SD7062 (14%) (sd7062-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: SD7062 (14%) (sd7062-il) Reynolds number: 500,000 Max Cl/Cd: 99.11 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sd7062-il-500000.txt Download as CSV file: xf-sd7062-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: SD7062 (14%)
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
------ -------- --------- --------- -------- -------- --------
-10.500 -0.2839 0.10278 0.10045 -0.0402 1.0000 0.0304
-10.250 -0.2827 0.09935 0.09705 -0.0413 1.0000 0.0310
-10.000 -0.3149 0.08823 0.08598 -0.0486 1.0000 0.0330
-9.750 -0.3076 0.08690 0.08469 -0.0476 1.0000 0.0333
-9.500 -0.3053 0.08466 0.08249 -0.0474 1.0000 0.0335
-9.250 -0.2200 0.05864 0.05657 -0.0694 0.9597 0.0382
-9.000 -0.2038 0.05529 0.05319 -0.0723 0.9426 0.0385
-8.750 -0.4363 0.02992 0.02561 -0.0973 0.9134 0.0244
-8.500 -0.4197 0.02772 0.02326 -0.0965 0.8989 0.0240
-8.250 -0.4050 0.02539 0.02063 -0.0956 0.8853 0.0239
-8.000 -0.3872 0.02366 0.01857 -0.0946 0.8726 0.0240
-7.750 -0.3670 0.02220 0.01682 -0.0938 0.8604 0.0241
-7.500 -0.3454 0.02078 0.01516 -0.0930 0.8499 0.0241
-7.250 -0.3225 0.01955 0.01370 -0.0924 0.8390 0.0241
-7.000 -0.2983 0.01856 0.01252 -0.0918 0.8290 0.0242
-6.750 -0.2746 0.01725 0.01103 -0.0912 0.8193 0.0244
-6.500 -0.2500 0.01616 0.00988 -0.0907 0.8096 0.0247
-6.250 -0.2249 0.01541 0.00905 -0.0902 0.8004 0.0251
-6.000 -0.1991 0.01479 0.00839 -0.0898 0.7907 0.0255
-5.750 -0.1733 0.01426 0.00776 -0.0893 0.7819 0.0260
-5.500 -0.1470 0.01374 0.00719 -0.0889 0.7723 0.0265
-5.000 -0.0938 0.01288 0.00619 -0.0881 0.7541 0.0279
-4.750 -0.0677 0.01241 0.00563 -0.0877 0.7456 0.0287
-4.500 -0.0410 0.01195 0.00518 -0.0875 0.7360 0.0299
-4.250 -0.0140 0.01165 0.00480 -0.0872 0.7274 0.0310
-4.000 0.0135 0.01134 0.00445 -0.0869 0.7178 0.0323
-3.750 0.0406 0.01100 0.00405 -0.0867 0.7091 0.0341
-3.500 0.0684 0.01074 0.00377 -0.0865 0.6995 0.0367
-3.250 0.0959 0.01048 0.00348 -0.0863 0.6907 0.0414
-3.000 0.1233 0.01008 0.00317 -0.0861 0.6811 0.0628
-2.750 0.1502 0.00963 0.00294 -0.0860 0.6721 0.1223
-2.500 0.1777 0.00934 0.00279 -0.0859 0.6625 0.1726
-2.250 0.2052 0.00909 0.00268 -0.0858 0.6533 0.2260
-2.000 0.2326 0.00886 0.00259 -0.0857 0.6435 0.2822
-1.750 0.2601 0.00862 0.00254 -0.0856 0.6340 0.3465
-1.500 0.2874 0.00844 0.00251 -0.0855 0.6245 0.4118
-1.250 0.3151 0.00830 0.00250 -0.0853 0.6148 0.4663
-1.000 0.3425 0.00823 0.00249 -0.0851 0.6054 0.5150
-0.750 0.3702 0.00815 0.00251 -0.0849 0.5953 0.5567
-0.500 0.3976 0.00811 0.00252 -0.0846 0.5859 0.5955
-0.250 0.4251 0.00808 0.00254 -0.0843 0.5758 0.6302
0.000 0.4526 0.00807 0.00256 -0.0840 0.5661 0.6624
0.250 0.4797 0.00808 0.00260 -0.0837 0.5562 0.6950
0.500 0.5067 0.00806 0.00264 -0.0833 0.5463 0.7284
0.750 0.5330 0.00808 0.00269 -0.0827 0.5367 0.7612
1.000 0.5593 0.00807 0.00274 -0.0821 0.5265 0.7946
1.250 0.5845 0.00808 0.00280 -0.0813 0.5170 0.8301
1.500 0.6086 0.00808 0.00286 -0.0801 0.5070 0.8690
1.750 0.6314 0.00807 0.00291 -0.0787 0.4977 0.9145
2.000 0.6651 0.00812 0.00292 -0.0796 0.4872 0.9681
2.250 0.7016 0.00821 0.00296 -0.0814 0.4764 1.0000
2.500 0.7286 0.00837 0.00302 -0.0812 0.4669 1.0000
2.750 0.7558 0.00851 0.00310 -0.0811 0.4567 1.0000
3.000 0.7829 0.00867 0.00319 -0.0809 0.4472 1.0000
3.250 0.8097 0.00884 0.00329 -0.0807 0.4374 1.0000
