GOE 434 AIRFOIL (goe434-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 434 AIRFOIL (goe434-il) Reynolds number: 500,000 Max Cl/Cd: 94.49 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe434-il-500000.txt Download as CSV file: xf-goe434-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 434 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.7803 0.10852 0.10456 -0.0735 1.0000 0.0626
-19.250 -0.8202 0.09881 0.09463 -0.0796 1.0000 0.0633
-19.000 -0.8435 0.09190 0.08755 -0.0840 1.0000 0.0640
-18.750 -0.8618 0.08584 0.08133 -0.0879 1.0000 0.0645
-18.500 -0.8775 0.08026 0.07559 -0.0916 1.0000 0.0650
-18.250 -0.8908 0.07514 0.07032 -0.0951 1.0000 0.0655
-18.000 -0.8765 0.07413 0.06935 -0.0949 1.0000 0.0661
-17.750 -0.8651 0.07253 0.06779 -0.0956 1.0000 0.0667
-17.500 -0.8568 0.07051 0.06577 -0.0967 1.0000 0.0672
-17.250 -0.8512 0.06813 0.06337 -0.0980 1.0000 0.0677
-17.000 -0.8488 0.06538 0.06058 -0.0996 1.0000 0.0683
-16.750 -0.8463 0.06272 0.05787 -0.1011 1.0000 0.0688
-16.500 -0.8457 0.05995 0.05505 -0.1026 1.0000 0.0694
-16.250 -0.8460 0.05730 0.05233 -0.1038 1.0000 0.0700
-16.000 -0.8481 0.05488 0.04985 -0.1045 1.0000 0.0705
-15.750 -0.8555 0.05259 0.04750 -0.1043 1.0000 0.0709
-15.500 -0.8476 0.04956 0.04435 -0.1079 0.9968 0.0714
-15.250 -0.8170 0.04885 0.04371 -0.1091 0.9936 0.0724
-15.000 -0.7926 0.04732 0.04221 -0.1117 0.9885 0.0731
-14.750 -0.7727 0.04543 0.04031 -0.1145 0.9805 0.0739
-14.500 -0.7560 0.04346 0.03832 -0.1169 0.9706 0.0747
-14.250 -0.7443 0.04156 0.03635 -0.1184 0.9572 0.0755
-14.000 -0.7390 0.03970 0.03440 -0.1187 0.9400 0.0762
-13.750 -0.7338 0.03796 0.03256 -0.1187 0.9199 0.0768
-13.500 -0.7280 0.03620 0.03067 -0.1189 0.8950 0.0774
-13.250 -0.7216 0.03447 0.02876 -0.1192 0.8661 0.0778
-13.000 -0.7076 0.03386 0.02807 -0.1176 0.8394 0.0788
-12.750 -0.6945 0.03284 0.02697 -0.1173 0.8153 0.0795
-12.500 -0.6812 0.03163 0.02567 -0.1176 0.7945 0.0803
-12.250 -0.6675 0.03036 0.02430 -0.1182 0.7767 0.0811
-12.000 -0.6536 0.02902 0.02285 -0.1191 0.7607 0.0820
-11.750 -0.6387 0.02767 0.02139 -0.1201 0.7468 0.0829
-11.500 -0.6230 0.02635 0.01995 -0.1212 0.7352 0.0838
-11.250 -0.6081 0.02510 0.01860 -0.1223 0.7252 0.0845
-11.000 -0.5908 0.02394 0.01736 -0.1233 0.7161 0.0855
-10.750 -0.5715 0.02266 0.01607 -0.1250 0.7091 0.0866
-10.500 -0.5485 0.02142 0.01480 -0.1272 0.7023 0.0877
-10.250 -0.5238 0.02043 0.01373 -0.1291 0.6960 0.0889
-10.000 -0.4988 0.01973 0.01293 -0.1302 0.6898 0.0902
-9.750 -0.4726 0.01912 0.01226 -0.1311 0.6854 0.0914
-9.500 -0.4462 0.01854 0.01163 -0.1318 0.6809 0.0924
-9.250 -0.4215 0.01773 0.01081 -0.1327 0.6763 0.0940
-9.000 -0.3951 0.01713 0.01019 -0.1334 0.6722 0.0956
-8.750 -0.3678 0.01668 0.00967 -0.1339 0.6681 0.0973
-8.500 -0.3398 0.01632 0.00925 -0.1345 0.6639 0.0990
-8.250 -0.3117 0.01586 0.00878 -0.1350 0.6613 0.1007
