GOE 626 AIRFOIL (goe626-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 626 AIRFOIL (goe626-il) Reynolds number: 500,000 Max Cl/Cd: 82.89 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe626-il-500000-n5.txt Download as CSV file: xf-goe626-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 626 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.7151 0.13221 0.12857 -0.0528 1.0000 0.0250
-19.250 -0.7209 0.12766 0.12396 -0.0551 1.0000 0.0252
-19.000 -0.7218 0.12408 0.12035 -0.0568 1.0000 0.0254
-18.750 -0.7236 0.12036 0.11659 -0.0586 1.0000 0.0255
-18.500 -0.7267 0.11643 0.11261 -0.0605 1.0000 0.0257
-18.250 -0.7280 0.11287 0.10901 -0.0621 1.0000 0.0258
-18.000 -0.7297 0.10927 0.10537 -0.0637 1.0000 0.0260
-17.750 -0.7317 0.10570 0.10176 -0.0653 1.0000 0.0261
-17.500 -0.7322 0.10245 0.09846 -0.0666 1.0000 0.0263
-17.250 -0.7337 0.09905 0.09502 -0.0680 1.0000 0.0264
-17.000 -0.7344 0.09587 0.09179 -0.0693 1.0000 0.0265
-16.750 -0.7350 0.09272 0.08860 -0.0705 1.0000 0.0268
-16.500 -0.7356 0.08966 0.08550 -0.0716 1.0000 0.0270
-16.250 -0.7362 0.08667 0.08246 -0.0727 1.0000 0.0272
-16.000 -0.7354 0.08400 0.07975 -0.0734 1.0000 0.0273
-15.750 -0.7349 0.08137 0.07708 -0.0741 1.0000 0.0275
-15.500 -0.7351 0.07867 0.07435 -0.0748 1.0000 0.0277
-15.250 -0.7351 0.07614 0.07178 -0.0752 1.0000 0.0278
-15.000 -0.7346 0.07379 0.06940 -0.0755 1.0000 0.0280
-14.750 -0.7331 0.07174 0.06733 -0.0755 1.0000 0.0280
-14.500 -0.7343 0.06939 0.06495 -0.0755 1.0000 0.0282
-14.250 -0.7367 0.06710 0.06263 -0.0754 1.0000 0.0283
-14.000 -0.7235 0.06457 0.06005 -0.0781 0.9989 0.0284
-13.750 -0.7091 0.06203 0.05747 -0.0811 0.9973 0.0286
-13.500 -0.6949 0.05939 0.05478 -0.0843 0.9950 0.0287
-13.250 -0.6808 0.05677 0.05211 -0.0875 0.9924 0.0289
-13.000 -0.6677 0.05476 0.05012 -0.0895 0.9892 0.0292
-12.750 -0.6542 0.05251 0.04787 -0.0921 0.9857 0.0295
-12.500 -0.6392 0.05012 0.04547 -0.0954 0.9824 0.0297
-12.250 -0.6282 0.04766 0.04298 -0.0984 0.9777 0.0298
-12.000 -0.6198 0.04494 0.04025 -0.1015 0.9716 0.0300
-11.750 -0.6076 0.04191 0.03718 -0.1060 0.9674 0.0303
-11.500 -0.6081 0.03884 0.03406 -0.1088 0.9566 0.0304
-11.250 -0.5962 0.03498 0.03014 -0.1153 0.9490 0.0305
-11.000 -0.5767 0.03074 0.02579 -0.1238 0.9414 0.0308
-10.750 -0.5509 0.02653 0.02145 -0.1324 0.9356 0.0311
-10.500 -0.5284 0.02301 0.01778 -0.1380 0.9274 0.0313
-10.250 -0.4981 0.02071 0.01532 -0.1423 0.9224 0.0317
-10.000 -0.4725 0.01939 0.01390 -0.1440 0.9161 0.0320
-9.750 -0.4455 0.01838 0.01279 -0.1454 0.9088 0.0323
-9.500 -0.4157 0.01749 0.01179 -0.1469 0.9028 0.0327
-9.250 -0.3915 0.01681 0.01104 -0.1470 0.8952 0.0330
-9.000 -0.3648 0.01599 0.01012 -0.1477 0.8884 0.0336
