WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=1,000,000 Ncrit=0
| Details | Polar file |
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Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il) Reynolds number: 1,000,000 Max Cl/Cd: 54.26 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx3-il-1000000.txt Download as CSV file: xf-fx3-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-20.000 -0.5597 0.13284 0.12991 -0.1019 0.8110 0.0086
-19.750 -0.6075 0.11909 0.11600 -0.1084 0.8111 0.0085
-19.500 -0.6463 0.10759 0.10434 -0.1143 0.8112 0.0085
-19.250 -0.6762 0.09822 0.09483 -0.1193 0.8113 0.0084
-19.000 -0.6990 0.09035 0.08682 -0.1236 0.8114 0.0084
-18.750 -0.7170 0.08358 0.07991 -0.1274 0.8114 0.0084
-18.500 -0.7307 0.07780 0.07401 -0.1305 0.8115 0.0085
-18.250 -0.7402 0.07284 0.06893 -0.1332 0.8116 0.0085
-18.000 -0.7472 0.06844 0.06442 -0.1355 0.8117 0.0085
-17.750 -0.7547 0.06423 0.06009 -0.1374 0.8118 0.0086
-17.500 -0.7704 0.05928 0.05498 -0.1391 0.8119 0.0087
-17.250 -0.7803 0.05525 0.05082 -0.1403 0.8120 0.0088
-17.000 -0.7850 0.05200 0.04747 -0.1412 0.8121 0.0090
-16.750 -0.7854 0.04929 0.04469 -0.1418 0.8122 0.0091
-16.500 -0.7824 0.04702 0.04235 -0.1424 0.8123 0.0093
-16.250 -0.7769 0.04510 0.04036 -0.1427 0.8124 0.0094
-16.000 -0.7697 0.04337 0.03858 -0.1430 0.8126 0.0096
-15.750 -0.7618 0.04177 0.03691 -0.1432 0.8127 0.0098
-15.500 -0.7525 0.04033 0.03542 -0.1434 0.8128 0.0100
-15.250 -0.7427 0.03899 0.03400 -0.1434 0.8130 0.0102
-15.000 -0.7315 0.03779 0.03275 -0.1434 0.8131 0.0104
-14.750 -0.7197 0.03667 0.03157 -0.1434 0.8133 0.0107
-14.500 -0.7060 0.03571 0.03055 -0.1435 0.8134 0.0109
-14.250 -0.6912 0.03487 0.02966 -0.1435 0.8136 0.0111
-14.000 -0.6827 0.03361 0.02832 -0.1430 0.8137 0.0114
-13.750 -0.6747 0.03234 0.02700 -0.1424 0.8139 0.0119
-13.500 -0.6615 0.03147 0.02610 -0.1421 0.8141 0.0123
-13.250 -0.6465 0.03076 0.02535 -0.1420 0.8143 0.0127
-13.000 -0.6309 0.03010 0.02466 -0.1418 0.8144 0.0131
-12.750 -0.6149 0.02950 0.02402 -0.1416 0.8146 0.0135
-12.500 -0.5981 0.02897 0.02347 -0.1414 0.8148 0.0140
-12.250 -0.5804 0.02852 0.02298 -0.1412 0.8150 0.0144
-12.000 -0.5673 0.02778 0.02219 -0.1406 0.8149 0.0151
-11.750 -0.5530 0.02717 0.02157 -0.1400 0.8149 0.0160
-11.500 -0.5363 0.02677 0.02116 -0.1396 0.8151 0.0169
-11.250 -0.5193 0.02643 0.02080 -0.1392 0.8153 0.0178
-11.000 -0.5015 0.02617 0.02051 -0.1389 0.8155 0.0185
-10.750 -0.4878 0.02574 0.02008 -0.1380 0.8157 0.0203
-10.500 -0.4718 0.02549 0.01985 -0.1374 0.8160 0.0220
-10.250 -0.4550 0.02534 0.01969 -0.1367 0.8163 0.0236
-10.000 -0.4406 0.02516 0.01954 -0.1358 0.8166 0.0265
-9.750 -0.4248 0.02514 0.01954 -0.1349 0.8171 0.0296
-9.500 -0.4144 0.02609 0.02049 -0.1330 0.8193 0.0326
-9.250 -0.3930 0.02556 0.01999 -0.1330 0.8196 0.0365
-9.000 -0.3690 0.02513 0.01955 -0.1334 0.8201 0.0385
-8.750 -0.4350 0.02952 0.02408 -0.1204 0.8350 0.0375
