J5012 12% (j5012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: J5012 12% (j5012-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.4 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-j5012-il-1000000-n5.txt Download as CSV file: xf-j5012-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: J5012 12%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.1128 0.11015 0.10730 -0.0173 1.0000 0.0088
-19.000 -1.1438 0.10074 0.09775 -0.0222 1.0000 0.0087
-18.750 -1.1783 0.09094 0.08779 -0.0272 1.0000 0.0087
-18.500 -1.2077 0.08222 0.07892 -0.0318 1.0000 0.0086
-18.250 -1.2311 0.07472 0.07128 -0.0357 1.0000 0.0086
-18.000 -1.2545 0.06741 0.06382 -0.0395 1.0000 0.0087
-17.750 -1.2700 0.06157 0.05785 -0.0424 1.0000 0.0086
-17.500 -1.2825 0.05641 0.05257 -0.0449 1.0000 0.0088
-17.250 -1.2895 0.05221 0.04827 -0.0467 1.0000 0.0089
-17.000 -1.2958 0.04831 0.04426 -0.0482 1.0000 0.0090
-16.750 -1.3021 0.04460 0.04044 -0.0493 1.0000 0.0090
-16.500 -1.3062 0.04137 0.03709 -0.0501 1.0000 0.0091
-16.250 -1.3020 0.03922 0.03486 -0.0503 1.0000 0.0093
-16.000 -1.3036 0.03656 0.03210 -0.0503 1.0000 0.0094
-15.750 -1.3018 0.03440 0.02985 -0.0500 1.0000 0.0095
-15.500 -1.2983 0.03254 0.02790 -0.0494 1.0000 0.0096
-15.250 -1.2930 0.03092 0.02619 -0.0486 1.0000 0.0098
-15.000 -1.2881 0.02937 0.02456 -0.0476 1.0000 0.0099
-14.750 -1.2828 0.02793 0.02303 -0.0463 1.0000 0.0101
-14.500 -1.2757 0.02672 0.02174 -0.0449 1.0000 0.0102
-14.250 -1.2673 0.02566 0.02060 -0.0433 1.0000 0.0103
-14.000 -1.2598 0.02459 0.01945 -0.0415 1.0000 0.0104
-13.750 -1.2507 0.02369 0.01847 -0.0397 1.0000 0.0105
-13.500 -1.2404 0.02290 0.01761 -0.0378 1.0000 0.0106
-13.250 -1.2333 0.02197 0.01661 -0.0354 1.0000 0.0108
-13.000 -1.2258 0.02112 0.01570 -0.0328 1.0000 0.0111
-12.750 -1.2171 0.02040 0.01492 -0.0302 1.0000 0.0113
-12.500 -1.2069 0.01981 0.01430 -0.0276 1.0000 0.0116
-12.250 -1.1967 0.01930 0.01375 -0.0249 1.0000 0.0119
-12.000 -1.1887 0.01880 0.01319 -0.0216 1.0000 0.0120
-11.750 -1.1807 0.01835 0.01270 -0.0181 1.0000 0.0123
-11.500 -1.1696 0.01790 0.01220 -0.0153 1.0000 0.0125
-11.250 -1.1569 0.01746 0.01171 -0.0127 1.0000 0.0128
-11.000 -1.1442 0.01702 0.01124 -0.0101 1.0000 0.0131
-10.750 -1.1309 0.01664 0.01080 -0.0075 1.0000 0.0132
-10.500 -1.1173 0.01627 0.01038 -0.0050 1.0000 0.0135
-10.250 -1.0981 0.01586 0.00994 -0.0036 0.9996 0.0137
-10.000 -1.0708 0.01529 0.00933 -0.0041 0.9983 0.0145
-9.750 -1.0425 0.01482 0.00885 -0.0047 0.9966 0.0152
-9.500 -1.0137 0.01439 0.00840 -0.0053 0.9948 0.0157
-9.250 -0.9855 0.01400 0.00797 -0.0058 0.9930 0.0163
-9.000 -0.9583 0.01363 0.00757 -0.0060 0.9906 0.0169
-8.750 -0.9300 0.01326 0.00718 -0.0064 0.9883 0.0175
-8.500 -0.9011 0.01286 0.00677 -0.0070 0.9862 0.0186
-8.250 -0.8710 0.01249 0.00640 -0.0078 0.9844 0.0201
