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GOE 501 AIRFOIL (goe501-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 501 AIRFOIL (goe501-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.87 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe501-il-1000000-n5.txt
Download as CSV file: xf-goe501-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 501 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.5405   0.08512   0.08289  -0.0973   0.9798   0.0206
 -15.000  -0.6136   0.06749   0.06503  -0.1125   0.9753   0.0208
 -14.750  -0.6666   0.05155   0.04885  -0.1317   0.9709   0.0205
 -14.500  -0.7154   0.03706   0.03407  -0.1509   0.9560   0.0206
 -14.250  -0.7574   0.02564   0.02231  -0.1647   0.9376   0.0204
 -14.000  -0.7439   0.02219   0.01864  -0.1696   0.9306   0.0210
 -13.750  -0.7257   0.02076   0.01708  -0.1707   0.9258   0.0215
 -13.500  -0.7060   0.01960   0.01584  -0.1713   0.9203   0.0221
 -13.250  -0.6839   0.01874   0.01489  -0.1717   0.9152   0.0228
 -13.000  -0.6609   0.01798   0.01405  -0.1720   0.9103   0.0235
 -12.750  -0.6373   0.01731   0.01330  -0.1721   0.9041   0.0241
 -12.500  -0.6129   0.01673   0.01261  -0.1722   0.8980   0.0247
 -12.250  -0.5884   0.01612   0.01191  -0.1724   0.8915   0.0253
 -12.000  -0.5635   0.01555   0.01128  -0.1724   0.8842   0.0261
 -11.750  -0.5380   0.01507   0.01073  -0.1725   0.8773   0.0267
 -11.500  -0.5122   0.01464   0.01022  -0.1725   0.8691   0.0274
 -11.250  -0.4862   0.01423   0.00972  -0.1725   0.8614   0.0280
 -11.000  -0.4599   0.01388   0.00927  -0.1725   0.8527   0.0287
 -10.750  -0.4334   0.01354   0.00884  -0.1724   0.8446   0.0291
 -10.500  -0.4074   0.01311   0.00833  -0.1724   0.8360   0.0299
 -10.250  -0.3806   0.01279   0.00794  -0.1724   0.8283   0.0307
 -10.000  -0.3538   0.01250   0.00759  -0.1724   0.8203   0.0314
  -9.750  -0.3268   0.01225   0.00726  -0.1724   0.8122   0.0321
  -9.500  -0.2999   0.01202   0.00693  -0.1722   0.8028   0.0329
  -9.250  -0.2727   0.01179   0.00662  -0.1722   0.7939   0.0335
  -9.000  -0.2457   0.01158   0.00631  -0.1721   0.7851   0.0339
  -8.750  -0.2185   0.01124   0.00592  -0.1721   0.7782   0.0348
  -8.500  -0.1909   0.01101   0.00563  -0.1721   0.7720   0.0356
  -8.000  -0.1353   0.01059   0.00512  -0.1721   0.7620   0.0371
  -7.750  -0.1073   0.01040   0.00487  -0.1721   0.7568   0.0378
  -7.500  -0.0794   0.01023   0.00463  -0.1721   0.7517   0.0385
  -7.250  -0.0513   0.01008   0.00442  -0.1721   0.7475   0.0391
  -7.000  -0.0230   0.00984   0.00415  -0.1722   0.7436   0.0401
  -6.750   0.0052   0.00965   0.00394  -0.1722   0.7396   0.0411
  -6.500   0.0333   0.00951   0.00376  -0.1722   0.7350   0.0420
  -6.250   0.0615   0.00938   0.00359  -0.1722   0.7305   0.0430
  -6.000   0.0900   0.00924   0.00341  -0.1723   0.7267   0.0440
  -5.750   0.1186   0.00912   0.00326  -0.1723   0.7231   0.0448
  -5.500   0.1468   0.00901   0.00310  -0.1723   0.7187   0.0457
  -5.250   0.1749   0.00888   0.00293  -0.1723   0.7140   0.0473