-8.500 -0.7125 0.03077 0.02511 -0.0661 0.8135 0.0225
-8.250 -0.7001 0.03037 0.02467 -0.0646 0.8118 0.0239
-8.000 -0.6827 0.02990 0.02423 -0.0641 0.8107 0.0276
-7.750 -0.6602 0.02965 0.02397 -0.0643 0.8100 0.0306
-7.500 -0.6350 0.02934 0.02371 -0.0651 0.8094 0.0356
-7.250 -0.6077 0.02925 0.02361 -0.0660 0.8089 0.0383
-7.000 -0.5806 0.02897 0.02336 -0.0671 0.8084 0.0420
-6.750 -0.5523 0.02887 0.02327 -0.0683 0.8081 0.0448
-6.500 -0.5233 0.02885 0.02323 -0.0695 0.8078 0.0467
-6.250 -0.4929 0.02865 0.02301 -0.0713 0.8075 0.0496
-6.000 -0.4617 0.02851 0.02290 -0.0732 0.8073 0.0525
-5.750 -0.4302 0.02848 0.02287 -0.0750 0.8070 0.0550
-5.500 -0.3978 0.02848 0.02286 -0.0768 0.8068 0.0568
-5.250 -0.4116 0.02874 0.02309 -0.0717 0.7989 0.0571
-5.000 -0.3788 0.02851 0.02284 -0.0738 0.7976 0.0604
-4.750 -0.3447 0.02834 0.02269 -0.0761 0.7966 0.0647
-4.500 -0.3111 0.02825 0.02261 -0.0781 0.7959 0.0683
-4.250 -0.2771 0.02821 0.02255 -0.0801 0.7953 0.0714
-4.000 -0.2399 0.02803 0.02242 -0.0829 0.7949 0.0807
-3.750 -0.2022 0.02789 0.02233 -0.0858 0.7945 0.0946
-3.500 -0.0751 0.02560 0.02225 -0.1146 0.7959 0.6024
-3.250 -0.0507 0.02610 0.02276 -0.1134 0.7950 0.6472
-3.000 -0.0223 0.02652 0.02314 -0.1132 0.7943 0.6565
-2.750 0.0043 0.02708 0.02369 -0.1123 0.7938 0.6640
-2.500 0.0107 0.02725 0.02390 -0.1079 0.7848 0.6681
-2.250 0.0267 0.02780 0.02450 -0.1046 0.7833 0.6710
-2.000 0.0512 0.02813 0.02484 -0.1035 0.7824 0.6739
-1.750 0.0874 0.02837 0.02499 -0.1056 0.7819 0.6791
-1.500 0.1152 0.02839 0.02503 -0.1055 0.7814 0.6803
-1.250 0.1388 0.02863 0.02530 -0.1040 0.7810 0.6816
-1.000 0.1628 0.02887 0.02557 -0.1025 0.7806 0.6830
-0.750 0.1622 0.02934 0.02606 -0.0978 0.7724 0.6845
-0.500 0.1866 0.02956 0.02629 -0.0970 0.7713 0.6874
-0.250 0.2210 0.02970 0.02639 -0.0988 0.7706 0.6940
0.000 0.2471 0.02968 0.02638 -0.0983 0.7700 0.6947
0.250 0.2779 0.02957 0.02627 -0.0991 0.7695 0.6952
0.500 0.3083 0.02947 0.02618 -0.0998 0.7691 0.6958
0.750 0.3393 0.02937 0.02608 -0.1006 0.7688 0.6964
1.000 0.3714 0.02923 0.02594 -0.1016 0.7685 0.6970
1.250 0.4048 0.02905 0.02575 -0.1030 0.7682 0.6977
1.500 0.4394 0.02881 0.02552 -0.1046 0.7680 0.6983
1.750 0.4741 0.02856 0.02527 -0.1062 0.7678 0.6990
2.000 0.5093 0.02830 0.02501 -0.1079 0.7676 0.6999
2.250 0.5450 0.02803 0.02475 -0.1099 0.7673 0.7009
2.500 0.5817 0.02774 0.02447 -0.1121 0.7671 0.7016
2.750 0.5852 0.02801 0.02475 -0.1094 0.7575 0.7025
3.000 0.6220 0.02773 0.02447 -0.1118 0.7572 0.7035
3.250 0.6586 0.02743 0.02417 -0.1140 0.7569 0.7040
3.500 0.6952 0.02714 0.02390 -0.1163 0.7565 0.7049
3.750 0.7325 0.02694 0.02370 -0.1185 0.7562 0.7062
4.000 0.7663 0.02663 0.02339 -0.1201 0.7547 0.7068
4.250 0.8151 0.02536 0.02215 -0.1243 0.7551 0.7072
4.500 0.8259 0.02552 0.02233 -0.1224 0.7459 0.7073
4.750 0.8472 0.02538 0.02222 -0.1219 0.7378 0.7072
5.000 0.8862 0.02454 0.02140 -0.1242 0.7337 0.7071
6.250 1.0711 0.01974 0.01598 -0.1330 0.6002 0.7063