-8.000 -0.8401 0.01217 0.00606 -0.0087 0.9830 0.0216
-7.750 -0.8146 0.01182 0.00573 -0.0084 0.9793 0.0239
-7.500 -0.7866 0.01152 0.00542 -0.0087 0.9760 0.0262
-7.250 -0.7568 0.01119 0.00510 -0.0093 0.9734 0.0293
-7.000 -0.7253 0.01089 0.00481 -0.0103 0.9714 0.0326
-6.750 -0.6922 0.01057 0.00452 -0.0117 0.9697 0.0370
-6.500 -0.6656 0.01033 0.00428 -0.0116 0.9644 0.0404
-6.250 -0.6349 0.01003 0.00401 -0.0124 0.9603 0.0466
-6.000 -0.6020 0.00975 0.00376 -0.0136 0.9569 0.0528
-5.750 -0.5722 0.00950 0.00353 -0.0142 0.9517 0.0595
-5.500 -0.5428 0.00923 0.00330 -0.0147 0.9452 0.0686
-5.250 -0.5120 0.00897 0.00308 -0.0155 0.9391 0.0793
-5.000 -0.4852 0.00871 0.00287 -0.0153 0.9301 0.0943
-4.750 -0.4579 0.00843 0.00267 -0.0153 0.9211 0.1135
-4.500 -0.4318 0.00818 0.00247 -0.0151 0.9108 0.1343
-4.250 -0.4064 0.00797 0.00231 -0.0146 0.8999 0.1529
-4.000 -0.3815 0.00775 0.00215 -0.0140 0.8886 0.1747
-3.750 -0.3569 0.00754 0.00200 -0.0133 0.8765 0.2000
-3.500 -0.3328 0.00734 0.00186 -0.0125 0.8637 0.2274
-3.250 -0.3087 0.00716 0.00173 -0.0118 0.8504 0.2522
-3.000 -0.2846 0.00699 0.00162 -0.0110 0.8364 0.2786
-2.750 -0.2611 0.00681 0.00151 -0.0101 0.8216 0.3104
-2.500 -0.2378 0.00662 0.00141 -0.0091 0.8066 0.3463
-2.250 -0.2141 0.00648 0.00132 -0.0082 0.7910 0.3772
-2.000 -0.1905 0.00635 0.00125 -0.0073 0.7748 0.4086
-1.750 -0.1666 0.00624 0.00118 -0.0064 0.7586 0.4363
-1.500 -0.1428 0.00614 0.00113 -0.0055 0.7414 0.4643
-1.250 -0.1191 0.00606 0.00108 -0.0046 0.7234 0.4937
-1.000 -0.0953 0.00599 0.00104 -0.0037 0.7049 0.5217
-0.750 -0.0714 0.00593 0.00101 -0.0028 0.6851 0.5483
-0.500 -0.0478 0.00589 0.00099 -0.0018 0.6638 0.5741
-0.250 -0.0239 0.00588 0.00098 -0.0009 0.6423 0.5976
0.000 0.0000 0.00587 0.00098 0.0000 0.6199 0.6200
0.250 0.0239 0.00589 0.00098 0.0009 0.5971 0.6416
0.500 0.0478 0.00590 0.00099 0.0018 0.5733 0.6633
0.750 0.0714 0.00593 0.00101 0.0028 0.5485 0.6850
1.000 0.0951 0.00600 0.00104 0.0037 0.5206 0.7049
1.250 0.1192 0.00606 0.00108 0.0046 0.4938 0.7231
1.500 0.1427 0.00614 0.00113 0.0055 0.4644 0.7416
1.750 0.1666 0.00624 0.00118 0.0064 0.4368 0.7585
2.000 0.1903 0.00635 0.00125 0.0073 0.4072 0.7751
2.250 0.2140 0.00648 0.00133 0.0082 0.3757 0.7912
2.500 0.2378 0.00662 0.00141 0.0091 0.3466 0.8067
2.750 0.2610 0.00681 0.00151 0.0101 0.3104 0.8216
3.000 0.2845 0.00699 0.00162 0.0110 0.2775 0.8367
3.250 0.3086 0.00716 0.00173 0.0118 0.2519 0.8503
3.500 0.3328 0.00734 0.00186 0.0126 0.2274 0.8637
3.750 0.3568 0.00754 0.00200 0.0133 0.1995 0.8766
4.000 0.3814 0.00775 0.00215 0.0140 0.1751 0.8885
4.500 0.4316 0.00819 0.00248 0.0151 0.1330 0.9108
4.750 0.4581 0.00842 0.00266 0.0153 0.1149 0.9212
5.000 0.4852 0.00871 0.00287 0.0153 0.0947 0.9302
5.250 0.5119 0.00897 0.00308 0.0155 0.0793 0.9392
5.500 0.5428 0.00923 0.00330 0.0147 0.0687 0.9452
5.750 0.5722 0.00950 0.00353 0.0142 0.0596 0.9517
