WORTMANN FX 2 AIRFOIL (fx2-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 2 AIRFOIL (fx2-il) Reynolds number: 500,000 Max Cl/Cd: 51.6 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx2-il-500000.txt Download as CSV file: xf-fx2-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.4217 0.09730 0.09327 -0.1684 0.8556 0.0170
-19.250 -0.4534 0.08825 0.08402 -0.1733 0.8553 0.0169
-19.000 -0.4707 0.08201 0.07763 -0.1768 0.8549 0.0168
-18.750 -0.4909 0.07560 0.07102 -0.1803 0.8546 0.0171
-18.500 -0.5009 0.07098 0.06626 -0.1828 0.8542 0.0171
-18.250 -0.5125 0.06639 0.06149 -0.1849 0.8538 0.0173
-18.000 -0.5187 0.06271 0.05765 -0.1869 0.8533 0.0175
-17.750 -0.5316 0.05855 0.05333 -0.1879 0.8530 0.0179
-17.500 -0.5323 0.05586 0.05051 -0.1887 0.8525 0.0178
-17.250 -0.5312 0.05353 0.04814 -0.1893 0.8522 0.0183
-17.000 -0.5289 0.05138 0.04592 -0.1896 0.8519 0.0185
-16.750 -0.5257 0.04937 0.04384 -0.1899 0.8517 0.0188
-16.500 -0.5210 0.04759 0.04201 -0.1901 0.8514 0.0192
-16.250 -0.5165 0.04583 0.04017 -0.1901 0.8511 0.0196
-16.000 -0.5116 0.04414 0.03839 -0.1900 0.8508 0.0200
-15.750 -0.5052 0.04265 0.03681 -0.1898 0.8505 0.0205
-15.500 -0.4977 0.04125 0.03532 -0.1895 0.8502 0.0208
-15.250 -0.4900 0.03994 0.03390 -0.1891 0.8498 0.0212
-15.000 -0.4814 0.03869 0.03257 -0.1884 0.8495 0.0216
-14.750 -0.4733 0.03750 0.03138 -0.1878 0.8492 0.0224
-14.500 -0.4639 0.03645 0.03031 -0.1872 0.8488 0.0230
-14.250 -0.4533 0.03554 0.02937 -0.1867 0.8484 0.0238
-14.000 -0.4426 0.03464 0.02842 -0.1860 0.8478 0.0245
-13.750 -0.4311 0.03381 0.02751 -0.1853 0.8472 0.0254
-13.500 -0.4213 0.03290 0.02656 -0.1843 0.8467 0.0263
-13.250 -0.4117 0.03205 0.02571 -0.1833 0.8463 0.0271
-13.000 -0.4007 0.03132 0.02497 -0.1824 0.8459 0.0281
-12.750 -0.3885 0.03068 0.02430 -0.1815 0.8455 0.0291
-12.500 -0.3764 0.03006 0.02363 -0.1805 0.8450 0.0304
-12.250 -0.3655 0.02940 0.02294 -0.1793 0.8446 0.0314
-12.000 -0.3562 0.02872 0.02229 -0.1779 0.8442 0.0329
-11.750 -0.3431 0.02826 0.02182 -0.1770 0.8437 0.0348
-11.500 -0.3298 0.02782 0.02134 -0.1759 0.8433 0.0366
-11.250 -0.3212 0.02720 0.02073 -0.1742 0.8429 0.0387
-11.000 -0.3093 0.02677 0.02032 -0.1729 0.8424 0.0407
-10.750 -0.2952 0.02647 0.02000 -0.1718 0.8420 0.0434
-10.500 -0.2866 0.02597 0.01949 -0.1700 0.8415 0.0462
-10.250 -0.2744 0.02560 0.01913 -0.1686 0.8409 0.0489
-10.000 -0.2596 0.02534 0.01886 -0.1675 0.8403 0.0519
-9.750 -0.2481 0.02502 0.01851 -0.1659 0.8397 0.0542
-9.500 -0.2412 0.02460 0.01811 -0.1636 0.8392 0.0573
-9.250 -0.2300 0.02436 0.01786 -0.1619 0.8387 0.0599
-9.000 -0.2171 0.02423 0.01770 -0.1603 0.8382 0.0627
-8.750 -0.2092 0.02401 0.01747 -0.1580 0.8377 0.0651
-8.500 -0.2073 0.02378 0.01725 -0.1548 0.8370 0.0679
-8.250 -0.2051 0.02391 0.01739 -0.1514 0.8363 0.0703
-8.000 -0.4847 0.03036 0.02394 -0.0962 0.8249 0.0542