-8.750 -0.3385 0.01530 0.00935 -0.1481 0.8819 0.0343
-8.500 -0.3129 0.01474 0.00872 -0.1481 0.8742 0.0349
-8.250 -0.2847 0.01425 0.00814 -0.1485 0.8663 0.0355
-8.000 -0.2594 0.01384 0.00765 -0.1482 0.8563 0.0361
-7.750 -0.2317 0.01347 0.00718 -0.1482 0.8470 0.0368
-7.500 -0.2056 0.01313 0.00678 -0.1479 0.8376 0.0377
-7.000 -0.1523 0.01240 0.00592 -0.1476 0.8191 0.0413
-6.500 -0.1005 0.01141 0.00498 -0.1473 0.7975 0.0757
-6.250 -0.0739 0.01114 0.00467 -0.1470 0.7853 0.0847
-6.000 -0.0478 0.01083 0.00433 -0.1466 0.7706 0.0958
-5.750 -0.0220 0.01053 0.00400 -0.1462 0.7532 0.1100
-5.500 0.0031 0.01020 0.00367 -0.1457 0.7313 0.1319
-5.250 0.0275 0.00998 0.00340 -0.1449 0.7031 0.1551
-5.000 0.0515 0.00988 0.00323 -0.1441 0.6759 0.1755
-4.750 0.0765 0.00986 0.00316 -0.1433 0.6552 0.1943
-4.500 0.1023 0.00990 0.00313 -0.1427 0.6389 0.2057
-4.250 0.1286 0.00995 0.00311 -0.1421 0.6258 0.2132
-4.000 0.1558 0.00999 0.00309 -0.1417 0.6157 0.2204
-3.750 0.1826 0.01005 0.00307 -0.1413 0.6060 0.2260
-3.500 0.2102 0.01010 0.00311 -0.1409 0.5975 0.2331
-3.250 0.2375 0.01018 0.00310 -0.1405 0.5887 0.2391
-3.000 0.2648 0.01022 0.00312 -0.1402 0.5815 0.2426
-2.750 0.2925 0.01026 0.00314 -0.1399 0.5739 0.2458
-2.500 0.3195 0.01034 0.00315 -0.1394 0.5659 0.2494
-2.250 0.3472 0.01038 0.00315 -0.1391 0.5581 0.2528
-2.000 0.3745 0.01044 0.00315 -0.1387 0.5497 0.2556
-1.750 0.4015 0.01048 0.00319 -0.1383 0.5424 0.2590
-1.500 0.4290 0.01053 0.00322 -0.1379 0.5343 0.2618
-1.250 0.4555 0.01061 0.00325 -0.1374 0.5258 0.2643
-1.000 0.4826 0.01067 0.00327 -0.1370 0.5153 0.2671
-0.750 0.5087 0.01075 0.00327 -0.1364 0.5039 0.2689
-0.500 0.5350 0.01082 0.00327 -0.1359 0.4921 0.2703
-0.250 0.5614 0.01088 0.00328 -0.1354 0.4829 0.2713
0.000 0.5875 0.01091 0.00328 -0.1348 0.4735 0.2729
0.250 0.6136 0.01096 0.00331 -0.1343 0.4643 0.2747
0.500 0.6391 0.01106 0.00336 -0.1336 0.4537 0.2764
0.750 0.6650 0.01114 0.00341 -0.1330 0.4435 0.2779
1.250 0.7164 0.01133 0.00353 -0.1318 0.4261 0.2808
1.500 0.7419 0.01144 0.00360 -0.1311 0.4186 0.2823
1.750 0.7677 0.01153 0.00367 -0.1305 0.4127 0.2838
2.000 0.7937 0.01162 0.00375 -0.1300 0.4066 0.2855
2.250 0.8190 0.01174 0.00384 -0.1293 0.4005 0.2870
2.500 0.8444 0.01186 0.00393 -0.1286 0.3953 0.2883
2.750 0.8700 0.01193 0.00401 -0.1280 0.3889 0.2899
3.000 0.8938 0.01208 0.00412 -0.1271 0.3799 0.2917
3.250 0.9189 0.01217 0.00423 -0.1264 0.3723 0.2934
3.500 0.9431 0.01231 0.00436 -0.1256 0.3648 0.2952
3.750 0.9672 0.01245 0.00449 -0.1247 0.3585 0.2970
4.000 0.9915 0.01258 0.00462 -0.1239 0.3506 0.2988
4.250 1.0143 0.01277 0.00477 -0.1228 0.3432 0.3007
4.500 1.0381 0.01290 0.00491 -0.1219 0.3358 0.3026
