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GOE 434 AIRFOIL (goe434-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
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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