GOE 434 AIRFOIL (goe434-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 434 AIRFOIL (goe434-il) Reynolds number: 1,000,000 Max Cl/Cd: 110.65 at α=4.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe434-il-1000000.txt Download as CSV file: xf-goe434-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.9089 0.09013 0.08641 -0.0801 1.0000 0.0563
-19.000 -0.9051 0.08734 0.08360 -0.0817 1.0000 0.0567
-18.750 -0.9011 0.08458 0.08081 -0.0832 1.0000 0.0572
-18.500 -0.8992 0.08151 0.07771 -0.0849 1.0000 0.0577
-18.250 -0.8950 0.07882 0.07499 -0.0864 1.0000 0.0582
-18.000 -0.8904 0.07618 0.07231 -0.0878 1.0000 0.0587
-17.750 -0.8882 0.07322 0.06930 -0.0895 1.0000 0.0591
-17.500 -0.8835 0.07058 0.06662 -0.0909 1.0000 0.0595
-17.250 -0.8785 0.06799 0.06398 -0.0924 1.0000 0.0599
-17.000 -0.8738 0.06572 0.06173 -0.0934 1.0000 0.0606
-16.750 -0.8710 0.06307 0.05907 -0.0948 1.0000 0.0612
-16.500 -0.8651 0.06070 0.05670 -0.0962 0.9987 0.0617
-16.000 -0.8431 0.05531 0.05124 -0.1016 0.9821 0.0628
-15.750 -0.8330 0.05303 0.04892 -0.1034 0.9716 0.0634
-15.500 -0.8284 0.05078 0.04661 -0.1042 0.9587 0.0639
-15.250 -0.8262 0.04845 0.04421 -0.1047 0.9449 0.0643
-15.000 -0.8214 0.04641 0.04210 -0.1052 0.9302 0.0648
-14.750 -0.8183 0.04416 0.03974 -0.1058 0.9114 0.0651
-14.500 -0.8141 0.04217 0.03761 -0.1062 0.8836 0.0654
-14.250 -0.8157 0.03975 0.03504 -0.1068 0.8497 0.0661
-14.000 -0.8143 0.03735 0.03249 -0.1080 0.8203 0.0667
-13.750 -0.8099 0.03504 0.03006 -0.1093 0.7972 0.0672
-13.500 -0.8022 0.03300 0.02791 -0.1106 0.7779 0.0678
-13.250 -0.7935 0.03098 0.02578 -0.1120 0.7596 0.0683
-13.000 -0.7831 0.02905 0.02374 -0.1135 0.7421 0.0689
-12.750 -0.7704 0.02727 0.02188 -0.1150 0.7272 0.0696
-12.500 -0.7566 0.02560 0.02009 -0.1165 0.7123 0.0702
-12.250 -0.7428 0.02402 0.01843 -0.1180 0.7010 0.0707
-12.000 -0.7221 0.02268 0.01697 -0.1200 0.6892 0.0712
-11.750 -0.7010 0.02084 0.01506 -0.1233 0.6819 0.0719
-11.500 -0.6767 0.01894 0.01307 -0.1276 0.6741 0.0728
-11.250 -0.6505 0.01802 0.01207 -0.1295 0.6660 0.0737
-11.000 -0.6236 0.01741 0.01143 -0.1305 0.6614 0.0745
-10.750 -0.5962 0.01690 0.01089 -0.1314 0.6570 0.0753
-10.500 -0.5686 0.01648 0.01042 -0.1320 0.6523 0.0762
-10.250 -0.5408 0.01613 0.01001 -0.1325 0.6473 0.0770
-10.000 -0.5129 0.01585 0.00965 -0.1329 0.6415 0.0776
-9.750 -0.4852 0.01537 0.00913 -0.1335 0.6383 0.0784
-9.500 -0.4576 0.01477 0.00853 -0.1343 0.6361 0.0797
-9.250 -0.4292 0.01437 0.00812 -0.1348 0.6336 0.0808
-9.000 -0.4003 0.01405 0.00778 -0.1352 0.6308 0.0818
-8.750 -0.3714 0.01377 0.00746 -0.1356 0.6278 0.0828
-8.500 -0.3423 0.01353 0.00718 -0.1359 0.6245 0.0837
-8.250 -0.3132 0.01334 0.00694 -0.1362 0.6210 0.0845
-8.000 -0.2844 0.01304 0.00659 -0.1366 0.6171 0.0859
