GOE 434 AIRFOIL (goe434-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 434 AIRFOIL (goe434-il) Reynolds number: 1,000,000 Max Cl/Cd: 93.9 at α=3.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe434-il-1000000-n5.txt Download as CSV file: xf-goe434-il-1000000-n5.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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.8750 0.09227 0.08847 -0.0783 1.0000 0.0500
-18.750 -0.8775 0.08864 0.08482 -0.0803 1.0000 0.0505
-18.250 -0.8760 0.08159 0.07769 -0.0852 0.9798 0.0515
-18.000 -0.8727 0.07853 0.07459 -0.0872 0.9694 0.0520
-17.750 -0.8732 0.07531 0.07131 -0.0888 0.9586 0.0525
-17.500 -0.8723 0.07249 0.06843 -0.0899 0.9470 0.0530
-17.250 -0.8705 0.06986 0.06573 -0.0909 0.9350 0.0535
-17.000 -0.8721 0.06687 0.06265 -0.0920 0.9191 0.0539
-16.750 -0.8698 0.06444 0.06010 -0.0926 0.8917 0.0543
-16.500 -0.8681 0.06203 0.05748 -0.0933 0.8518 0.0546
-16.250 -0.8702 0.05892 0.05419 -0.0947 0.8205 0.0550
-16.000 -0.8690 0.05615 0.05130 -0.0962 0.7979 0.0555
-15.750 -0.8706 0.05300 0.04803 -0.0979 0.7798 0.0560
-15.500 -0.8681 0.05037 0.04529 -0.0994 0.7625 0.0564
-15.250 -0.8687 0.04737 0.04221 -0.1011 0.7474 0.0569
-15.000 -0.8667 0.04479 0.03953 -0.1026 0.7333 0.0573
-14.750 -0.8671 0.04191 0.03654 -0.1043 0.7195 0.0578
-14.500 -0.8642 0.03940 0.03394 -0.1058 0.7077 0.0583
-14.250 -0.8620 0.03674 0.03119 -0.1074 0.6960 0.0587
-14.000 -0.8583 0.03418 0.02853 -0.1091 0.6859 0.0591
-13.750 -0.8519 0.03184 0.02611 -0.1107 0.6772 0.0596
-13.500 -0.8445 0.02954 0.02372 -0.1124 0.6683 0.0600
-13.250 -0.8381 0.02697 0.02108 -0.1146 0.6614 0.0606
-13.000 -0.8301 0.02473 0.01878 -0.1166 0.6552 0.0611
-12.750 -0.8139 0.02278 0.01677 -0.1193 0.6485 0.0617
-12.250 -0.7672 0.01969 0.01353 -0.1253 0.6368 0.0631
-12.000 -0.7401 0.01862 0.01240 -0.1278 0.6329 0.0638
-11.750 -0.7133 0.01795 0.01167 -0.1290 0.6289 0.0644
-11.500 -0.6863 0.01742 0.01109 -0.1299 0.6250 0.0650
-11.250 -0.6590 0.01698 0.01059 -0.1306 0.6210 0.0655
-11.000 -0.6321 0.01644 0.01002 -0.1313 0.6169 0.0663
-10.750 -0.6045 0.01600 0.00956 -0.1319 0.6140 0.0672
-10.500 -0.5763 0.01561 0.00915 -0.1324 0.6120 0.0679
-10.250 -0.5479 0.01526 0.00878 -0.1329 0.6097 0.0687
-10.000 -0.5193 0.01494 0.00844 -0.1334 0.6069 0.0694
-9.750 -0.4905 0.01466 0.00813 -0.1337 0.6041 0.0702
-9.500 -0.4616 0.01442 0.00785 -0.1341 0.6014 0.0709
-9.250 -0.4326 0.01418 0.00758 -0.1344 0.5988 0.0715
-9.000 -0.4039 0.01386 0.00724 -0.1348 0.5962 0.0724
-8.750 -0.3750 0.01360 0.00695 -0.1351 0.5933 0.0733
-8.500 -0.3460 0.01336 0.00669 -0.1355 0.5904 0.0742
-8.250 -0.3163 0.01312 0.00645 -0.1358 0.5891 0.0752
-8.000 -0.2866 0.01291 0.00623 -0.1362 0.5876 0.0761