6.500 1.0633 0.02126 0.01729 -0.1279 0.5592 0.7061
6.750 1.0599 0.02271 0.01849 -0.1237 0.5135 0.7060
7.000 1.0581 0.02414 0.01965 -0.1196 0.4615 0.7062
7.250 1.0597 0.02542 0.02063 -0.1163 0.4077 0.7060
7.500 1.0647 0.02654 0.02146 -0.1135 0.3533 0.7058
7.750 1.0714 0.02761 0.02222 -0.1110 0.2958 0.7057
8.000 1.0782 0.02868 0.02296 -0.1085 0.2377 0.7055
8.250 1.0864 0.02975 0.02371 -0.1063 0.1816 0.7053
8.500 1.0984 0.03067 0.02440 -0.1047 0.1430 0.7052
8.750 1.1124 0.03149 0.02506 -0.1034 0.1141 0.7051
9.000 1.1290 0.03221 0.02568 -0.1025 0.0954 0.7049
9.250 1.1467 0.03287 0.02629 -0.1018 0.0824 0.7048
9.500 1.1642 0.03356 0.02692 -0.1011 0.0709 0.7047
9.750 1.1806 0.03434 0.02763 -0.1002 0.0589 0.7046
10.000 1.1931 0.03536 0.02851 -0.0988 0.0399 0.7045
10.250 1.2049 0.03643 0.02947 -0.0973 0.0252 0.7044
10.500 1.2196 0.03735 0.03036 -0.0962 0.0206 0.7043
10.750 1.2369 0.03811 0.03117 -0.0955 0.0192 0.7043
11.000 1.2524 0.03899 0.03206 -0.0945 0.0176 0.7042
11.250 1.2656 0.04005 0.03315 -0.0932 0.0158 0.7041
11.500 1.2822 0.04088 0.03402 -0.0925 0.0152 0.7041
11.750 1.2975 0.04182 0.03500 -0.0916 0.0145 0.7040
12.000 1.3121 0.04280 0.03600 -0.0907 0.0138 0.7039
12.250 1.3251 0.04390 0.03714 -0.0896 0.0130 0.7039
12.500 1.3332 0.04539 0.03869 -0.0878 0.0122 0.7038
12.750 1.3480 0.04642 0.03977 -0.0870 0.0119 0.7038
13.000 1.3611 0.04757 0.04097 -0.0860 0.0115 0.7038
13.250 1.3741 0.04874 0.04219 -0.0850 0.0111 0.7039
13.500 1.3868 0.04994 0.04343 -0.0840 0.0107 0.7040
13.750 1.3985 0.05125 0.04478 -0.0830 0.0103 0.7039
14.000 1.4080 0.05275 0.04632 -0.0818 0.0099 0.7039
14.250 1.4125 0.05469 0.04833 -0.0801 0.0095 0.7038
14.500 1.4163 0.05676 0.05048 -0.0785 0.0093 0.7037
14.750 1.4271 0.05825 0.05204 -0.0776 0.0091 0.7036
15.000 1.4364 0.05990 0.05375 -0.0767 0.0089 0.7036
15.250 1.4445 0.06168 0.05560 -0.0757 0.0087 0.7035
15.500 1.4519 0.06353 0.05752 -0.0747 0.0085 0.7034
15.750 1.4585 0.06550 0.05956 -0.0738 0.0083 0.7034
16.000 1.4653 0.06747 0.06160 -0.0729 0.0081 0.7033
16.250 1.4707 0.06963 0.06382 -0.0721 0.0079 0.7033
16.500 1.4755 0.07188 0.06614 -0.0713 0.0078 0.7032
16.750 1.4788 0.07435 0.06867 -0.0706 0.0076 0.7031
17.000 1.4795 0.07713 0.07153 -0.0698 0.0075 0.7031
17.250 1.4765 0.08035 0.07484 -0.0689 0.0073 0.7030
17.500 1.4683 0.08418 0.07878 -0.0680 0.0072 0.7029
17.750 1.4636 0.08770 0.08241 -0.0674 0.0070 0.7029
18.000 1.4648 0.09066 0.08547 -0.0672 0.0070 0.7028
18.250 1.4670 0.09353 0.08843 -0.0673 0.0069 0.7028
18.500 1.4672 0.09668 0.09167 -0.0674 0.0068 0.7027
18.750 1.4674 0.09988 0.09498 -0.0676 0.0067 0.7027
19.000 1.4653 0.10340 0.09859 -0.0680 0.0066 0.7026
19.250 1.4638 0.10689 0.10219 -0.0686 0.0065 0.7026
19.500 1.4597 0.11076 0.10617 -0.0693 0.0064 0.7025
19.750 1.4579 0.11443 0.10993 -0.0702 0.0063 0.7025
20.000 1.4530 0.11856 0.11416 -0.0713 0.0062 0.7024
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