WORTMANN FX 2 AIRFOIL (fx2-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 2 AIRFOIL (fx2-il) Reynolds number: 500,000 Max Cl/Cd: 50.48 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx2-il-500000-n5.txt Download as CSV file: xf-fx2-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.5210 0.09132 0.08647 -0.1598 0.8226 0.0093
-19.500 -0.5337 0.08567 0.08071 -0.1629 0.8224 0.0094
-19.250 -0.5449 0.08048 0.07541 -0.1657 0.8221 0.0094
-19.000 -0.5538 0.07576 0.07057 -0.1682 0.8218 0.0094
-18.750 -0.5605 0.07145 0.06616 -0.1706 0.8215 0.0096
-18.500 -0.5660 0.06749 0.06211 -0.1726 0.8212 0.0097
-18.250 -0.5663 0.06430 0.05883 -0.1743 0.8209 0.0098
-18.000 -0.5690 0.06095 0.05538 -0.1758 0.8205 0.0099
-17.750 -0.5700 0.05793 0.05228 -0.1771 0.8202 0.0100
-17.500 -0.5690 0.05523 0.04949 -0.1781 0.8198 0.0103
-17.250 -0.5670 0.05276 0.04692 -0.1790 0.8195 0.0104
-17.000 -0.5628 0.05057 0.04464 -0.1797 0.8191 0.0107
-16.750 -0.5605 0.04829 0.04227 -0.1803 0.8187 0.0108
-16.500 -0.5552 0.04637 0.04027 -0.1807 0.8183 0.0110
-16.250 -0.5482 0.04465 0.03846 -0.1810 0.8180 0.0113
-16.000 -0.5418 0.04294 0.03666 -0.1812 0.8176 0.0115
-15.750 -0.5376 0.04111 0.03477 -0.1812 0.8172 0.0118
-15.500 -0.5309 0.03953 0.03314 -0.1812 0.8168 0.0122
-15.250 -0.5237 0.03805 0.03161 -0.1811 0.8164 0.0124
-15.000 -0.5145 0.03675 0.03025 -0.1809 0.8160 0.0127
-14.750 -0.5038 0.03561 0.02904 -0.1808 0.8156 0.0131
-14.500 -0.4933 0.03449 0.02786 -0.1805 0.8153 0.0135
-14.250 -0.4828 0.03339 0.02671 -0.1801 0.8149 0.0139
-14.000 -0.4703 0.03247 0.02573 -0.1798 0.8145 0.0146
-13.750 -0.4596 0.03145 0.02465 -0.1793 0.8141 0.0152
-13.500 -0.4483 0.03050 0.02367 -0.1788 0.8136 0.0158
-13.250 -0.4362 0.02964 0.02277 -0.1782 0.8131 0.0164
-13.000 -0.4243 0.02878 0.02187 -0.1776 0.8126 0.0171
-12.750 -0.4105 0.02806 0.02110 -0.1770 0.8122 0.0181
-12.500 -0.3970 0.02735 0.02034 -0.1764 0.8118 0.0189
-12.250 -0.3851 0.02658 0.01956 -0.1755 0.8114 0.0206
-12.000 -0.3715 0.02593 0.01890 -0.1748 0.8110 0.0219
-11.750 -0.3573 0.02533 0.01827 -0.1741 0.8106 0.0235
-11.500 -0.3441 0.02472 0.01766 -0.1732 0.8102 0.0262
-11.250 -0.3299 0.02418 0.01711 -0.1724 0.8098 0.0286
-11.000 -0.3152 0.02370 0.01664 -0.1715 0.8094 0.0319
-10.750 -0.3005 0.02324 0.01619 -0.1706 0.8091 0.0357
-10.500 -0.2860 0.02279 0.01574 -0.1696 0.8088 0.0386
-10.250 -0.2711 0.02237 0.01533 -0.1686 0.8084 0.0420
-10.000 -0.2552 0.02201 0.01495 -0.1677 0.8081 0.0447
-9.750 -0.2414 0.02158 0.01453 -0.1665 0.8077 0.0474
-9.500 -0.2270 0.02119 0.01415 -0.1653 0.8073 0.0496
-9.250 -0.2118 0.02085 0.01380 -0.1642 0.8069 0.0522
-9.000 -0.1963 0.02053 0.01346 -0.1631 0.8065 0.0540