  -5.000   0.2036   0.00875   0.00281  -0.1723   0.7101   0.0487
  -4.750   0.2321   0.00865   0.00269  -0.1724   0.7060   0.0500
  -4.500   0.2605   0.00857   0.00257  -0.1724   0.7016   0.0512
  -4.000   0.3174   0.00839   0.00234  -0.1724   0.6937   0.0537
  -3.750   0.3459   0.00829   0.00224  -0.1724   0.6889   0.0556
  -3.500   0.3737   0.00825   0.00217  -0.1723   0.6816   0.0575
  -3.250   0.4019   0.00819   0.00208  -0.1722   0.6735   0.0592
  -3.000   0.4294   0.00817   0.00201  -0.1720   0.6640   0.0604
  -2.750   0.4575   0.00811   0.00193  -0.1720   0.6543   0.0624
  -2.500   0.4849   0.00808   0.00186  -0.1718   0.6418   0.0651
  -2.250   0.5119   0.00808   0.00180  -0.1715   0.6256   0.0675
  -2.000   0.5373   0.00818   0.00178  -0.1709   0.5978   0.0694
  -1.750   0.5616   0.00836   0.00179  -0.1701   0.5656   0.0715
  -1.500   0.5870   0.00846   0.00180  -0.1696   0.5433   0.0758
  -1.250   0.6129   0.00856   0.00182  -0.1692   0.5272   0.0799
  -1.000   0.6391   0.00862   0.00185  -0.1688   0.5142   0.0881
  -0.750   0.6657   0.00857   0.00188  -0.1686   0.5035   0.1305
  -0.500   0.6925   0.00862   0.00193  -0.1683   0.4947   0.1448
  -0.250   0.7194   0.00867   0.00197  -0.1680   0.4867   0.1524
   0.000   0.7460   0.00874   0.00202  -0.1677   0.4790   0.1598
   0.250   0.7727   0.00881   0.00207  -0.1675   0.4700   0.1656
   0.500   0.7989   0.00889   0.00213  -0.1671   0.4605   0.1756
   0.750   0.8252   0.00895   0.00220  -0.1667   0.4509   0.1896
   1.000   0.8517   0.00899   0.00227  -0.1665   0.4445   0.2120
   1.250   0.8784   0.00900   0.00235  -0.1662   0.4383   0.2462
   1.500   0.9044   0.00906   0.00245  -0.1659   0.4316   0.2733
   1.750   0.9309   0.00911   0.00254  -0.1656   0.4260   0.2943
   2.000   0.9570   0.00919   0.00264  -0.1652   0.4192   0.3088
   2.250   0.9824   0.00931   0.00275  -0.1647   0.4120   0.3246
   2.500   1.0084   0.00939   0.00285  -0.1643   0.4053   0.3383
   2.750   1.0335   0.00952   0.00298  -0.1637   0.3978   0.3530
   3.000   1.0591   0.00961   0.00309  -0.1633   0.3919   0.3667
   3.250   1.0841   0.00973   0.00322  -0.1627   0.3846   0.3774
   3.500   1.1087   0.00987   0.00335  -0.1621   0.3776   0.3889
   3.750   1.1334   0.00999   0.00349  -0.1615   0.3702   0.4035
   4.000   1.1569   0.01016   0.00365  -0.1606   0.3609   0.4182
   4.250   1.1795   0.01036   0.00384  -0.1597   0.3482   0.4348
   4.500   1.2004   0.01061   0.00407  -0.1584   0.3307   0.4632
   4.750   1.2186   0.01091   0.00437  -0.1567   0.3057   0.5168
   5.000   1.2340   0.01128   0.00470  -0.1544   0.2808   0.5663
   5.250   1.2388   0.01215   0.00531  -0.1503   0.2229   0.6020
   5.500   1.2468   0.01292   0.00594  -0.1469   0.1816   0.6418
   5.750   1.2643   0.01312   0.00632  -0.1451   0.1728   0.7376
   6.250   1.3038   0.01336   0.00693  -0.1423   0.1628   1.0000
   6.500   1.3242   0.01364   0.00721  -0.1410   0.1608   1.0000
   6.750   1.3443   0.01393   0.00751  -0.1398   0.1589   1.0000