4.750 1.0597 0.01308 0.00507 -0.1206 0.3274 0.3046
5.000 1.0814 0.01326 0.00522 -0.1193 0.3190 0.3063
5.250 1.1026 0.01343 0.00539 -0.1179 0.3109 0.3087
5.500 1.1238 0.01360 0.00558 -0.1166 0.3042 0.3111
5.750 1.1447 0.01381 0.00579 -0.1152 0.2949 0.3135
6.000 1.1646 0.01407 0.00603 -0.1137 0.2844 0.3160
6.250 1.1835 0.01439 0.00630 -0.1121 0.2721 0.3186
6.500 1.2018 0.01474 0.00660 -0.1103 0.2576 0.3211
6.750 1.2187 0.01516 0.00695 -0.1084 0.2401 0.3235
7.250 1.2453 0.01635 0.00792 -0.1036 0.1931 0.3289
7.500 1.2592 0.01693 0.00844 -0.1014 0.1785 0.3323
7.750 1.2747 0.01742 0.00891 -0.0994 0.1702 0.3364
8.000 1.2906 0.01790 0.00939 -0.0976 0.1641 0.3407
8.500 1.3219 0.01887 0.01041 -0.0939 0.1541 0.3520
8.750 1.3372 0.01938 0.01095 -0.0920 0.1503 0.3592
9.000 1.3540 0.01981 0.01145 -0.0905 0.1472 0.3677
9.250 1.3696 0.02031 0.01201 -0.0888 0.1437 0.3792
9.500 1.3838 0.02090 0.01265 -0.0870 0.1399 0.3948
9.750 1.3968 0.02155 0.01337 -0.0851 0.1358 0.4173
10.000 1.4124 0.02205 0.01401 -0.0835 0.1323 0.4550
10.250 1.4243 0.02275 0.01482 -0.0817 0.1253 0.5097
10.750 1.4506 0.02411 0.01690 -0.0792 0.0998 1.0000
11.000 1.4434 0.02626 0.01885 -0.0759 0.0736 1.0000
11.250 1.4485 0.02769 0.02027 -0.0739 0.0681 1.0000
11.500 1.4543 0.02914 0.02174 -0.0720 0.0645 1.0000
11.750 1.4616 0.03054 0.02317 -0.0705 0.0624 1.0000
12.000 1.4692 0.03196 0.02463 -0.0690 0.0610 1.0000
12.250 1.4761 0.03351 0.02622 -0.0677 0.0598 1.0000
12.500 1.4816 0.03523 0.02799 -0.0664 0.0587 1.0000
12.750 1.4860 0.03712 0.02993 -0.0652 0.0576 1.0000
13.000 1.4894 0.03919 0.03205 -0.0642 0.0566 1.0000
13.250 1.4934 0.04130 0.03423 -0.0633 0.0557 1.0000
13.500 1.4988 0.04336 0.03636 -0.0627 0.0552 1.0000
13.750 1.5030 0.04560 0.03867 -0.0621 0.0546 1.0000
14.000 1.5064 0.04801 0.04115 -0.0617 0.0539 1.0000
14.250 1.5087 0.05061 0.04382 -0.0614 0.0533 1.0000
14.500 1.5102 0.05335 0.04664 -0.0612 0.0527 1.0000
14.750 1.5103 0.05631 0.04966 -0.0611 0.0521 1.0000
15.000 1.5101 0.05937 0.05279 -0.0611 0.0516 1.0000
15.250 1.5088 0.06262 0.05612 -0.0612 0.0511 1.0000
15.500 1.5069 0.06602 0.05959 -0.0614 0.0506 1.0000
15.750 1.5039 0.06963 0.06328 -0.0618 0.0502 1.0000
16.000 1.4999 0.07345 0.06719 -0.0624 0.0498 1.0000
16.250 1.4953 0.07745 0.07126 -0.0631 0.0493 1.0000
16.500 1.4929 0.08120 0.07510 -0.0638 0.0491 1.0000
16.750 1.4926 0.08470 0.07868 -0.0645 0.0489 1.0000
17.000 1.4925 0.08822 0.08229 -0.0653 0.0486 1.0000
17.250 1.4920 0.09184 0.08600 -0.0662 0.0482 1.0000
17.500 1.4922 0.09537 0.08961 -0.0671 0.0478 1.0000
17.750 1.4908 0.09919 0.09351 -0.0682 0.0475 1.0000
18.000 1.4907 0.10281 0.09721 -0.0693 0.0470 1.0000
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