-7.750 -0.4971 0.02995 0.02352 -0.0904 0.8235 0.0560
-7.500 -0.5211 0.02990 0.02343 -0.0825 0.8225 0.0566
-7.250 -0.6081 0.03077 0.02420 -0.0641 0.8143 0.0528
-7.000 -0.6112 0.03037 0.02376 -0.0601 0.8122 0.0548
-6.750 -0.5919 0.02984 0.02323 -0.0596 0.8102 0.0583
-6.500 -0.5646 0.02952 0.02288 -0.0603 0.8089 0.0621
-6.250 -0.5362 0.02899 0.02231 -0.0612 0.8078 0.0658
-6.000 -0.5081 0.02845 0.02177 -0.0621 0.8071 0.0703
-5.750 -0.4769 0.02816 0.02144 -0.0634 0.8065 0.0744
-5.500 -0.4457 0.02774 0.02100 -0.0649 0.8060 0.0798
-5.250 -0.4137 0.02739 0.02066 -0.0664 0.8055 0.0865
-5.000 -0.3807 0.02702 0.02035 -0.0681 0.8051 0.1001
-4.750 -0.3490 0.02611 0.01986 -0.0704 0.8047 0.1812
-4.000 -0.3362 0.02321 0.01863 -0.0625 0.7912 0.5685
-3.750 -0.3345 0.02359 0.01907 -0.0585 0.7846 0.5880
-3.500 -0.3163 0.02385 0.01941 -0.0571 0.7812 0.6080
-3.250 -0.2873 0.02408 0.01963 -0.0574 0.7796 0.6234
-3.000 -0.2556 0.02427 0.01976 -0.0583 0.7784 0.6347
-2.750 -0.2234 0.02458 0.02001 -0.0592 0.7776 0.6457
-2.500 -0.1915 0.02497 0.02039 -0.0599 0.7769 0.6519
-2.250 -0.1586 0.02534 0.02072 -0.0608 0.7763 0.6587
-2.000 -0.1538 0.02588 0.02123 -0.0574 0.7695 0.6636
-1.750 -0.1322 0.02624 0.02161 -0.0565 0.7663 0.6664
-1.500 -0.1035 0.02646 0.02181 -0.0568 0.7649 0.6691
-1.250 -0.0730 0.02668 0.02201 -0.0574 0.7638 0.6734
-1.000 -0.0402 0.02678 0.02203 -0.0586 0.7630 0.6784
-0.750 -0.0082 0.02679 0.02205 -0.0595 0.7624 0.6802
-0.500 0.0238 0.02689 0.02216 -0.0603 0.7618 0.6821
-0.250 0.0238 0.02755 0.02284 -0.0561 0.7537 0.6846
0.000 0.0515 0.02756 0.02283 -0.0565 0.7517 0.6865
0.250 0.0817 0.02752 0.02276 -0.0573 0.7505 0.6884
0.500 0.1133 0.02744 0.02264 -0.0584 0.7496 0.6905
0.750 0.1462 0.02732 0.02248 -0.0598 0.7488 0.6928
1.000 0.1791 0.02718 0.02230 -0.0611 0.7482 0.6946
1.250 0.2118 0.02700 0.02213 -0.0622 0.7477 0.6958
1.500 0.2450 0.02684 0.02198 -0.0635 0.7473 0.6970
1.750 0.2785 0.02670 0.02185 -0.0647 0.7469 0.6983
2.000 0.3122 0.02654 0.02170 -0.0660 0.7465 0.6998
2.250 0.3060 0.02711 0.02228 -0.0610 0.7354 0.7018
2.500 0.3398 0.02687 0.02205 -0.0623 0.7348 0.7037
2.750 0.3740 0.02662 0.02180 -0.0637 0.7342 0.7060
3.000 0.4085 0.02635 0.02152 -0.0652 0.7337 0.7082
3.250 0.4434 0.02607 0.02124 -0.0667 0.7332 0.7102
3.500 0.4774 0.02567 0.02087 -0.0680 0.7328 0.7116
3.750 0.4746 0.02629 0.02152 -0.0635 0.7220 0.7132
4.000 0.5076 0.02596 0.02123 -0.0646 0.7212 0.7147
4.250 0.5412 0.02562 0.02092 -0.0658 0.7206 0.7162
4.500 0.5754 0.02524 0.02058 -0.0671 0.7200 0.7179
4.750 0.6043 0.02490 0.02027 -0.0675 0.7173 0.7198
5.000 0.6479 0.02403 0.01944 -0.0702 0.7182 0.7216
5.250 0.6573 0.02418 0.01960 -0.0675 0.7082 0.7237
5.500 0.6959 0.02339 0.01883 -0.0693 0.7072 0.7253
5.750 0.7329 0.02252 0.01801 -0.0709 0.7062 0.7268
