NACA 2415 (naca2415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 2415 (naca2415-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.23 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca2415-il-1000000.txt Download as CSV file: xf-naca2415-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 2415
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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.1460 0.08857 0.08524 -0.0453 1.0000 0.0263
-18.750 -1.1614 0.08261 0.07919 -0.0485 1.0000 0.0265
-18.500 -1.1772 0.07671 0.07319 -0.0517 1.0000 0.0266
-18.250 -1.1917 0.07106 0.06745 -0.0548 1.0000 0.0268
-18.000 -1.2059 0.06558 0.06185 -0.0577 1.0000 0.0269
-17.750 -1.2180 0.06041 0.05658 -0.0605 1.0000 0.0271
-17.500 -1.2279 0.05558 0.05164 -0.0632 1.0000 0.0273
-17.250 -1.2349 0.05117 0.04712 -0.0656 1.0000 0.0275
-17.000 -1.2390 0.04720 0.04304 -0.0678 1.0000 0.0277
-16.750 -1.2401 0.04372 0.03946 -0.0697 1.0000 0.0279
-16.500 -1.2386 0.04066 0.03628 -0.0713 1.0000 0.0281
-16.250 -1.2346 0.03801 0.03354 -0.0726 1.0000 0.0282
-16.000 -1.2417 0.03438 0.02980 -0.0738 1.0000 0.0285
-15.750 -1.2445 0.03148 0.02682 -0.0744 1.0000 0.0288
-15.500 -1.2426 0.02929 0.02456 -0.0744 1.0000 0.0291
-15.250 -1.2370 0.02763 0.02284 -0.0739 1.0000 0.0295
-15.000 -1.2292 0.02631 0.02147 -0.0731 1.0000 0.0298
-14.750 -1.2204 0.02519 0.02030 -0.0719 1.0000 0.0302
-14.500 -1.2116 0.02422 0.01926 -0.0704 1.0000 0.0305
-14.250 -1.2037 0.02337 0.01836 -0.0684 1.0000 0.0309
-14.000 -1.1991 0.02265 0.01759 -0.0654 1.0000 0.0311
-13.750 -1.2011 0.02212 0.01701 -0.0607 1.0000 0.0314
-13.500 -1.1982 0.02163 0.01647 -0.0567 1.0000 0.0317
-13.250 -1.1923 0.02119 0.01597 -0.0532 1.0000 0.0320
-13.000 -1.1848 0.02079 0.01551 -0.0499 1.0000 0.0322
-12.750 -1.1788 0.02026 0.01493 -0.0464 1.0000 0.0325
-12.500 -1.1683 0.01935 0.01398 -0.0441 0.9995 0.0331
-12.250 -1.1404 0.01859 0.01319 -0.0449 0.9980 0.0337
-12.000 -1.1106 0.01801 0.01259 -0.0459 0.9965 0.0343
-11.750 -1.0797 0.01751 0.01205 -0.0471 0.9951 0.0350
-11.500 -1.0481 0.01701 0.01152 -0.0483 0.9940 0.0357
-11.250 -1.0157 0.01654 0.01101 -0.0497 0.9931 0.0363
-11.000 -0.9868 0.01612 0.01054 -0.0502 0.9907 0.0367
-10.750 -0.9579 0.01548 0.00986 -0.0510 0.9883 0.0376
-10.500 -0.9271 0.01491 0.00928 -0.0520 0.9864 0.0386
-10.250 -0.8943 0.01446 0.00882 -0.0534 0.9850 0.0396
-10.000 -0.8604 0.01405 0.00839 -0.0549 0.9838 0.0405
-9.750 -0.8255 0.01368 0.00799 -0.0566 0.9829 0.0415
-9.500 -0.7910 0.01321 0.00749 -0.0582 0.9819 0.0427
-9.250 -0.7641 0.01277 0.00706 -0.0582 0.9775 0.0443
-9.000 -0.7334 0.01242 0.00670 -0.0589 0.9741 0.0460
-8.750 -0.7017 0.01212 0.00638 -0.0597 0.9713 0.0475
-8.500 -0.6740 0.01168 0.00595 -0.0598 0.9674 0.0503