-8.000 -0.2838 0.01534 0.00828 -0.1356 0.6582 0.1030
-7.750 -0.2552 0.01495 0.00789 -0.1361 0.6550 0.1057
-7.500 -0.2264 0.01461 0.00753 -0.1366 0.6520 0.1088
-7.250 -0.1975 0.01424 0.00718 -0.1370 0.6490 0.1134
-7.000 -0.1685 0.01394 0.00688 -0.1375 0.6458 0.1199
-6.750 -0.1393 0.01367 0.00664 -0.1379 0.6421 0.1310
-6.500 -0.1096 0.01345 0.00645 -0.1384 0.6389 0.1459
-6.250 -0.0801 0.01318 0.00623 -0.1387 0.6369 0.1591
-6.000 -0.0507 0.01288 0.00598 -0.1391 0.6343 0.1709
-5.750 -0.0211 0.01262 0.00575 -0.1395 0.6315 0.1818
-5.500 0.0086 0.01239 0.00556 -0.1399 0.6286 0.1929
-5.250 0.0383 0.01218 0.00540 -0.1403 0.6258 0.2063
-5.000 0.0682 0.01202 0.00529 -0.1406 0.6230 0.2222
-4.750 0.0983 0.01195 0.00524 -0.1409 0.6202 0.2384
-4.500 0.1288 0.01196 0.00526 -0.1413 0.6170 0.2521
-4.250 0.1593 0.01202 0.00531 -0.1416 0.6142 0.2630
-4.000 0.1894 0.01197 0.00531 -0.1418 0.6123 0.2728
-3.750 0.2197 0.01196 0.00530 -0.1420 0.6100 0.2812
-3.500 0.2499 0.01195 0.00533 -0.1423 0.6076 0.2886
-3.250 0.2802 0.01199 0.00534 -0.1425 0.6051 0.2949
-3.000 0.3105 0.01199 0.00532 -0.1427 0.6025 0.3003
-2.750 0.3406 0.01198 0.00534 -0.1429 0.5998 0.3061
-2.500 0.3708 0.01203 0.00537 -0.1431 0.5970 0.3118
-2.250 0.4013 0.01216 0.00543 -0.1433 0.5940 0.3166
-2.000 0.4318 0.01230 0.00554 -0.1437 0.5902 0.3215
-1.750 0.4612 0.01222 0.00553 -0.1437 0.5880 0.3264
-1.500 0.4908 0.01219 0.00552 -0.1438 0.5850 0.3306
-1.250 0.5204 0.01217 0.00551 -0.1439 0.5813 0.3346
-1.000 0.5502 0.01217 0.00547 -0.1440 0.5775 0.3384
-0.750 0.5801 0.01221 0.00546 -0.1441 0.5742 0.3411
-0.500 0.6098 0.01217 0.00542 -0.1443 0.5709 0.3463
-0.250 0.6400 0.01229 0.00553 -0.1445 0.5668 0.3507
0.000 0.6689 0.01224 0.00554 -0.1445 0.5641 0.3550
0.250 0.6980 0.01224 0.00556 -0.1445 0.5605 0.3596
0.500 0.7273 0.01226 0.00557 -0.1445 0.5567 0.3637
0.750 0.7566 0.01223 0.00552 -0.1446 0.5530 0.3676
1.000 0.7857 0.01219 0.00549 -0.1446 0.5491 0.3730
1.250 0.8151 0.01226 0.00555 -0.1448 0.5447 0.3771
1.500 0.8434 0.01222 0.00556 -0.1446 0.5408 0.3809
1.750 0.8720 0.01222 0.00558 -0.1446 0.5366 0.3850
2.000 0.9006 0.01223 0.00558 -0.1445 0.5324 0.3886
2.250 0.9290 0.01226 0.00556 -0.1444 0.5276 0.3922
2.500 0.9570 0.01224 0.00559 -0.1443 0.5226 0.3987
2.750 0.9848 0.01222 0.00564 -0.1441 0.5170 0.4042
3.000 1.0122 0.01224 0.00566 -0.1439 0.5110 0.4099
3.250 1.0393 0.01235 0.00570 -0.1436 0.5055 0.4151
3.500 1.0670 0.01235 0.00578 -0.1434 0.4999 0.4215
3.750 1.0938 0.01238 0.00585 -0.1431 0.4932 0.4287
4.000 1.1194 0.01248 0.00593 -0.1426 0.4866 0.4356
4.250 1.1461 0.01256 0.00604 -0.1423 0.4792 0.4422
4.500 1.1710 0.01266 0.00615 -0.1417 0.4713 0.4510
4.750 1.1960 0.01279 0.00631 -0.1411 0.4633 0.4607
5.000 1.2193 0.01298 0.00647 -0.1403 0.4537 0.4700
5.250 1.2425 0.01315 0.00668 -0.1394 0.4439 0.4819
5.500 1.2629 0.01342 0.00692 -0.1381 0.4331 0.4936
