NACA 6412 (naca6412-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 6412 (naca6412-il) Reynolds number: 1,000,000 Max Cl/Cd: 142.65 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca6412-il-1000000.txt Download as CSV file: xf-naca6412-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 6412
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
------ -------- --------- --------- -------- -------- --------
-12.500 -0.2381 0.12675 0.12497 -0.0613 0.9949 0.0187
-12.250 -0.5884 0.02989 0.02711 -0.1461 0.9731 0.0181
-12.000 -0.5846 0.02502 0.02188 -0.1496 0.9651 0.0184
-11.750 -0.5665 0.02313 0.01984 -0.1503 0.9603 0.0187
-11.500 -0.5449 0.02194 0.01854 -0.1507 0.9563 0.0190
-11.250 -0.5247 0.02101 0.01752 -0.1503 0.9507 0.0193
-11.000 -0.5028 0.02003 0.01643 -0.1501 0.9460 0.0196
-10.750 -0.4796 0.01910 0.01537 -0.1501 0.9419 0.0200
-10.500 -0.4574 0.01829 0.01445 -0.1497 0.9365 0.0204
-10.250 -0.4341 0.01753 0.01356 -0.1493 0.9311 0.0207
-10.000 -0.4093 0.01689 0.01278 -0.1491 0.9259 0.0211
-9.750 -0.3853 0.01631 0.01209 -0.1486 0.9193 0.0213
-9.500 -0.3640 0.01502 0.01061 -0.1481 0.9128 0.0219
-9.250 -0.3398 0.01429 0.00980 -0.1478 0.9070 0.0224
-9.000 -0.3144 0.01381 0.00926 -0.1475 0.9012 0.0228
-8.750 -0.2883 0.01336 0.00872 -0.1473 0.8959 0.0234
-8.500 -0.2621 0.01294 0.00822 -0.1470 0.8905 0.0239
-8.250 -0.2360 0.01252 0.00772 -0.1468 0.8845 0.0244
-8.000 -0.2093 0.01216 0.00725 -0.1465 0.8790 0.0249
-7.750 -0.1831 0.01172 0.00672 -0.1463 0.8732 0.0254
-7.500 -0.1577 0.01115 0.00610 -0.1459 0.8667 0.0264
-7.250 -0.1307 0.01089 0.00577 -0.1457 0.8606 0.0272
-7.000 -0.1038 0.01059 0.00543 -0.1455 0.8541 0.0280
-6.750 -0.0767 0.01034 0.00510 -0.1453 0.8476 0.0288
-6.500 -0.0493 0.01015 0.00483 -0.1451 0.8414 0.0295
-6.250 -0.0233 0.00968 0.00432 -0.1447 0.8341 0.0309
-6.000 0.0038 0.00950 0.00408 -0.1445 0.8270 0.0322
-5.750 0.0312 0.00932 0.00386 -0.1443 0.8195 0.0336
-5.500 0.0580 0.00909 0.00355 -0.1440 0.8119 0.0352
-5.250 0.0851 0.00886 0.00330 -0.1437 0.8042 0.0373
-5.000 0.1122 0.00874 0.00312 -0.1435 0.7959 0.0393
-4.750 0.1392 0.00852 0.00288 -0.1432 0.7877 0.0421
-4.500 0.1663 0.00842 0.00273 -0.1429 0.7791 0.0450
-4.250 0.1934 0.00827 0.00256 -0.1427 0.7709 0.0485
-4.000 0.2204 0.00818 0.00243 -0.1424 0.7621 0.0519
-3.750 0.2476 0.00807 0.00228 -0.1421 0.7533 0.0555
-3.500 0.2742 0.00799 0.00217 -0.1417 0.7437 0.0598