-7.750 -0.2553 0.01271 0.00625 -0.1370 0.6144 0.0875
-7.500 -0.2257 0.01242 0.00596 -0.1374 0.6130 0.0888
-7.250 -0.1959 0.01217 0.00571 -0.1378 0.6112 0.0902
-7.000 -0.1659 0.01197 0.00549 -0.1381 0.6092 0.0915
-6.750 -0.1361 0.01174 0.00525 -0.1384 0.6069 0.0934
-6.500 -0.1063 0.01147 0.00499 -0.1388 0.6043 0.0960
-6.250 -0.0765 0.01126 0.00477 -0.1391 0.6016 0.0987
-6.000 -0.0469 0.01104 0.00455 -0.1394 0.5989 0.1036
-5.750 -0.0176 0.01072 0.00431 -0.1398 0.5959 0.1197
-5.500 0.0120 0.01047 0.00416 -0.1402 0.5925 0.1438
-5.250 0.0422 0.01033 0.00405 -0.1406 0.5900 0.1553
-5.000 0.0727 0.01018 0.00393 -0.1409 0.5889 0.1633
-4.750 0.1031 0.01002 0.00381 -0.1412 0.5874 0.1710
-4.500 0.1334 0.00986 0.00368 -0.1416 0.5857 0.1800
-4.250 0.1638 0.00970 0.00357 -0.1419 0.5839 0.1901
-4.000 0.1941 0.00952 0.00345 -0.1423 0.5819 0.2049
-3.750 0.2243 0.00934 0.00336 -0.1426 0.5797 0.2286
-3.500 0.2546 0.00925 0.00332 -0.1429 0.5774 0.2452
-3.250 0.2849 0.00919 0.00330 -0.1432 0.5749 0.2582
-3.000 0.3151 0.00919 0.00330 -0.1434 0.5717 0.2673
-2.750 0.3453 0.00926 0.00335 -0.1436 0.5674 0.2752
-2.500 0.3759 0.00922 0.00332 -0.1438 0.5658 0.2804
-2.250 0.4064 0.00915 0.00330 -0.1441 0.5637 0.2867
-2.000 0.4369 0.00912 0.00329 -0.1443 0.5609 0.2919
-1.750 0.4673 0.00912 0.00328 -0.1445 0.5580 0.2962
-1.500 0.4976 0.00911 0.00327 -0.1447 0.5552 0.3008
-1.250 0.5276 0.00910 0.00326 -0.1449 0.5521 0.3062
-1.000 0.5574 0.00915 0.00329 -0.1450 0.5484 0.3102
-0.750 0.5875 0.00921 0.00333 -0.1452 0.5449 0.3137
-0.500 0.6178 0.00920 0.00333 -0.1454 0.5427 0.3164
-0.250 0.6481 0.00920 0.00333 -0.1456 0.5394 0.3184
0.000 0.6782 0.00915 0.00331 -0.1458 0.5357 0.3234
0.250 0.7079 0.00915 0.00332 -0.1459 0.5318 0.3284
0.500 0.7372 0.00920 0.00336 -0.1460 0.5278 0.3327
0.750 0.7667 0.00925 0.00340 -0.1461 0.5239 0.3364
1.000 0.7969 0.00926 0.00342 -0.1463 0.5203 0.3390
1.250 0.8266 0.00929 0.00345 -0.1464 0.5157 0.3410
1.500 0.8557 0.00930 0.00346 -0.1465 0.5104 0.3463
1.750 0.8842 0.00935 0.00350 -0.1464 0.5045 0.3517
2.000 0.9139 0.00936 0.00355 -0.1466 0.4991 0.3564
2.250 0.9426 0.00943 0.00360 -0.1466 0.4923 0.3604
2.500 0.9705 0.00953 0.00367 -0.1464 0.4846 0.3634
2.750 0.9990 0.00962 0.00373 -0.1463 0.4763 0.3656
3.000 1.0261 0.00972 0.00381 -0.1461 0.4678 0.3728
3.250 1.0543 0.00980 0.00391 -0.1461 0.4596 0.3786
3.500 1.0804 0.00997 0.00404 -0.1456 0.4497 0.3836
3.750 1.1075 0.01012 0.00416 -0.1454 0.4396 0.3884
4.000 1.1329 0.01033 0.00432 -0.1449 0.4287 0.3938
4.250 1.1584 0.01051 0.00450 -0.1444 0.4177 0.4031
4.500 1.1839 0.01070 0.00468 -0.1439 0.4080 0.4102
4.750 1.2077 0.01096 0.00489 -0.1432 0.3970 0.4157
5.000 1.2327 0.01116 0.00508 -0.1426 0.3869 0.4247
5.250 1.2549 0.01146 0.00535 -0.1416 0.3749 0.4340