5.750 1.2837 0.01364 0.00717 -0.1368 0.4230 0.5059
6.000 1.2998 0.01398 0.00749 -0.1348 0.4127 0.5191
6.250 1.3195 0.01430 0.00783 -0.1335 0.4015 0.5326
6.500 1.3371 0.01474 0.00826 -0.1319 0.3898 0.5472
6.750 1.3516 0.01531 0.00880 -0.1299 0.3762 0.5606
7.000 1.3663 0.01591 0.00938 -0.1280 0.3605 0.5749
7.250 1.3772 0.01668 0.01012 -0.1258 0.3420 0.5885
7.500 1.3843 0.01771 0.01106 -0.1231 0.3197 0.6020
7.750 1.3865 0.01905 0.01232 -0.1201 0.2938 0.6151
8.250 1.3875 0.02234 0.01547 -0.1147 0.2565 0.6417
8.500 1.3934 0.02384 0.01697 -0.1128 0.2459 0.6563
8.750 1.3990 0.02542 0.01857 -0.1111 0.2379 0.6728
9.000 1.4070 0.02690 0.02010 -0.1096 0.2316 0.6907
9.250 1.4113 0.02871 0.02194 -0.1081 0.2260 0.7100
9.500 1.4207 0.03015 0.02346 -0.1069 0.2221 0.7327
9.750 1.4310 0.03154 0.02494 -0.1058 0.2187 0.7585
10.000 1.4386 0.03315 0.02664 -0.1046 0.2154 0.7875
10.250 1.4446 0.03483 0.02842 -0.1033 0.2123 0.8244
10.500 1.4441 0.03647 0.03027 -0.1011 0.2093 1.0000
10.750 1.4543 0.03805 0.03186 -0.1003 0.2070 1.0000
11.000 1.4660 0.03952 0.03337 -0.0996 0.2051 1.0000
11.250 1.4769 0.04104 0.03491 -0.0989 0.2029 1.0000
11.500 1.4855 0.04278 0.03667 -0.0982 0.2007 1.0000
11.750 1.4936 0.04457 0.03846 -0.0974 0.1985 1.0000
12.000 1.5004 0.04648 0.04036 -0.0965 0.1961 1.0000
12.250 1.5053 0.04852 0.04237 -0.0956 0.1932 1.0000
12.500 1.5165 0.05005 0.04394 -0.0950 0.1916 1.0000
12.750 1.5283 0.05155 0.04549 -0.0945 0.1900 1.0000
13.000 1.5383 0.05325 0.04723 -0.0940 0.1883 1.0000
13.250 1.5482 0.05495 0.04895 -0.0934 0.1866 1.0000
13.500 1.5580 0.05664 0.05067 -0.0929 0.1847 1.0000
13.750 1.5664 0.05845 0.05248 -0.0923 0.1829 1.0000
14.000 1.5727 0.06049 0.05451 -0.0917 0.1807 1.0000
14.250 1.5800 0.06228 0.05627 -0.0910 0.1781 1.0000
14.500 1.5906 0.06399 0.05805 -0.0907 0.1768 1.0000
14.750 1.6008 0.06574 0.05985 -0.0903 0.1752 1.0000
15.000 1.6090 0.06770 0.06187 -0.0900 0.1734 1.0000
15.250 1.6175 0.06962 0.06382 -0.0897 0.1714 1.0000
15.500 1.6253 0.07157 0.06580 -0.0894 0.1694 1.0000
15.750 1.6311 0.07375 0.06798 -0.0890 0.1673 1.0000
16.000 1.6366 0.07589 0.07010 -0.0886 0.1650 1.0000
16.250 1.6448 0.07786 0.07213 -0.0883 0.1633 1.0000
16.500 1.6530 0.07987 0.07422 -0.0882 0.1614 1.0000
16.750 1.6590 0.08216 0.07656 -0.0881 0.1593 1.0000
17.000 1.6644 0.08447 0.07891 -0.0880 0.1569 1.0000
17.250 1.6687 0.08689 0.08134 -0.0879 0.1545 1.0000
17.500 1.6706 0.08956 0.08399 -0.0878 0.1518 1.0000
17.750 1.6767 0.09188 0.08641 -0.0878 0.1495 1.0000
18.000 1.6818 0.09431 0.08890 -0.0879 0.1465 1.0000
18.250 1.6822 0.09730 0.09191 -0.0881 0.1434 1.0000
18.500 1.6817 0.10034 0.09494 -0.0882 0.1401 1.0000
18.750 1.6852 0.10300 0.09770 -0.0885 0.1365 1.0000
19.000 1.6841 0.10620 0.10092 -0.0889 0.1324 1.0000
19.250 1.6818 0.10958 0.10432 -0.0893 0.1282 1.0000
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