-3.250 0.3014 0.00790 0.00206 -0.1415 0.7339 0.0641
-3.000 0.3281 0.00784 0.00197 -0.1411 0.7240 0.0699
-2.750 0.3548 0.00777 0.00188 -0.1408 0.7135 0.0759
-2.500 0.3817 0.00773 0.00181 -0.1405 0.7035 0.0823
-2.250 0.4079 0.00769 0.00175 -0.1401 0.6925 0.0910
-2.000 0.4346 0.00766 0.00170 -0.1397 0.6810 0.0999
-1.750 0.4611 0.00764 0.00167 -0.1394 0.6701 0.1096
-1.500 0.4871 0.00763 0.00165 -0.1389 0.6590 0.1218
-1.250 0.5136 0.00761 0.00163 -0.1386 0.6476 0.1336
-1.000 0.5399 0.00762 0.00162 -0.1382 0.6362 0.1456
-0.750 0.5658 0.00766 0.00162 -0.1377 0.6247 0.1582
-0.500 0.5922 0.00766 0.00164 -0.1373 0.6135 0.1742
-0.250 0.6183 0.00768 0.00166 -0.1369 0.6028 0.1908
0.000 0.6438 0.00773 0.00169 -0.1364 0.5917 0.2090
0.250 0.6703 0.00775 0.00173 -0.1361 0.5814 0.2297
0.500 0.6960 0.00778 0.00178 -0.1356 0.5717 0.2530
0.750 0.7219 0.00781 0.00183 -0.1352 0.5621 0.2791
1.000 0.7477 0.00783 0.00190 -0.1348 0.5531 0.3112
1.250 0.7732 0.00785 0.00197 -0.1343 0.5442 0.3483
1.500 0.7981 0.00775 0.00205 -0.1338 0.5366 0.4267
1.750 0.8176 0.00727 0.00223 -0.1322 0.5294 0.7060
2.000 0.8914 0.00694 0.00244 -0.1428 0.5209 0.9999
2.250 0.9181 0.00706 0.00251 -0.1425 0.5140 0.9999
2.500 0.9439 0.00723 0.00261 -0.1421 0.5073 0.9999
2.750 0.9712 0.00731 0.00268 -0.1420 0.5019 0.9999
3.000 0.9976 0.00745 0.00278 -0.1417 0.4959 0.9999
3.250 1.0234 0.00761 0.00289 -0.1414 0.4901 0.9999
3.500 1.0507 0.00770 0.00298 -0.1413 0.4856 0.9999
3.750 1.0771 0.00783 0.00309 -0.1410 0.4801 0.9999
4.000 1.1026 0.00802 0.00323 -0.1406 0.4742 0.9999
4.250 1.1297 0.00812 0.00334 -0.1405 0.4704 0.9999
4.500 1.1564 0.00824 0.00346 -0.1403 0.4659 0.9999
4.750 1.1821 0.00840 0.00360 -0.1400 0.4604 0.9999
5.000 1.2078 0.00857 0.00375 -0.1396 0.4548 0.9999
5.250 1.2344 0.00868 0.00387 -0.1395 0.4491 0.9999
5.500 1.2590 0.00889 0.00404 -0.1389 0.4411 0.9999
5.750 1.2853 0.00901 0.00417 -0.1387 0.4336 0.9999
6.000 1.3097 0.00922 0.00434 -0.1382 0.4247 0.9999
6.250 1.3354 0.00937 0.00449 -0.1379 0.4157 0.9999
6.500 1.3592 0.00960 0.00468 -0.1372 0.4071 0.9999
6.750 1.3845 0.00976 0.00486 -0.1369 0.3977 0.9999
7.000 1.4079 0.01002 0.00507 -0.1362 0.3856 0.9999
7.250 1.4306 0.01030 0.00530 -0.1354 0.3738 0.9999
7.500 1.4528 0.01061 0.00557 -0.1345 0.3587 0.9999
7.750 1.4739 0.01096 0.00586 -0.1334 0.3428 0.9999
8.000 1.4931 0.01135 0.00618 -0.1320 0.3246 0.9999