-8.750 -0.1837 0.02013 0.01307 -0.1616 0.8059 0.0565
-8.500 -0.1712 0.01974 0.01268 -0.1600 0.8052 0.0590
-8.250 -0.1580 0.01938 0.01233 -0.1585 0.8046 0.0614
-8.000 -0.1441 0.01908 0.01201 -0.1570 0.8040 0.0640
-7.750 -0.1291 0.01882 0.01174 -0.1557 0.8034 0.0662
-7.500 -0.1190 0.01842 0.01135 -0.1536 0.8028 0.0697
-7.250 -0.1086 0.01805 0.01100 -0.1515 0.8021 0.0733
-7.000 -0.0973 0.01773 0.01068 -0.1495 0.8015 0.0760
-6.750 -0.0859 0.01743 0.01037 -0.1475 0.8008 0.0791
-6.500 -0.0763 0.01710 0.01004 -0.1452 0.8001 0.0840
-6.250 -0.0703 0.01672 0.00970 -0.1422 0.7994 0.0917
-6.000 -0.0705 0.01635 0.00939 -0.1382 0.7985 0.1046
-5.750 -0.0789 0.01590 0.00905 -0.1329 0.7975 0.1288
-5.500 -0.0739 0.01537 0.00861 -0.1301 0.7966 0.1613
-5.250 -0.0657 0.01486 0.00826 -0.1278 0.7959 0.2026
-5.000 -0.0566 0.01423 0.00786 -0.1257 0.7953 0.2645
-4.750 -0.0462 0.01340 0.00738 -0.1241 0.7946 0.3559
-4.500 -0.0330 0.01259 0.00698 -0.1229 0.7940 0.4551
-4.250 -0.0272 0.01252 0.00722 -0.1194 0.7925 0.5312
-4.000 -0.0227 0.01286 0.00764 -0.1154 0.7900 0.5522
-3.750 -0.0134 0.01313 0.00797 -0.1122 0.7878 0.5702
-3.500 -0.0005 0.01339 0.00829 -0.1097 0.7861 0.5866
-3.250 0.0170 0.01362 0.00857 -0.1081 0.7848 0.5995
-3.000 0.0381 0.01382 0.00880 -0.1071 0.7838 0.6117
-2.750 0.0637 0.01394 0.00891 -0.1069 0.7831 0.6225
-2.500 0.0902 0.01411 0.00908 -0.1069 0.7825 0.6298
-2.250 0.1165 0.01421 0.00911 -0.1071 0.7819 0.6365
-2.000 0.1435 0.01435 0.00925 -0.1072 0.7814 0.6394
-1.750 0.1726 0.01444 0.00932 -0.1078 0.7810 0.6430
-1.500 0.2038 0.01450 0.00932 -0.1089 0.7807 0.6487
-1.250 0.2361 0.01453 0.00932 -0.1101 0.7803 0.6518
-1.000 0.2689 0.01453 0.00931 -0.1115 0.7800 0.6531
-0.750 0.3022 0.01453 0.00929 -0.1130 0.7797 0.6545
0.750 0.2653 0.01941 0.01418 -0.0788 0.7446 0.6672
1.000 0.2918 0.01945 0.01422 -0.0789 0.7432 0.6684
1.250 0.3203 0.01942 0.01420 -0.0794 0.7422 0.6698
1.500 0.3494 0.01937 0.01415 -0.0800 0.7414 0.6712
1.750 0.3795 0.01928 0.01407 -0.0807 0.7407 0.6728
2.000 0.4098 0.01918 0.01397 -0.0815 0.7402 0.6746
2.250 0.4408 0.01905 0.01384 -0.0825 0.7396 0.6764
2.500 0.4722 0.01890 0.01368 -0.0835 0.7392 0.6783
2.750 0.5032 0.01873 0.01350 -0.0844 0.7385 0.6799
3.500 0.5498 0.01947 0.01434 -0.0793 0.7236 0.6833
3.750 0.5908 0.01886 0.01376 -0.0817 0.7252 0.6844
4.250 0.6168 0.01958 0.01454 -0.0775 0.7125 0.6871
4.750 0.6536 0.01983 0.01483 -0.0751 0.6981 0.6898
5.000 0.6642 0.02039 0.01540 -0.0727 0.6869 0.6912
5.250 0.6990 0.01987 0.01490 -0.0741 0.6833 0.6924
5.500 0.7206 0.01996 0.01499 -0.0734 0.6725 0.6937
5.750 0.7633 0.01899 0.01398 -0.0759 0.6598 0.6947
6.000 0.8112 0.01784 0.01276 -0.0791 0.6444 0.6956