-7.750 -0.2568 0.01272 0.00602 -0.1365 0.5860 0.0769
-7.500 -0.2269 0.01254 0.00583 -0.1368 0.5842 0.0776
-7.250 -0.1971 0.01234 0.00561 -0.1371 0.5821 0.0785
-7.000 -0.1675 0.01211 0.00538 -0.1374 0.5798 0.0797
-6.750 -0.1377 0.01192 0.00518 -0.1377 0.5772 0.0810
-6.500 -0.1080 0.01176 0.00500 -0.1380 0.5743 0.0821
-6.250 -0.0783 0.01163 0.00484 -0.1382 0.5711 0.0832
-6.000 -0.0486 0.01152 0.00469 -0.1384 0.5679 0.0843
-5.750 -0.0185 0.01136 0.00453 -0.1388 0.5663 0.0858
-5.500 0.0118 0.01117 0.00436 -0.1391 0.5651 0.0879
-5.250 0.0420 0.01101 0.00421 -0.1394 0.5635 0.0900
-5.000 0.0723 0.01086 0.00407 -0.1397 0.5616 0.0925
-4.750 0.1025 0.01067 0.00390 -0.1401 0.5594 0.0979
-4.500 0.1322 0.01029 0.00367 -0.1406 0.5574 0.1262
-4.250 0.1622 0.01011 0.00355 -0.1409 0.5554 0.1422
-4.000 0.1924 0.01002 0.00347 -0.1412 0.5531 0.1494
-3.750 0.2225 0.00992 0.00339 -0.1414 0.5505 0.1565
-3.500 0.2525 0.00988 0.00333 -0.1416 0.5477 0.1607
-3.250 0.2825 0.00980 0.00326 -0.1419 0.5451 0.1666
-3.000 0.3131 0.00971 0.00320 -0.1422 0.5435 0.1723
-2.750 0.3436 0.00959 0.00312 -0.1425 0.5410 0.1806
-2.500 0.3739 0.00948 0.00305 -0.1428 0.5379 0.1905
-2.250 0.4040 0.00933 0.00297 -0.1431 0.5342 0.2094
-2.000 0.4337 0.00922 0.00292 -0.1434 0.5296 0.2323
-1.750 0.4633 0.00918 0.00291 -0.1435 0.5252 0.2489
-1.500 0.4937 0.00915 0.00291 -0.1438 0.5227 0.2602
-1.250 0.5241 0.00911 0.00292 -0.1441 0.5193 0.2683
-1.000 0.5542 0.00911 0.00292 -0.1442 0.5152 0.2745
-0.750 0.5841 0.00914 0.00294 -0.1444 0.5111 0.2782
-0.500 0.6134 0.00917 0.00295 -0.1445 0.5061 0.2835
-0.250 0.6434 0.00918 0.00298 -0.1446 0.5011 0.2883
0.000 0.6730 0.00921 0.00300 -0.1448 0.4943 0.2931
0.250 0.7018 0.00929 0.00304 -0.1447 0.4872 0.2966
0.500 0.7315 0.00932 0.00308 -0.1449 0.4820 0.3011
0.750 0.7606 0.00937 0.00313 -0.1449 0.4748 0.3059
1.000 0.7889 0.00947 0.00319 -0.1448 0.4667 0.3097
1.250 0.8176 0.00956 0.00326 -0.1448 0.4578 0.3133
1.500 0.8452 0.00970 0.00335 -0.1446 0.4484 0.3163
1.750 0.8729 0.00984 0.00345 -0.1444 0.4371 0.3189
2.000 0.9001 0.00999 0.00356 -0.1442 0.4266 0.3244
2.250 0.9269 0.01015 0.00370 -0.1439 0.4157 0.3291
2.500 0.9536 0.01033 0.00384 -0.1436 0.4041 0.3330
2.750 0.9793 0.01056 0.00401 -0.1431 0.3915 0.3363
3.000 1.0051 0.01078 0.00417 -0.1427 0.3798 0.3391
3.250 1.0310 0.01098 0.00433 -0.1422 0.3696 0.3412
3.500 1.0553 0.01125 0.00454 -0.1416 0.3563 0.3458
3.750 1.0783 0.01157 0.00479 -0.1407 0.3395 0.3508
4.000 1.0988 0.01199 0.00511 -0.1394 0.3162 0.3563
4.250 1.1140 0.01260 0.00555 -0.1374 0.2855 0.3611
4.500 1.1237 0.01324 0.00603 -0.1343 0.2574 0.3644
4.750 1.1388 0.01381 0.00651 -0.1322 0.2385 0.3686
5.000 1.1569 0.01430 0.00695 -0.1307 0.2260 0.3742