6.000 0.6019 0.00976 0.00376 0.0137 0.0522 0.9569
6.250 0.6348 0.01003 0.00401 0.0124 0.0461 0.9603
6.500 0.6655 0.01033 0.00428 0.0116 0.0404 0.9643
6.750 0.6921 0.01058 0.00452 0.0117 0.0366 0.9697
7.000 0.7253 0.01089 0.00481 0.0103 0.0324 0.9714
7.250 0.7568 0.01119 0.00510 0.0093 0.0292 0.9734
7.500 0.7865 0.01152 0.00542 0.0087 0.0262 0.9760
7.750 0.8146 0.01182 0.00573 0.0084 0.0239 0.9793
8.000 0.8400 0.01218 0.00607 0.0087 0.0215 0.9830
8.250 0.8710 0.01250 0.00640 0.0078 0.0201 0.9844
8.500 0.9011 0.01285 0.00677 0.0070 0.0188 0.9862
8.750 0.9300 0.01327 0.00718 0.0064 0.0174 0.9883
9.000 0.9583 0.01363 0.00758 0.0060 0.0168 0.9907
9.250 0.9855 0.01400 0.00797 0.0058 0.0162 0.9930
9.500 1.0137 0.01440 0.00841 0.0053 0.0156 0.9948
9.750 1.0425 0.01483 0.00886 0.0047 0.0150 0.9966
10.000 1.0708 0.01530 0.00934 0.0041 0.0144 0.9983
10.250 1.0982 0.01587 0.00995 0.0036 0.0137 0.9996
10.500 1.1177 0.01625 0.01037 0.0049 0.0135 1.0000
10.750 1.1308 0.01664 0.01081 0.0075 0.0132 1.0000
11.000 1.1438 0.01705 0.01126 0.0101 0.0130 1.0000
11.250 1.1569 0.01746 0.01172 0.0127 0.0128 1.0000
11.500 1.1692 0.01792 0.01223 0.0153 0.0126 1.0000
11.750 1.1806 0.01836 0.01271 0.0181 0.0123 1.0000
12.000 1.1884 0.01881 0.01320 0.0216 0.0121 1.0000
12.250 1.1969 0.01930 0.01374 0.0248 0.0119 1.0000
12.500 1.2066 0.01983 0.01432 0.0276 0.0116 1.0000
12.750 1.2166 0.02043 0.01497 0.0303 0.0114 1.0000
13.000 1.2264 0.02110 0.01568 0.0327 0.0112 1.0000
13.250 1.2347 0.02190 0.01654 0.0352 0.0109 1.0000
13.500 1.2408 0.02290 0.01761 0.0377 0.0106 1.0000
13.750 1.2496 0.02378 0.01857 0.0398 0.0105 1.0000
14.000 1.2587 0.02469 0.01955 0.0416 0.0105 1.0000
14.250 1.2685 0.02560 0.02055 0.0432 0.0103 1.0000
14.500 1.2758 0.02675 0.02177 0.0448 0.0102 1.0000
14.750 1.2827 0.02798 0.02309 0.0462 0.0101 1.0000
15.000 1.2881 0.02941 0.02461 0.0475 0.0100 1.0000
15.250 1.2940 0.03089 0.02616 0.0485 0.0099 1.0000
15.500 1.3001 0.03244 0.02779 0.0492 0.0096 1.0000
15.750 1.3022 0.03444 0.02989 0.0499 0.0096 1.0000
16.000 1.3069 0.03632 0.03185 0.0501 0.0094 1.0000
16.250 1.3093 0.03855 0.03416 0.0502 0.0092 1.0000
16.500 1.3070 0.04139 0.03712 0.0498 0.0091 1.0000
16.750 1.3045 0.04446 0.04029 0.0492 0.0090 1.0000
17.000 1.3001 0.04793 0.04386 0.0481 0.0089 1.0000
17.250 1.2928 0.05196 0.04800 0.0466 0.0088 1.0000
17.500 1.2852 0.05624 0.05239 0.0447 0.0087 1.0000
17.750 1.2721 0.06150 0.05778 0.0422 0.0087 1.0000
18.000 1.2558 0.06747 0.06389 0.0391 0.0087 1.0000
18.250 1.2350 0.07437 0.07092 0.0356 0.0087 1.0000
18.500 1.2102 0.08213 0.07883 0.0315 0.0087 1.0000
18.750 1.1813 0.09079 0.08764 0.0270 0.0087 1.0000
19.000 1.1490 0.10021 0.09721 0.0221 0.0086 1.0000
19.250 1.1151 0.11015 0.10730 0.0169 0.0088 1.0000
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