7517
10.500 0.9612 0.03567 0.02774 -0.0354 0.2276 0.7528
10.750 0.9634 0.03735 0.02920 -0.0332 0.1903 0.7539
11.000 0.9681 0.03894 0.03061 -0.0313 0.1589 0.7552
11.250 0.9764 0.04032 0.03188 -0.0299 0.1330 0.7567
11.500 0.9840 0.04179 0.03323 -0.0286 0.1083 0.7581
11.750 0.9925 0.04316 0.03453 -0.0272 0.0932 0.7595
12.000 1.0024 0.04446 0.03583 -0.0261 0.0833 0.7610
12.250 1.0121 0.04581 0.03722 -0.0249 0.0756 0.7625
12.500 1.0237 0.04705 0.03852 -0.0241 0.0689 0.7635
12.750 1.0336 0.04847 0.03996 -0.0231 0.0614 0.7644
13.000 1.0455 0.04976 0.04130 -0.0224 0.0533 0.7652
13.250 1.0560 0.05119 0.04275 -0.0216 0.0448 0.7660
13.500 1.0651 0.05278 0.04431 -0.0208 0.0363 0.7668
13.750 1.0735 0.05447 0.04602 -0.0200 0.0317 0.7676
14.000 1.0808 0.05630 0.04788 -0.0192 0.0285 0.7684
14.250 1.0884 0.05814 0.04981 -0.0185 0.0264 0.7695
14.500 1.0960 0.06002 0.05177 -0.0179 0.0248 0.7705
14.750 1.1014 0.06218 0.05399 -0.0172 0.0231 0.7714
15.000 1.1049 0.06460 0.05647 -0.0166 0.0220 0.7721
15.250 1.1122 0.06665 0.05865 -0.0163 0.0212 0.7728
15.500 1.1178 0.06894 0.06105 -0.0159 0.0202 0.7735
15.750 1.1226 0.07131 0.06354 -0.0156 0.0194 0.7742
16.000 1.1272 0.07375 0.06610 -0.0154 0.0188 0.7748
16.250 1.1306 0.07637 0.06882 -0.0152 0.0182 0.7755
16.500 1.1320 0.07926 0.07181 -0.0152 0.0176 0.7762
16.750 1.1331 0.08226 0.07490 -0.0152 0.0170 0.7769
17.000 1.1381 0.08483 0.07762 -0.0154 0.0165 0.7776
17.250 1.1416 0.08760 0.08053 -0.0156 0.0160 0.7784
17.500 1.1447 0.09045 0.08351 -0.0160 0.0156 0.7792
17.750 1.1472 0.09343 0.08662 -0.0164 0.0152 0.7801
18.000 1.1494 0.09649 0.08980 -0.0170 0.0148 0.7809
18.250 1.1513 0.09961 0.09305 -0.0177 0.0146 0.7818
18.500 1.1527 0.10282 0.09637 -0.0185 0.0143 0.7827
18.750 1.1534 0.10614 0.09978 -0.0195 0.0140 0.7836
19.000 1.1543 0.10943 0.10317 -0.0205 0.0137 0.7846
19.250 1.1550 0.11274 0.10655 -0.0216 0.0135 0.7855
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