5.250 1.1766 0.01472 0.00735 -0.1295 0.2181 0.3796
5.500 1.1956 0.01518 0.00779 -0.1282 0.2111 0.3847
5.750 1.2152 0.01561 0.00821 -0.1271 0.2061 0.3893
6.000 1.2357 0.01601 0.00862 -0.1261 0.2022 0.3957
6.250 1.2549 0.01646 0.00910 -0.1249 0.1983 0.4037
6.500 1.2729 0.01700 0.00963 -0.1237 0.1941 0.4109
6.750 1.2922 0.01748 0.01013 -0.1226 0.1912 0.4166
7.000 1.3114 0.01798 0.01066 -0.1216 0.1884 0.4253
7.250 1.3297 0.01855 0.01126 -0.1206 0.1853 0.4342
7.500 1.3466 0.01922 0.01194 -0.1194 0.1824 0.4419
7.750 1.3632 0.01992 0.01267 -0.1183 0.1796 0.4517
8.000 1.3803 0.02063 0.01342 -0.1173 0.1775 0.4627
8.250 1.3984 0.02130 0.01413 -0.1164 0.1759 0.4726
8.500 1.4155 0.02206 0.01495 -0.1155 0.1738 0.4867
8.750 1.4318 0.02289 0.01582 -0.1146 0.1718 0.4995
9.000 1.4471 0.02381 0.01680 -0.1137 0.1698 0.5150
9.250 1.4612 0.02486 0.01788 -0.1127 0.1678 0.5269
9.500 1.4749 0.02596 0.01902 -0.1117 0.1657 0.5401
9.750 1.4884 0.02711 0.02021 -0.1108 0.1640 0.5508
10.000 1.5035 0.02813 0.02130 -0.1101 0.1629 0.5625
10.250 1.5171 0.02930 0.02253 -0.1093 0.1615 0.5736
10.500 1.5304 0.03051 0.02378 -0.1085 0.1599 0.5839
10.750 1.5423 0.03186 0.02519 -0.1077 0.1582 0.5963
11.000 1.5537 0.03326 0.02664 -0.1068 0.1564 0.6083
11.250 1.5628 0.03489 0.02832 -0.1060 0.1544 0.6218
11.500 1.5722 0.03649 0.02997 -0.1051 0.1522 0.6348
11.750 1.5826 0.03805 0.03160 -0.1044 0.1508 0.6496
12.000 1.5937 0.03954 0.03317 -0.1037 0.1491 0.6669
12.250 1.6032 0.04119 0.03490 -0.1030 0.1470 0.6867
12.500 1.6116 0.04296 0.03674 -0.1022 0.1450 0.7120
12.750 1.6194 0.04475 0.03861 -0.1015 0.1427 0.7413
13.000 1.6246 0.04685 0.04079 -0.1007 0.1405 0.7685
13.250 1.6346 0.04846 0.04250 -0.1001 0.1389 0.7992
13.500 1.6428 0.05012 0.04438 -0.0993 0.1367 0.8688
13.750 1.6460 0.05200 0.04640 -0.0981 0.1343 1.0000
14.000 1.6519 0.05405 0.04845 -0.0974 0.1315 1.0000
14.250 1.6561 0.05632 0.05074 -0.0968 0.1289 1.0000
14.500 1.6616 0.05847 0.05290 -0.0962 0.1252 1.0000
14.750 1.6649 0.06081 0.05523 -0.0955 0.1208 1.0000
15.000 1.6673 0.06331 0.05775 -0.0949 0.1171 1.0000
15.250 1.6680 0.06597 0.06039 -0.0943 0.1115 1.0000
15.500 1.6678 0.06875 0.06316 -0.0937 0.1047 1.0000
15.750 1.6617 0.07220 0.06658 -0.0931 0.0963 1.0000
16.000 1.6562 0.07558 0.06993 -0.0925 0.0885 1.0000
16.250 1.6525 0.07887 0.07322 -0.0921 0.0844 1.0000
16.500 1.6522 0.08176 0.07612 -0.0917 0.0812 1.0000
16.750 1.6515 0.08479 0.07918 -0.0915 0.0793 1.0000
17.000 1.6538 0.08743 0.08184 -0.0913 0.0780 1.0000
17.250 1.6557 0.09015 0.08460 -0.0911 0.0768 1.0000
17.500 1.6556 0.09314 0.08763 -0.0911 0.0757 1.0000
17.750 1.6575 0.09588 0.09041 -0.0910 0.0747 1.0000
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