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GOE 500 AIRFOIL (goe500-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 500 AIRFOIL (goe500-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.63 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe500-il-1000000-n5.txt
Download as CSV file: xf-goe500-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 500 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.2921   0.06076   0.05859  -0.1185   0.9378   0.0091
 -10.750  -0.3642   0.04774   0.04536  -0.1277   0.9133   0.0088
 -10.500  -0.4196   0.02502   0.02205  -0.1555   0.8943   0.0086
 -10.250  -0.3986   0.02189   0.01866  -0.1596   0.8901   0.0087
 -10.000  -0.3751   0.02021   0.01679  -0.1614   0.8867   0.0089
  -9.750  -0.3507   0.01889   0.01532  -0.1626   0.8832   0.0091
  -9.500  -0.3256   0.01779   0.01408  -0.1635   0.8797   0.0093
  -9.250  -0.3002   0.01679   0.01293  -0.1642   0.8763   0.0095
  -9.000  -0.2744   0.01583   0.01181  -0.1648   0.8733   0.0097
  -8.750  -0.2481   0.01499   0.01083  -0.1653   0.8699   0.0099
  -8.500  -0.2214   0.01429   0.01002  -0.1656   0.8662   0.0101
  -8.250  -0.1946   0.01364   0.00925  -0.1659   0.8626   0.0102
  -8.000  -0.1676   0.01309   0.00858  -0.1661   0.8593   0.0104
  -7.750  -0.1402   0.01258   0.00799  -0.1664   0.8556   0.0105
  -7.500  -0.1128   0.01211   0.00742  -0.1666   0.8515   0.0106
  -7.250  -0.0856   0.01144   0.00663  -0.1668   0.8475   0.0108
  -7.000  -0.0582   0.01082   0.00589  -0.1670   0.8435   0.0111
  -6.750  -0.0306   0.01036   0.00535  -0.1672   0.8385   0.0114
  -6.500  -0.0029   0.00998   0.00489  -0.1673   0.8330   0.0118
  -6.250   0.0248   0.00967   0.00450  -0.1673   0.8267   0.0121
  -6.000   0.0525   0.00937   0.00413  -0.1673   0.8187   0.0125
  -5.750   0.0803   0.00911   0.00380  -0.1673   0.8107   0.0129
  -5.500   0.1078   0.00890   0.00350  -0.1672   0.8016   0.0135
  -5.250   0.1356   0.00871   0.00323  -0.1671   0.7913   0.0139
  -5.000   0.1631   0.00854   0.00298  -0.1670   0.7800   0.0143
  -4.750   0.1904   0.00836   0.00269  -0.1669   0.7681   0.0149
  -4.500   0.2178   0.00819   0.00244  -0.1667   0.7564   0.0158
  -4.250   0.2454   0.00805   0.00223  -0.1666   0.7463   0.0168
  -4.000   0.2732   0.00793   0.00205  -0.1665   0.7378   0.0182
  -3.750   0.3008   0.00781   0.00188  -0.1664   0.7295   0.0220
  -3.500   0.3285   0.00761   0.00173  -0.1664   0.7214   0.0387
  -3.250   0.3560   0.00752   0.00162  -0.1663   0.7132   0.0480
  -3.000   0.3839   0.00746   0.00153  -0.1663   0.7048   0.0536
  -2.750   0.4115   0.00740   0.00146  -0.1662   0.6970   0.0607
  -2.500   0.4393   0.00733   0.00140  -0.1661   0.6895   0.0713
  -2.250   0.4669   0.00730   0.00138  -0.1660   0.6826   0.0832
  -2.000   0.4948   0.00728   0.00135  -0.1660   0.6753   0.0900
  -1.750   0.5224   0.00729   0.00133  -0.1658   0.6679   0.0968
  -1.500   0.5501   0.00729   0.00131  -0.1657   0.6599   0.1022
  -1.250   0.5776   0.00729   0.00129  -0.1656   0.6519   0.1062
  -1.000   0.6052   0.00730   0.00127  -0.1655   0.6436   0.1093
  -0.750   0.6326   0.00733   0.00126  -0.1653   0.6362   0.1120
  -0.500   0.6602   0.00734   0.00126  -0.1652   0.6281   0.1165
  -0.250   0.6875   0.00735   0.00127  -0.1651   0.6204   0.1225
   0.000   0.7148   0.00738   0.00128  -0.1649   0.6118   0.1272
   0.250   0.7421   0.00740   0.00130  -0.1647   0.6032   0.1366
   0.500   0.7689   0.00739   0.00134  -0.1645   0.5935   0.1672
   0.750   0.7959   0.00735   0.00139  -0.1644   0.5830   0.2188
   1.000   0.8227   0.00739   0.00146  -0.1642   0.5729   0.2437
   1.250   0.8491   0.00747   0.00153  -0.1639   0.5599   0.2636
   1.500   0.8741   0.00763   0.00163  -0.1633   0.5371   0.2814
   1.750   0.8993   0.00778   0.00174  -0.1628   0.5158   0.3019
   2.000   0.9248   0.00792   0.00185  -0.1624   0.4988   0.3194
   2.250   0.9495   0.00811   0.00198  -0.1618   0.4780   0.3402
   2.500   0.9737   0.00832   0.00215  -0.1611   0.4543   0.3663
   2.750   0.9987   0.00847   0.00230  -0.1606   0.4386   0.3986
   3.000   1.0239   0.00860   0.00246  -0.1601   0.4259   0.4366
   3.250   1.0490   0.00873   0.00263  -0.1597   0.4136   0.4787
