GOE 243 (MVA PR.3) AIRFOIL (goe243-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 243 (MVA PR.3) AIRFOIL (goe243-il) Reynolds number: 1,000,000 Max Cl/Cd: 107.89 at α=2.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe243-il-1000000-n5.txt Download as CSV file: xf-goe243-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 243 (MVA PR.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.3666 0.06122 0.05771 -0.1231 0.8013 0.0226
-13.250 -0.3794 0.05544 0.05178 -0.1282 0.7951 0.0226
-13.000 -0.3840 0.05101 0.04722 -0.1322 0.7880 0.0226
-12.750 -0.3839 0.04734 0.04342 -0.1357 0.7812 0.0227
-12.500 -0.3792 0.04424 0.04022 -0.1388 0.7762 0.0227
-12.250 -0.3727 0.04137 0.03727 -0.1419 0.7705 0.0227
-12.000 -0.3642 0.03880 0.03460 -0.1447 0.7642 0.0228
-11.750 -0.3580 0.03626 0.03195 -0.1473 0.7582 0.0229
-11.500 -0.3467 0.03371 0.02931 -0.1510 0.7530 0.0230
-11.250 -0.3288 0.03156 0.02708 -0.1548 0.7475 0.0231
-11.000 -0.3069 0.02972 0.02516 -0.1585 0.7422 0.0232
-10.750 -0.2821 0.02804 0.02341 -0.1623 0.7372 0.0233
-10.500 -0.2545 0.02655 0.02187 -0.1660 0.7327 0.0234
-10.250 -0.2253 0.02516 0.02042 -0.1696 0.7274 0.0235
-10.000 -0.1947 0.02393 0.01912 -0.1731 0.7222 0.0237
-9.750 -0.1631 0.02277 0.01789 -0.1766 0.7167 0.0238
-9.500 -0.1300 0.02171 0.01678 -0.1800 0.7110 0.0239
-9.250 -0.0966 0.02074 0.01574 -0.1833 0.7026 0.0240
-9.000 -0.0627 0.01986 0.01478 -0.1864 0.6946 0.0242
-8.750 -0.0278 0.01902 0.01388 -0.1896 0.6878 0.0243
-8.500 0.0073 0.01824 0.01303 -0.1926 0.6817 0.0245
-8.250 0.0424 0.01754 0.01226 -0.1954 0.6757 0.0247
-8.000 0.0785 0.01684 0.01152 -0.1984 0.6711 0.0248
-7.750 0.1145 0.01620 0.01082 -0.2011 0.6655 0.0250
-7.500 0.1504 0.01562 0.01017 -0.2038 0.6592 0.0252
-7.250 0.1865 0.01506 0.00955 -0.2064 0.6537 0.0254
-7.000 0.2229 0.01451 0.00896 -0.2090 0.6487 0.0256
-6.750 0.2590 0.01402 0.00840 -0.2114 0.6426 0.0258
-6.500 0.2946 0.01358 0.00789 -0.2137 0.6360 0.0259
-6.250 0.3307 0.01314 0.00740 -0.2160 0.6305 0.0261
-6.000 0.3663 0.01274 0.00695 -0.2181 0.6246 0.0263
-5.750 0.4012 0.01241 0.00655 -0.2201 0.6181 0.0264
-5.500 0.4379 0.01193 0.00601 -0.2225 0.6120 0.0268
-5.250 0.4726 0.01161 0.00565 -0.2243 0.6051 0.0271
-5.000 0.5057 0.01141 0.00538 -0.2256 0.5968 0.0275
-4.750 0.5385 0.01122 0.00515 -0.2267 0.5887 0.0278
-4.500 0.5704 0.01111 0.00496 -0.2276 0.5782 0.0282
-4.250 0.6022 0.01100 0.00480 -0.2285 0.5691 0.0287