-8.250 -0.6486 0.01139 0.00566 -0.0593 0.9614 0.0529
-8.000 -0.6218 0.01104 0.00532 -0.0591 0.9566 0.0566
-7.750 -0.5961 0.01078 0.00506 -0.0586 0.9506 0.0604
-7.500 -0.5710 0.01046 0.00476 -0.0580 0.9439 0.0659
-7.250 -0.5446 0.01018 0.00450 -0.0576 0.9381 0.0719
-7.000 -0.5189 0.00995 0.00428 -0.0571 0.9302 0.0782
-6.750 -0.4924 0.00970 0.00404 -0.0567 0.9233 0.0854
-6.500 -0.4663 0.00946 0.00384 -0.0563 0.9148 0.0927
-6.250 -0.4393 0.00928 0.00364 -0.0560 0.9068 0.0992
-6.000 -0.4125 0.00907 0.00346 -0.0557 0.8976 0.1069
-5.750 -0.3855 0.00889 0.00327 -0.0554 0.8885 0.1145
-5.500 -0.3582 0.00873 0.00311 -0.0552 0.8783 0.1219
-5.250 -0.3312 0.00855 0.00294 -0.0549 0.8681 0.1318
-5.000 -0.3040 0.00839 0.00279 -0.0547 0.8570 0.1415
-4.500 -0.2494 0.00811 0.00251 -0.0542 0.8344 0.1634
-4.250 -0.2221 0.00797 0.00239 -0.0540 0.8221 0.1766
-4.000 -0.1948 0.00783 0.00227 -0.0538 0.8102 0.1920
-3.750 -0.1676 0.00770 0.00217 -0.0536 0.7982 0.2113
-3.500 -0.1401 0.00758 0.00208 -0.0534 0.7858 0.2313
-3.250 -0.1125 0.00747 0.00200 -0.0533 0.7738 0.2486
-3.000 -0.0850 0.00739 0.00192 -0.0531 0.7618 0.2653
-2.750 -0.0572 0.00730 0.00186 -0.0530 0.7495 0.2822
-2.500 -0.0295 0.00722 0.00179 -0.0529 0.7371 0.2994
-2.250 -0.0019 0.00715 0.00174 -0.0527 0.7240 0.3170
-2.000 0.0256 0.00709 0.00169 -0.0526 0.7101 0.3361
-1.750 0.0534 0.00702 0.00164 -0.0524 0.6970 0.3571
-1.500 0.0809 0.00694 0.00160 -0.0523 0.6841 0.3815
-1.250 0.1081 0.00687 0.00157 -0.0521 0.6708 0.4098
-1.000 0.1354 0.00678 0.00155 -0.0519 0.6570 0.4415
-0.750 0.1625 0.00668 0.00154 -0.0517 0.6430 0.4790
-0.500 0.1895 0.00662 0.00154 -0.0514 0.6276 0.5168
-0.250 0.2164 0.00657 0.00155 -0.0512 0.6121 0.5539
0.000 0.2434 0.00655 0.00156 -0.0509 0.5974 0.5869
0.250 0.2705 0.00654 0.00159 -0.0507 0.5831 0.6176
0.500 0.2978 0.00652 0.00162 -0.0504 0.5689 0.6453
0.750 0.3250 0.00652 0.00165 -0.0502 0.5548 0.6734
1.000 0.3519 0.00652 0.00169 -0.0499 0.5418 0.7019
1.250 0.3788 0.00652 0.00174 -0.0496 0.5300 0.7344
1.500 0.4056 0.00648 0.00180 -0.0492 0.5194 0.7700
1.750 0.4319 0.00650 0.00188 -0.0487 0.5082 0.8026
2.000 0.4585 0.00651 0.00196 -0.0483 0.4967 0.8329
2.250 0.4851 0.00656 0.00204 -0.0478 0.4859 0.8590
3.250 0.5895 0.00694 0.00241 -0.0456 0.4338 0.9369
3.750 0.6460 0.00721 0.00263 -0.0454 0.4097 0.9633
4.000 0.6771 0.00738 0.00275 -0.0460 0.3980 0.9724
4.250 0.7077 0.00757 0.00288 -0.0466 0.3850 0.9814
4.500 0.7456 0.00776 0.00302 -0.0488 0.3713 0.9858
4.750 0.7842 0.00799 0.00318 -0.0511 0.3547 0.9905
5.000 0.8220 0.00828 0.00336 -0.0534 0.3335 0.9941
5.250 0.8596 0.00854 0.00352 -0.0556 0.3132 0.9964
5.500 0.8954 0.00878 0.00369 -0.0575 0.2954 0.9987
5.750 0.9252 0.00905 0.00386 -0.0581 0.2755 1.0000
6.000 0.9434 0.00931 0.00403 -0.0562 0.2556 1.0000