6.000 0.7697 0.02163 0.01718 -0.0724 0.7051 0.7282
6.250 0.7748 0.02208 0.01766 -0.0690 0.6932 0.7297
6.500 0.8100 0.02140 0.01704 -0.0702 0.6910 0.7311
7.000 0.8491 0.02153 0.01726 -0.0682 0.6725 0.7345
7.250 0.8806 0.02109 0.01684 -0.0689 0.6638 0.7362
7.500 0.9185 0.02029 0.01603 -0.0706 0.6496 0.7378
7.750 0.9606 0.01930 0.01493 -0.0728 0.6265 0.7392
8.000 0.9855 0.01910 0.01454 -0.0724 0.5906 0.7404
8.250 0.9929 0.01976 0.01501 -0.0694 0.5541 0.7415
8.500 0.9905 0.02081 0.01585 -0.0651 0.5143 0.7427
8.750 0.9824 0.02221 0.01700 -0.0601 0.4672 0.7438
9.000 0.9787 0.02358 0.01816 -0.0559 0.4265 0.7449
9.250 0.9747 0.02504 0.01939 -0.0519 0.3810 0.7460
9.500 0.9732 0.02649 0.02060 -0.0484 0.3364 0.7470
9.750 0.9706 0.02807 0.02190 -0.0449 0.2833 0.7480
10.000 0.9734 0.02943 0.02302 -0.0422 0.2384 0.7489
10.250 0.9763 0.03085 0.02419 -0.0397 0.1949 0.7499
10.500 0.9828 0.03212 0.02527 -0.0377 0.1607 0.7508
10.750 0.9912 0.03331 0.02630 -0.0359 0.1296 0.7517
11.000 0.9994 0.03455 0.02735 -0.0343 0.1002 0.7526
11.250 1.0108 0.03562 0.02836 -0.0330 0.0879 0.7536
11.500 1.0227 0.03668 0.02939 -0.0318 0.0790 0.7546
11.750 1.0356 0.03771 0.03040 -0.0308 0.0713 0.7554
12.000 1.0498 0.03866 0.03136 -0.0299 0.0645 0.7562
12.250 1.0616 0.03980 0.03248 -0.0289 0.0552 0.7571
12.500 1.0724 0.04101 0.03363 -0.0278 0.0434 0.7580
12.750 1.0834 0.04220 0.03479 -0.0267 0.0365 0.7591
13.000 1.0931 0.04355 0.03613 -0.0255 0.0319 0.7598
13.250 1.1034 0.04488 0.03749 -0.0245 0.0294 0.7607
13.500 1.1112 0.04645 0.03909 -0.0232 0.0273 0.7617
13.750 1.1222 0.04778 0.04050 -0.0224 0.0260 0.7628
14.000 1.1315 0.04927 0.04206 -0.0214 0.0249 0.7638
14.250 1.1398 0.05090 0.04373 -0.0205 0.0238 0.7649
14.500 1.1420 0.05313 0.04600 -0.0192 0.0226 0.7655
14.750 1.1525 0.05464 0.04760 -0.0185 0.0220 0.7663
15.000 1.1608 0.05638 0.04942 -0.0179 0.0212 0.7671
15.250 1.1682 0.05824 0.05135 -0.0172 0.0205 0.7679
15.500 1.1749 0.06021 0.05338 -0.0166 0.0200 0.7685
15.750 1.1793 0.06244 0.05565 -0.0159 0.0193 0.7690
16.000 1.1814 0.06497 0.05824 -0.0153 0.0189 0.7695
16.250 1.1854 0.06735 0.06070 -0.0147 0.0184 0.7700
16.500 1.1927 0.06942 0.06287 -0.0145 0.0180 0.7705
16.750 1.1997 0.07153 0.06507 -0.0143 0.0177 0.7710
17.000 1.2059 0.07379 0.06741 -0.0142 0.0172 0.7715
17.250 1.2116 0.07611 0.06982 -0.0141 0.0168 0.7720
17.500 1.2170 0.07852 0.07231 -0.0141 0.0164 0.7725
17.750 1.2220 0.08099 0.07483 -0.0143 0.0160 0.7730
18.000 1.2260 0.08359 0.07748 -0.0144 0.0157 0.7734
18.250 1.2298 0.08615 0.08008 -0.0144 0.0152 0.7739
18.500 1.2347 0.08865 0.08269 -0.0146 0.0150 0.7745
18.750 1.2378 0.09150 0.08568 -0.0151 0.0148 0.7752
19.000 1.2409 0.09435 0.08866 -0.0156 0.0146 0.7759
19.250 1.2437 0.09730 0.09174 -0.0161 0.0144 0.7766
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