-4.000 0.6337 0.01091 0.00465 -0.2293 0.5593 0.0292
-3.750 0.6651 0.01083 0.00451 -0.2300 0.5502 0.0296
-3.500 0.6959 0.01079 0.00440 -0.2306 0.5388 0.0300
-3.250 0.7266 0.01076 0.00429 -0.2312 0.5273 0.0304
-3.000 0.7570 0.01074 0.00419 -0.2318 0.5145 0.0311
-2.750 0.7873 0.01073 0.00412 -0.2323 0.5022 0.0318
-2.500 0.8168 0.01078 0.00410 -0.2326 0.4890 0.0326
-2.250 0.8456 0.01088 0.00409 -0.2328 0.4748 0.0334
-2.000 0.8747 0.01094 0.00409 -0.2331 0.4624 0.0343
-1.750 0.9040 0.01100 0.00409 -0.2333 0.4527 0.0359
-1.500 0.9329 0.01107 0.00412 -0.2335 0.4425 0.0380
-1.250 0.9617 0.01115 0.00415 -0.2337 0.4334 0.0417
-1.000 0.9906 0.01121 0.00419 -0.2339 0.4240 0.0508
-0.750 1.0192 0.01128 0.00425 -0.2341 0.4156 0.0679
-0.500 1.0482 0.01132 0.00430 -0.2344 0.4082 0.0853
-0.250 1.0768 0.01138 0.00436 -0.2346 0.4000 0.1142
0.000 1.1097 0.01107 0.00433 -0.2361 0.3940 0.2600
0.250 1.1377 0.01116 0.00444 -0.2361 0.3881 0.2771
0.500 1.1648 0.01132 0.00458 -0.2360 0.3812 0.2931
0.750 1.1921 0.01145 0.00471 -0.2359 0.3757 0.3044
1.000 1.2193 0.01159 0.00484 -0.2357 0.3698 0.3142
1.250 1.2453 0.01179 0.00500 -0.2353 0.3631 0.3205
1.500 1.2715 0.01196 0.00516 -0.2350 0.3568 0.3305
1.750 1.2977 0.01213 0.00531 -0.2347 0.3507 0.3384
2.000 1.3228 0.01235 0.00549 -0.2342 0.3446 0.3417
2.250 1.3480 0.01255 0.00566 -0.2337 0.3392 0.3469
2.500 1.3734 0.01273 0.00583 -0.2333 0.3341 0.3520
2.750 1.3973 0.01297 0.00605 -0.2326 0.3273 0.3568
3.000 1.4202 0.01324 0.00628 -0.2317 0.3207 0.3608
3.250 1.4432 0.01348 0.00649 -0.2308 0.3139 0.3643
3.500 1.4611 0.01380 0.00678 -0.2290 0.3062 0.3698
3.750 1.4806 0.01408 0.00704 -0.2275 0.3003 0.3752
4.000 1.5008 0.01443 0.00736 -0.2263 0.2925 0.3803
4.250 1.5198 0.01487 0.00775 -0.2248 0.2834 0.3847
4.500 1.5367 0.01541 0.00823 -0.2231 0.2711 0.3899
4.750 1.5545 0.01592 0.00870 -0.2216 0.2597 0.3963
5.000 1.5693 0.01659 0.00930 -0.2197 0.2456 0.4026
5.250 1.5805 0.01748 0.01007 -0.2172 0.2267 0.4080
5.500 1.5810 0.01899 0.01138 -0.2134 0.1925 0.4138
5.750 1.5918 0.01998 0.01230 -0.2111 0.1787 0.4211
6.000 1.6066 0.02075 0.01305 -0.2094 0.1724 0.4279
6.250 1.6210 0.02156 0.01385 -0.2077 0.1668 0.4341
6.500 1.6381 0.02222 0.01454 -0.2065 0.1644 0.4424
6.750 1.6545 0.02294 0.01528 -0.2051 0.1624 0.4503
7.000 1.6706 0.02369 0.01604 -0.2038 0.1605 0.4574
7.250 1.6858 0.02452 0.01691 -0.2024 0.1587 0.4661
7.500 1.7008 0.02537 0.01778 -0.2010 0.1568 0.4747