6.250 0.9614 0.00960 0.00422 -0.0544 0.2368 1.0000
6.500 0.9802 0.00988 0.00442 -0.0526 0.2217 1.0000
6.750 0.9998 0.01015 0.00462 -0.0511 0.2088 1.0000
7.000 1.0197 0.01042 0.00484 -0.0495 0.1968 1.0000
7.250 1.0395 0.01072 0.00508 -0.0480 0.1841 1.0000
7.500 1.0596 0.01104 0.00533 -0.0466 0.1702 1.0000
7.750 1.0799 0.01139 0.00560 -0.0452 0.1550 1.0000
8.000 1.1001 0.01178 0.00590 -0.0439 0.1397 1.0000
8.250 1.1203 0.01218 0.00622 -0.0426 0.1264 1.0000
8.500 1.1405 0.01259 0.00657 -0.0413 0.1152 1.0000
8.750 1.1611 0.01298 0.00690 -0.0402 0.1062 1.0000
9.000 1.1819 0.01335 0.00725 -0.0390 0.0980 1.0000
9.250 1.2017 0.01378 0.00763 -0.0377 0.0899 1.0000
9.500 1.2204 0.01424 0.00804 -0.0363 0.0816 1.0000
9.750 1.2382 0.01469 0.00845 -0.0346 0.0742 1.0000
10.000 1.2547 0.01515 0.00888 -0.0328 0.0677 1.0000
10.250 1.2706 0.01565 0.00935 -0.0309 0.0620 1.0000
10.500 1.2856 0.01623 0.00990 -0.0290 0.0571 1.0000
10.750 1.3028 0.01671 0.01039 -0.0274 0.0542 1.0000
11.000 1.3177 0.01732 0.01100 -0.0256 0.0512 1.0000
11.250 1.3337 0.01790 0.01159 -0.0240 0.0491 1.0000
11.500 1.3498 0.01847 0.01220 -0.0225 0.0474 1.0000
11.750 1.3642 0.01917 0.01290 -0.0209 0.0458 1.0000
12.000 1.3760 0.02003 0.01378 -0.0190 0.0440 1.0000
12.250 1.3919 0.02067 0.01446 -0.0177 0.0432 1.0000
12.500 1.4065 0.02140 0.01524 -0.0164 0.0424 1.0000
12.750 1.4200 0.02223 0.01611 -0.0150 0.0415 1.0000
13.000 1.4320 0.02318 0.01709 -0.0135 0.0406 1.0000
13.250 1.4418 0.02432 0.01826 -0.0120 0.0396 1.0000
13.500 1.4481 0.02575 0.01974 -0.0103 0.0386 1.0000
13.750 1.4608 0.02678 0.02083 -0.0093 0.0382 1.0000
14.000 1.4722 0.02794 0.02205 -0.0083 0.0377 1.0000
14.250 1.4825 0.02921 0.02337 -0.0073 0.0371 1.0000
14.500 1.4918 0.03061 0.02484 -0.0064 0.0365 1.0000
14.750 1.4997 0.03218 0.02646 -0.0056 0.0360 1.0000
15.000 1.5059 0.03395 0.02828 -0.0048 0.0354 1.0000
15.250 1.5096 0.03600 0.03039 -0.0040 0.0349 1.0000
15.500 1.5093 0.03852 0.03297 -0.0034 0.0343 1.0000
15.750 1.5065 0.04140 0.03593 -0.0029 0.0338 1.0000
16.000 1.5127 0.04344 0.03805 -0.0027 0.0335 1.0000
16.250 1.5174 0.04569 0.04038 -0.0026 0.0332 1.0000
16.500 1.5207 0.04817 0.04293 -0.0026 0.0328 1.0000
16.750 1.5227 0.05083 0.04568 -0.0027 0.0324 1.0000
17.000 1.5231 0.05372 0.04864 -0.0029 0.0320 1.0000
17.250 1.5225 0.05680 0.05180 -0.0033 0.0317 1.0000
17.500 1.5207 0.06009 0.05517 -0.0038 0.0313 1.0000
17.750 1.5175 0.06360 0.05875 -0.0044 0.0310 1.0000
18.000 1.5122 0.06742 0.06264 -0.0052 0.0306 1.0000
18.250 1.5044 0.07163 0.06692 -0.0061 0.0303 1.0000
18.500 1.4934 0.07633 0.07170 -0.0073 0.0299 1.0000
18.750 1.4790 0.08150 0.07697 -0.0087 0.0296 1.0000
19.000 1.4732 0.08562 0.08118 -0.0098 0.0293 1.0000
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