5.500 1.2761 0.01176 0.00561 -0.1405 0.3614 0.4419
5.750 1.2942 0.01209 0.00590 -0.1387 0.3461 0.4531
6.000 1.3095 0.01259 0.00633 -0.1367 0.3260 0.4644
6.250 1.3219 0.01332 0.00693 -0.1343 0.2989 0.4747
6.500 1.3287 0.01430 0.00775 -0.1313 0.2679 0.4873
6.750 1.3372 0.01523 0.00857 -0.1286 0.2460 0.4979
7.000 1.3494 0.01601 0.00932 -0.1265 0.2326 0.5125
7.250 1.3625 0.01679 0.01007 -0.1246 0.2229 0.5248
7.500 1.3787 0.01743 0.01074 -0.1232 0.2171 0.5395
7.750 1.3928 0.01821 0.01152 -0.1217 0.2116 0.5515
8.000 1.4081 0.01896 0.01231 -0.1203 0.2070 0.5654
8.250 1.4250 0.01966 0.01303 -0.1192 0.2039 0.5771
8.500 1.4401 0.02047 0.01389 -0.1180 0.2006 0.5909
9.000 1.4657 0.02254 0.01601 -0.1154 0.1938 0.6168
9.250 1.4806 0.02348 0.01701 -0.1144 0.1919 0.6299
9.500 1.4972 0.02434 0.01794 -0.1136 0.1903 0.6454
9.750 1.5119 0.02535 0.01902 -0.1127 0.1885 0.6615
10.000 1.5255 0.02646 0.02020 -0.1118 0.1865 0.6799
10.250 1.5374 0.02772 0.02153 -0.1108 0.1844 0.7015
10.500 1.5473 0.02916 0.02304 -0.1097 0.1822 0.7259
10.750 1.5559 0.03071 0.02466 -0.1086 0.1797 0.7521
11.000 1.5645 0.03232 0.02637 -0.1076 0.1777 0.7805
11.250 1.5793 0.03338 0.02755 -0.1069 0.1766 0.8152
11.500 1.5878 0.03443 0.02892 -0.1054 0.1754 1.0000
11.750 1.5997 0.03583 0.03034 -0.1047 0.1738 1.0000
12.000 1.6092 0.03747 0.03201 -0.1039 0.1720 1.0000
12.250 1.6182 0.03916 0.03371 -0.1031 0.1702 1.0000
12.500 1.6249 0.04108 0.03564 -0.1022 0.1683 1.0000
12.750 1.6303 0.04311 0.03768 -0.1013 0.1661 1.0000
13.000 1.6352 0.04522 0.03981 -0.1005 0.1642 1.0000
13.250 1.6468 0.04673 0.04137 -0.0999 0.1632 1.0000
13.500 1.6583 0.04821 0.04289 -0.0994 0.1619 1.0000
13.750 1.6677 0.04993 0.04464 -0.0987 0.1602 1.0000
14.000 1.6747 0.05189 0.04661 -0.0981 0.1583 1.0000
14.250 1.6818 0.05381 0.04854 -0.0974 0.1561 1.0000
14.500 1.6860 0.05606 0.05081 -0.0968 0.1540 1.0000
14.750 1.6885 0.05849 0.05326 -0.0961 0.1518 1.0000
15.000 1.7002 0.06000 0.05481 -0.0956 0.1506 1.0000
15.250 1.7095 0.06172 0.05657 -0.0951 0.1488 1.0000
15.500 1.7151 0.06389 0.05877 -0.0947 0.1467 1.0000
15.750 1.7209 0.06601 0.06090 -0.0942 0.1443 1.0000
16.000 1.7243 0.06838 0.06327 -0.0936 0.1416 1.0000
16.250 1.7285 0.07074 0.06567 -0.0932 0.1394 1.0000
16.500 1.7360 0.07269 0.06766 -0.0928 0.1367 1.0000
16.750 1.7407 0.07495 0.06991 -0.0924 0.1331 1.0000
17.000 1.7388 0.07798 0.07296 -0.0920 0.1295 1.0000
17.250 1.7442 0.08020 0.07520 -0.0917 0.1253 1.0000
17.500 1.7418 0.08331 0.07829 -0.0914 0.1201 1.0000
17.750 1.7407 0.08628 0.08127 -0.0912 0.1141 1.0000
18.000 1.7371 0.08954 0.08450 -0.0910 0.1070 1.0000
18.250 1.7283 0.09347 0.08842 -0.0909 0.1004 1.0000
18.500 1.7220 0.09713 0.09206 -0.0909 0.0945 1.0000
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