6.250 0.8502 0.01704 0.01183 -0.0809 0.6207 0.6965
6.500 0.8687 0.01721 0.01191 -0.0796 0.5957 0.6974
6.750 0.8802 0.01771 0.01230 -0.0773 0.5710 0.6984
7.000 0.8871 0.01845 0.01292 -0.0743 0.5441 0.6994
7.250 0.8861 0.01954 0.01384 -0.0701 0.5084 0.7004
7.500 0.8858 0.02067 0.01480 -0.0662 0.4713 0.7016
7.750 0.8849 0.02192 0.01586 -0.0624 0.4341 0.7026
8.000 0.8878 0.02305 0.01683 -0.0592 0.3987 0.7036
8.250 0.8888 0.02432 0.01787 -0.0559 0.3551 0.7045
8.500 0.8908 0.02563 0.01894 -0.0528 0.3112 0.7054
8.750 0.8930 0.02697 0.02001 -0.0499 0.2601 0.7062
9.000 0.8987 0.02817 0.02097 -0.0475 0.2154 0.7070
9.250 0.9065 0.02930 0.02191 -0.0455 0.1790 0.7077
9.500 0.9195 0.03017 0.02270 -0.0442 0.1596 0.7084
9.750 0.9302 0.03120 0.02358 -0.0426 0.1309 0.7091
10.000 0.9398 0.03233 0.02453 -0.0410 0.0990 0.7097
10.250 0.9527 0.03328 0.02539 -0.0398 0.0840 0.7104
10.500 0.9669 0.03417 0.02625 -0.0388 0.0761 0.7112
10.750 0.9823 0.03495 0.02706 -0.0379 0.0704 0.7121
11.000 0.9975 0.03577 0.02790 -0.0370 0.0652 0.7128
11.250 1.0126 0.03662 0.02876 -0.0361 0.0601 0.7134
11.500 1.0282 0.03745 0.02961 -0.0354 0.0543 0.7141
11.750 1.0420 0.03841 0.03058 -0.0345 0.0479 0.7147
12.000 1.0538 0.03952 0.03165 -0.0334 0.0359 0.7157
12.250 1.0641 0.04078 0.03283 -0.0322 0.0260 0.7164
12.500 1.0759 0.04196 0.03402 -0.0312 0.0224 0.7173
12.750 1.0882 0.04313 0.03522 -0.0302 0.0200 0.7180
13.000 1.1001 0.04434 0.03648 -0.0293 0.0183 0.7186
13.250 1.1120 0.04558 0.03775 -0.0285 0.0170 0.7194
13.500 1.1242 0.04680 0.03906 -0.0277 0.0162 0.7202
13.750 1.1361 0.04806 0.04038 -0.0269 0.0153 0.7210
14.000 1.1474 0.04941 0.04177 -0.0261 0.0145 0.7219
14.250 1.1563 0.05099 0.04340 -0.0253 0.0136 0.7226
14.500 1.1663 0.05251 0.04499 -0.0245 0.0132 0.7231
14.750 1.1771 0.05398 0.04653 -0.0239 0.0127 0.7237
15.000 1.1867 0.05558 0.04819 -0.0232 0.0122 0.7241
15.250 1.1965 0.05718 0.04987 -0.0227 0.0119 0.7245
15.500 1.2044 0.05900 0.05176 -0.0221 0.0114 0.7249
15.750 1.2122 0.06086 0.05368 -0.0215 0.0110 0.7252
16.000 1.2178 0.06298 0.05586 -0.0210 0.0106 0.7256
16.250 1.2248 0.06499 0.05794 -0.0206 0.0102 0.7259
16.500 1.2302 0.06723 0.06027 -0.0202 0.0100 0.7262
16.750 1.2372 0.06932 0.06246 -0.0199 0.0097 0.7266
17.250 1.2474 0.07400 0.06732 -0.0196 0.0092 0.7274
17.500 1.2519 0.07646 0.06987 -0.0195 0.0089 0.7278
17.750 1.2559 0.07905 0.07255 -0.0196 0.0087 0.7282
18.000 1.2588 0.08180 0.07539 -0.0197 0.0086 0.7287
18.250 1.2600 0.08480 0.07849 -0.0200 0.0084 0.7291
18.500 1.2603 0.08800 0.08178 -0.0203 0.0083 0.7295
18.750 1.2576 0.09163 0.08550 -0.0209 0.0080 0.7299
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