   3.500   1.0736   0.00890   0.00281  -0.1591   0.3977   0.5137
   3.750   1.0976   0.00910   0.00300  -0.1584   0.3778   0.5501
   4.000   1.1207   0.00932   0.00324  -0.1576   0.3545   0.6065
   4.250   1.1419   0.00966   0.00351  -0.1565   0.3175   0.6635
   4.500   1.1568   0.00995   0.00402  -0.1543   0.2505   0.9971
   4.750   1.1710   0.01089   0.00460  -0.1520   0.1852   1.0000
   5.000   1.1831   0.01197   0.00526  -0.1494   0.1101   1.0000
   5.250   1.1962   0.01294   0.00591  -0.1469   0.0497   1.0000
   5.500   1.2171   0.01333   0.00624  -0.1457   0.0390   1.0000
   5.750   1.2387   0.01365   0.00653  -0.1446   0.0359   1.0000
   6.000   1.2599   0.01395   0.00682  -0.1435   0.0334   1.0000
   6.250   1.2798   0.01426   0.00714  -0.1420   0.0313   1.0000
   6.500   1.2993   0.01457   0.00745  -0.1405   0.0305   1.0000
   6.750   1.3187   0.01487   0.00777  -0.1390   0.0302   1.0000
   7.000   1.3379   0.01518   0.00809  -0.1376   0.0295   1.0000
   7.250   1.3565   0.01552   0.00846  -0.1360   0.0289   1.0000
   7.500   1.3749   0.01588   0.00883  -0.1344   0.0283   1.0000
   7.750   1.3929   0.01626   0.00923  -0.1328   0.0275   1.0000
   8.000   1.4104   0.01667   0.00966  -0.1312   0.0268   1.0000
   8.250   1.4273   0.01713   0.01012  -0.1295   0.0259   1.0000
   8.500   1.4437   0.01762   0.01063  -0.1278   0.0250   1.0000
   8.750   1.4596   0.01815   0.01118  -0.1260   0.0240   1.0000
   9.000   1.4749   0.01873   0.01179  -0.1242   0.0232   1.0000
   9.250   1.4905   0.01929   0.01239  -0.1225   0.0227   1.0000
   9.500   1.5075   0.01978   0.01290  -0.1210   0.0224   1.0000
   9.750   1.5241   0.02029   0.01345  -0.1196   0.0218   1.0000
  10.000   1.5399   0.02087   0.01406  -0.1180   0.0213   1.0000
  10.250   1.5554   0.02148   0.01468  -0.1165   0.0201   1.0000
  10.500   1.5695   0.02218   0.01537  -0.1148   0.0180   1.0000
  10.750   1.5792   0.02320   0.01629  -0.1127   0.0099   1.0000
  11.000   1.5839   0.02462   0.01771  -0.1100   0.0051   1.0000
  11.250   1.5936   0.02572   0.01887  -0.1080   0.0044   1.0000
  11.500   1.6025   0.02691   0.02012  -0.1060   0.0038   1.0000
  11.750   1.6122   0.02807   0.02134  -0.1042   0.0035   1.0000
  12.000   1.6222   0.02925   0.02258  -0.1025   0.0034   1.0000
  12.250   1.6316   0.03049   0.02389  -0.1009   0.0033   1.0000
  12.500   1.6404   0.03183   0.02529  -0.0993   0.0032   1.0000
  12.750   1.6484   0.03327   0.02680  -0.0977   0.0031   1.0000
  13.000   1.6557   0.03482   0.02842  -0.0962   0.0030   1.0000
  13.250   1.6622   0.03648   0.03017  -0.0947   0.0029   1.0000
  13.500   1.6687   0.03821   0.03197  -0.0933   0.0029   1.0000
  13.750   1.6740   0.04013   0.03396  -0.0920   0.0027   1.0000
  14.000   1.6787   0.04216   0.03607  -0.0908   0.0027   1.0000
  14.250   1.6830   0.04429   0.03828  -0.0897   0.0026   1.0000
  14.500   1.6863   0.04661   0.04068  -0.0887   0.0025   1.0000
  14.750   1.6892   0.04905   0.04321  -0.0879   0.0025   1.0000
  15.000   1.6915   0.05163   0.04587  -0.0871   0.0024   1.0000
  15.250   1.6920   0.05450   0.04884  -0.0864   0.0023   1.0000
  15.500   1.6915   0.05759   0.05203  -0.0859   0.0023   1.0000
  15.750   1.6904   0.06085   0.05541  -0.0856   0.0022   1.0000
  16.000   1.6871   0.06452   0.05919  -0.0854   0.0022   1.0000
  16.250   1.6865   0.06788   0.06265  -0.0854   0.0021   1.0000
  16.500   1.6864   0.07126   0.06613  -0.0856   0.0021   1.0000
  16.750   1.6848   0.07495   0.06992  -0.0859   0.0021   1.0000
  17.000   1.6829   0.07877   0.07384  -0.0864   0.0021   1.0000
  17.250   1.6799   0.08283   0.07801  -0.0870   0.0021   1.0000
  17.500   1.6768   0.08699   0.08228  -0.0878   0.0021   1.0000
  17.750   1.6727   0.09140   0.08680  -0.0889   0.0021   1.0000
  18.000   1.6681   0.09600   0.09151  -0.0901   0.0020   1.0000
  18.250   1.6629   0.10074   0.09636  -0.0915   0.0020   1.0000
  18.500   1.6578   0.10553   0.10126  -0.0930   0.0020   1.0000
  18.750   1.6514   0.11063   0.10648  -0.0948   0.0020   1.0000
  19.000   1.6450   0.11579   0.11174  -0.0968   0.0019   1.0000
  19.250   1.6380   0.12111   0.11718  -0.0989   0.0019   1.0000
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