7.750 1.7153 0.02629 0.01873 -0.1997 0.1550 0.4829
8.000 1.7296 0.02723 0.01970 -0.1983 0.1532 0.4916
8.250 1.7441 0.02816 0.02066 -0.1970 0.1521 0.4984
8.500 1.7591 0.02908 0.02163 -0.1958 0.1516 0.5044
8.750 1.7741 0.03000 0.02260 -0.1946 0.1512 0.5108
9.000 1.7879 0.03105 0.02368 -0.1934 0.1507 0.5163
9.250 1.8017 0.03208 0.02476 -0.1922 0.1502 0.5208
9.500 1.8148 0.03320 0.02593 -0.1909 0.1497 0.5256
9.750 1.8275 0.03438 0.02715 -0.1897 0.1491 0.5310
10.000 1.8402 0.03557 0.02838 -0.1885 0.1486 0.5357
10.250 1.8517 0.03690 0.02976 -0.1873 0.1481 0.5395
10.500 1.8636 0.03820 0.03109 -0.1861 0.1475 0.5422
10.750 1.8741 0.03964 0.03259 -0.1849 0.1470 0.5455
11.000 1.8845 0.04110 0.03410 -0.1837 0.1465 0.5491
11.250 1.8946 0.04261 0.03566 -0.1826 0.1460 0.5529
11.500 1.9036 0.04427 0.03737 -0.1814 0.1455 0.5564
11.750 1.9130 0.04588 0.03902 -0.1802 0.1450 0.5595
12.000 1.9204 0.04773 0.04092 -0.1791 0.1445 0.5620
12.250 1.9286 0.04949 0.04274 -0.1780 0.1440 0.5650
12.500 1.9350 0.05147 0.04478 -0.1768 0.1436 0.5681
12.750 1.9419 0.05340 0.04678 -0.1757 0.1431 0.5712
13.000 1.9473 0.05553 0.04897 -0.1747 0.1426 0.5739
13.250 1.9526 0.05769 0.05118 -0.1736 0.1421 0.5765
13.500 1.9570 0.05996 0.05351 -0.1726 0.1417 0.5789
13.750 1.9604 0.06235 0.05596 -0.1715 0.1412 0.5809
14.000 1.9634 0.06481 0.05849 -0.1706 0.1408 0.5831
14.250 1.9655 0.06740 0.06115 -0.1696 0.1403 0.5853
14.500 1.9672 0.07006 0.06389 -0.1687 0.1398 0.5876
14.750 1.9674 0.07291 0.06681 -0.1678 0.1392 0.5899
15.000 1.9714 0.07530 0.06927 -0.1671 0.1388 0.5925
15.250 1.9751 0.07776 0.07181 -0.1664 0.1386 0.5951
15.500 1.9810 0.07993 0.07405 -0.1658 0.1382 0.5977
15.750 1.9832 0.08260 0.07679 -0.1652 0.1379 0.5999
16.000 1.9879 0.08494 0.07920 -0.1647 0.1374 0.6022
16.250 1.9911 0.08749 0.08182 -0.1642 0.1368 0.6046
16.500 1.9929 0.09022 0.08463 -0.1637 0.1363 0.6066
16.750 1.9957 0.09278 0.08726 -0.1633 0.1359 0.6090
17.000 1.9956 0.09576 0.09032 -0.1629 0.1353 0.6113
17.250 1.9982 0.09836 0.09299 -0.1625 0.1347 0.6138
17.500 1.9978 0.10137 0.09607 -0.1623 0.1340 0.6159
17.750 1.9989 0.10419 0.09895 -0.1621 0.1331 0.6178
18.000 1.9992 0.10713 0.10195 -0.1619 0.1326 0.6194
18.250 1.9984 0.11020 0.10510 -0.1619 0.1320 0.6215
18.500 1.9992 0.11303 0.10799 -0.1619 0.1313 0.6239
18.750 1.9965 0.11639 0.11141 -0.1620 0.1305 0.6263
19.000 1.9962 0.11938 0.11446 -0.1621 0.1295 0.6292
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