8.250 1.5101 0.01185 0.00658 -0.1302 0.3022 0.9999
8.500 1.5244 0.01249 0.00708 -0.1280 0.2760 0.9999
8.750 1.5375 0.01323 0.00766 -0.1257 0.2485 0.9999
9.000 1.5493 0.01405 0.00833 -0.1232 0.2197 0.9999
9.250 1.5596 0.01496 0.00908 -0.1206 0.1906 0.9999
9.500 1.5686 0.01597 0.00993 -0.1178 0.1626 0.9999
9.750 1.5768 0.01703 0.01085 -0.1151 0.1370 0.9999
10.000 1.5846 0.01815 0.01184 -0.1124 0.1148 0.9999
10.250 1.5927 0.01928 0.01286 -0.1098 0.0962 0.9999
10.500 1.6003 0.02047 0.01396 -0.1073 0.0808 0.9999
10.750 1.6092 0.02162 0.01506 -0.1051 0.0689 0.9999
11.000 1.6180 0.02280 0.01621 -0.1030 0.0601 0.9999
11.500 1.6370 0.02519 0.01858 -0.0993 0.0472 0.9999
11.750 1.6458 0.02647 0.01988 -0.0975 0.0424 0.9999
12.000 1.6538 0.02786 0.02128 -0.0957 0.0386 0.9999
12.250 1.6624 0.02925 0.02269 -0.0941 0.0352 0.9999
12.500 1.6687 0.03086 0.02431 -0.0924 0.0321 0.9999
12.750 1.6767 0.03236 0.02586 -0.0909 0.0297 0.9999
13.000 1.6824 0.03412 0.02764 -0.0894 0.0275 0.9999
13.250 1.6879 0.03595 0.02952 -0.0880 0.0256 0.9999
13.500 1.6937 0.03781 0.03143 -0.0867 0.0241 0.9999
13.750 1.6955 0.04010 0.03375 -0.0853 0.0224 0.9999
14.000 1.7003 0.04218 0.03590 -0.0842 0.0213 0.9999
14.250 1.7043 0.04440 0.03819 -0.0832 0.0202 0.9999
14.500 1.7056 0.04695 0.04079 -0.0822 0.0193 0.9999
14.750 1.7028 0.05000 0.04391 -0.0812 0.0183 0.9999
15.000 1.7063 0.05244 0.04643 -0.0805 0.0178 0.9999
15.250 1.7079 0.05513 0.04920 -0.0799 0.0172 0.9999
15.500 1.7084 0.05801 0.05215 -0.0793 0.0167 0.9999
15.750 1.7073 0.06113 0.05533 -0.0788 0.0162 0.9999
16.000 1.7035 0.06460 0.05887 -0.0784 0.0157 0.9999
16.250 1.6960 0.06861 0.06297 -0.0781 0.0152 0.9999
16.500 1.6929 0.07215 0.06660 -0.0779 0.0149 0.9999
16.750 1.6922 0.07540 0.06994 -0.0778 0.0147 0.9999
17.000 1.6896 0.07891 0.07354 -0.0778 0.0144 0.9999
17.250 1.6858 0.08262 0.07733 -0.0779 0.0142 0.9999
17.500 1.6817 0.08641 0.08122 -0.0781 0.0139 0.9999
17.750 1.6776 0.09024 0.08513 -0.0784 0.0137 0.9999
18.000 1.6730 0.09416 0.08913 -0.0787 0.0134 0.9999
18.250 1.6669 0.09832 0.09337 -0.0792 0.0132 0.9999
18.500 1.6597 0.10266 0.09779 -0.0798 0.0130 0.9999
18.750 1.6514 0.10721 0.10243 -0.0806 0.0128 0.9999
19.000 1.6422 0.11196 0.10727 -0.0815 0.0126 0.9999
19.250 1.6307 0.11712 0.11251 -0.0826 0.0124 0.9999
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