   7.000   1.3637   0.01427   0.00784  -0.1384   0.1562   1.0000
   7.250   1.3822   0.01465   0.00821  -0.1369   0.1527   1.0000
   7.500   1.4011   0.01501   0.00858  -0.1355   0.1499   1.0000
   7.750   1.4204   0.01536   0.00894  -0.1342   0.1479   1.0000
   8.000   1.4402   0.01568   0.00929  -0.1330   0.1469   1.0000
   8.250   1.4597   0.01602   0.00966  -0.1318   0.1454   1.0000
   8.500   1.4786   0.01640   0.01006  -0.1305   0.1433   1.0000
   8.750   1.4965   0.01683   0.01050  -0.1291   0.1404   1.0000
   9.000   1.5135   0.01732   0.01099  -0.1276   0.1369   1.0000
   9.250   1.5300   0.01785   0.01152  -0.1260   0.1325   1.0000
   9.500   1.5469   0.01836   0.01203  -0.1246   0.1260   1.0000
  10.000   1.5594   0.02068   0.01404  -0.1192   0.0812   1.0000
  10.250   1.5674   0.02179   0.01512  -0.1168   0.0715   1.0000
  10.500   1.5788   0.02272   0.01606  -0.1150   0.0671   1.0000
  10.750   1.5901   0.02369   0.01703  -0.1132   0.0631   1.0000
  11.000   1.6025   0.02460   0.01797  -0.1116   0.0606   1.0000
  11.250   1.6132   0.02566   0.01904  -0.1099   0.0576   1.0000
  11.500   1.6237   0.02676   0.02016  -0.1082   0.0550   1.0000
  11.750   1.6357   0.02779   0.02122  -0.1068   0.0534   1.0000
  12.000   1.6468   0.02890   0.02237  -0.1053   0.0512   1.0000
  12.250   1.6561   0.03018   0.02367  -0.1038   0.0489   1.0000
  12.500   1.6646   0.03157   0.02508  -0.1023   0.0465   1.0000
  12.750   1.6754   0.03280   0.02635  -0.1010   0.0450   1.0000
  13.000   1.6847   0.03420   0.02779  -0.0998   0.0429   1.0000
  13.250   1.6926   0.03576   0.02938  -0.0984   0.0407   1.0000
  13.500   1.7000   0.03739   0.03103  -0.0972   0.0385   1.0000
  13.750   1.7075   0.03906   0.03274  -0.0960   0.0361   1.0000
  14.000   1.7124   0.04101   0.03470  -0.0948   0.0328   1.0000
  14.250   1.7165   0.04311   0.03681  -0.0937   0.0287   1.0000
  14.500   1.7165   0.04567   0.03938  -0.0924   0.0233   1.0000
  14.750   1.7155   0.04844   0.04215  -0.0914   0.0190   1.0000
  15.000   1.7161   0.05113   0.04488  -0.0905   0.0167   1.0000
  15.250   1.7185   0.05369   0.04749  -0.0898   0.0154   1.0000
  15.500   1.7194   0.05649   0.05035  -0.0891   0.0143   1.0000
  15.750   1.7208   0.05931   0.05324  -0.0887   0.0135   1.0000
  16.000   1.7227   0.06215   0.05615  -0.0884   0.0128   1.0000
  16.250   1.7240   0.06515   0.05922  -0.0882   0.0122   1.0000
  16.500   1.7240   0.06839   0.06253  -0.0881   0.0117   1.0000
  16.750   1.7234   0.07176   0.06597  -0.0882   0.0112   1.0000
  17.000   1.7239   0.07506   0.06935  -0.0884   0.0108   1.0000
  17.250   1.7240   0.07848   0.07285  -0.0887   0.0104   1.0000
  17.500   1.7232   0.08208   0.07653  -0.0892   0.0100   1.0000
  17.750   1.7216   0.08584   0.08036  -0.0897   0.0097   1.0000
  18.000   1.7196   0.08968   0.08429  -0.0904   0.0094   1.0000
  18.250   1.7170   0.09367   0.08836  -0.0912   0.0091   1.0000
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