3.500 0.8369 0.00899 0.00340 -0.0805 0.4276 1.0000
3.750 0.8632 0.00921 0.00352 -0.0802 0.4181 1.0000
4.000 0.8903 0.00935 0.00365 -0.0801 0.4086 1.0000
4.250 0.9166 0.00956 0.00379 -0.0798 0.3993 1.0000
4.500 0.9431 0.00975 0.00394 -0.0796 0.3897 1.0000
4.750 0.9693 0.00995 0.00409 -0.0793 0.3807 1.0000
5.000 0.9952 0.01018 0.00426 -0.0789 0.3712 1.0000
5.250 1.0214 0.01037 0.00444 -0.0787 0.3623 1.0000
5.500 1.0465 0.01064 0.00463 -0.0782 0.3531 1.0000
5.750 1.0726 0.01083 0.00482 -0.0779 0.3441 1.0000
6.000 1.0972 0.01112 0.00505 -0.0774 0.3354 1.0000
6.250 1.1229 0.01133 0.00525 -0.0771 0.3267 1.0000
6.500 1.1472 0.01162 0.00549 -0.0766 0.3182 1.0000
6.750 1.1722 0.01186 0.00573 -0.0761 0.3096 1.0000
7.000 1.1960 0.01217 0.00599 -0.0755 0.3014 1.0000
7.250 1.2204 0.01243 0.00625 -0.0750 0.2932 1.0000
7.500 1.2435 0.01275 0.00655 -0.0743 0.2854 1.0000
7.750 1.2671 0.01304 0.00683 -0.0737 0.2774 1.0000
8.000 1.2893 0.01339 0.00715 -0.0729 0.2699 1.0000
8.250 1.3123 0.01369 0.00746 -0.0722 0.2623 1.0000
8.500 1.3330 0.01409 0.00782 -0.0712 0.2550 1.0000
8.750 1.3553 0.01439 0.00814 -0.0704 0.2477 1.0000
9.000 1.3740 0.01486 0.00856 -0.0691 0.2406 1.0000
9.250 1.3956 0.01515 0.00890 -0.0682 0.2340 1.0000
9.500 1.4120 0.01561 0.00932 -0.0665 0.2271 1.0000
9.750 1.4297 0.01598 0.00973 -0.0650 0.2210 1.0000
10.000 1.4452 0.01644 0.01018 -0.0632 0.2145 1.0000
10.250 1.4597 0.01696 0.01070 -0.0613 0.2085 1.0000
10.500 1.4758 0.01743 0.01120 -0.0598 0.2025 1.0000
10.750 1.4875 0.01811 0.01186 -0.0577 0.1964 1.0000
11.000 1.5036 0.01862 0.01242 -0.0563 0.1909 1.0000
11.250 1.5162 0.01932 0.01312 -0.0546 0.1850 1.0000
11.500 1.5276 0.02011 0.01392 -0.0528 0.1797 1.0000
11.750 1.5416 0.02080 0.01466 -0.0514 0.1743 1.0000
12.000 1.5506 0.02179 0.01564 -0.0496 0.1689 1.0000
12.250 1.5628 0.02266 0.01656 -0.0483 0.1639 1.0000
12.500 1.5736 0.02364 0.01757 -0.0469 0.1587 1.0000
12.750 1.5792 0.02501 0.01893 -0.0452 0.1537 1.0000
13.000 1.5919 0.02596 0.01997 -0.0442 0.1494 1.0000
13.250 1.6002 0.02726 0.02129 -0.0430 0.1448 1.0000
13.500 1.6031 0.02902 0.02304 -0.0416 0.1402 1.0000
13.750 1.6146 0.03018 0.02430 -0.0408 0.1363 1.0000
14.000 1.6209 0.03179 0.02595 -0.0399 0.1320 1.0000
14.250 1.6218 0.03392 0.02808 -0.0389 0.1278 1.0000
14.500 1.6303 0.03546 0.02971 -0.0382 0.1244 1.0000
14.750 1.6351 0.03736 0.03168 -0.0376 0.1206 1.0000
15.000 1.6349 0.03980 0.03413 -0.0370 0.1169 1.0000
15.250 1.6370 0.04211 0.03651 -0.0366 0.1137 1.0000
15.500 1.6418 0.04422 0.03870 -0.0363 0.1103 1.0000
15.750 1.6419 0.04688 0.04142 -0.0361 0.1072 1.0000
16.000 1.6368 0.05021 0.04477 -0.0362 0.1040 1.0000
16.250 1.6401 0.05270 0.04736 -0.0362 0.1013 1.0000
16.500 1.6411 0.05552 0.05027 -0.0365 0.0984 1.0000
16.750 1.6376 0.05896 0.05376 -0.0369 0.0956 1.0000
17.000 1.6290 0.06311 0.05795 -0.0376 0.0927 1.0000
17.250 1.6305 0.06609 0.06104 -0.0382 0.0904 1.0000
17.500 1.6288 0.06956 0.06460 -0.0390 0.0877 1.0000
17.750 1.6229 0.07367 0.06877 -0.0401 0.0852 1.0000
18.000 1.6128 0.07841 0.07355 -0.0414 0.0828 1.0000
18.250 1.6096 0.08230 0.07755 -0.0426 0.0807 1.0000
18.500 1.6068 0.08620 0.08155 -0.0439 0.0784 1.0000
18.750 1.6002 0.09074 0.08616 -0.0455 0.0762 1.0000
19.000 1.5896 0.09590 0.09137 -0.0474 0.0740 1.0000
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