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GOE 7K AIRFOIL (goe07k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 7K AIRFOIL (goe07k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 142.85 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe07k-il-1000000-n5.txt
Download as CSV file: xf-goe07k-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 7K 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
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.1193   0.08321   0.08130  -0.1314   0.9467   0.0042
 -10.000  -0.1297   0.07476   0.07286  -0.1362   0.9428   0.0039
  -9.750  -0.3358   0.02302   0.01989  -0.1624   0.9108   0.0037
  -9.500  -0.3282   0.02002   0.01648  -0.1606   0.9064   0.0038
  -9.250  -0.3102   0.01792   0.01403  -0.1602   0.9035   0.0040
  -9.000  -0.2877   0.01665   0.01253  -0.1603   0.9011   0.0041
  -8.750  -0.2801   0.01582   0.01155  -0.1566   0.8971   0.0042
  -8.500  -0.2626   0.01502   0.01059  -0.1550   0.8939   0.0043
  -8.250  -0.2401   0.01429   0.00971  -0.1545   0.8913   0.0044
  -8.000  -0.2124   0.01375   0.00906  -0.1551   0.8891   0.0048
  -7.750  -0.1849   0.01290   0.00802  -0.1557   0.8872   0.0049
  -7.500  -0.1744   0.01247   0.00748  -0.1522   0.8839   0.0050
  -7.250  -0.1585   0.01197   0.00687  -0.1498   0.8808   0.0053
  -7.000  -0.1377   0.01147   0.00624  -0.1486   0.8782   0.0054
  -6.750  -0.1140   0.01095   0.00562  -0.1481   0.8759   0.0058
  -6.500  -0.0866   0.01051   0.00509  -0.1484   0.8738   0.0061
  -6.250  -0.0639   0.01023   0.00475  -0.1476   0.8715   0.0064
  -6.000  -0.0506   0.00994   0.00441  -0.1445   0.8680   0.0068
  -5.750  -0.0306   0.00972   0.00413  -0.1430   0.8651   0.0074
  -5.500  -0.0082   0.00939   0.00374  -0.1420   0.8626   0.0078
  -5.250   0.0174   0.00913   0.00343  -0.1418   0.8603   0.0087
  -5.000   0.0460   0.00890   0.00314  -0.1422   0.8584   0.0096
  -4.750   0.0602   0.00869   0.00290  -0.1393   0.8553   0.0105
  -4.500   0.0782   0.00850   0.00270  -0.1373   0.8521   0.0117
  -4.250   0.1001   0.00833   0.00249  -0.1361   0.8491   0.0129
  -4.000   0.1241   0.00813   0.00227  -0.1355   0.8465   0.0155
  -3.750   0.1512   0.00797   0.00208  -0.1356   0.8441   0.0197
  -3.500   0.1675   0.00783   0.00196  -0.1331   0.8407   0.0238
  -3.250   0.1872   0.00772   0.00189  -0.1314   0.8374   0.0323
  -3.000   0.2097   0.00764   0.00180  -0.1304   0.8343   0.0379
  -2.750   0.2349   0.00757   0.00173  -0.1300   0.8317   0.0435
  -2.500   0.2613   0.00754   0.00166  -0.1299   0.8292   0.0465
  -2.250   0.2801   0.00752   0.00164  -0.1280   0.8258   0.0477
  -2.000   0.3004   0.00743   0.00153  -0.1265   0.8222   0.0509
  -1.750   0.3232   0.00735   0.00144  -0.1255   0.8189   0.0533
  -1.500   0.3485   0.00729   0.00136  -0.1251   0.8160   0.0552
  -1.250   0.3694   0.00725   0.00131  -0.1237   0.8125   0.0565
  -1.000   0.3903   0.00722   0.00127  -0.1223   0.8087   0.0575
  -0.750   0.4132   0.00719   0.00122  -0.1213   0.8053   0.0581
  -0.500   0.4377   0.00717   0.00118  -0.1208   0.8022   0.0594
  -0.250   0.4612   0.00715   0.00115  -0.1200   0.7992   0.0608
   0.000   0.4819   0.00712   0.00116  -0.1185   0.7955   0.0679
   0.250   0.5006   0.00698   0.00118  -0.1166   0.7909   0.1328
   0.500   0.5201   0.00675   0.00121  -0.1151   0.7863   0.2447
   0.750   0.5323   0.00645   0.00130  -0.1118   0.7799   0.3937
   1.000   0.5485   0.00622   0.00135  -0.1095   0.7737   0.5128
   1.250   0.5631   0.00591   0.00144  -0.1068   0.7688   0.6577
   1.750   0.7917   0.00591   0.00227  -0.1484   0.7538   0.9907
   2.000   0.8253   0.00604   0.00237  -0.1500   0.7453   0.9942
   2.250   0.8565   0.00615   0.00244  -0.1511   0.7328   0.9966
   2.500   0.8917   0.00625   0.00251  -0.1532   0.7213   0.9991
   2.750   0.9128   0.00639   0.00260  -0.1519   0.7056   1.0000
   3.000   0.9250   0.00652   0.00271  -0.1485   0.6933   1.0000
   3.250   0.9356   0.00667   0.00282  -0.1448   0.6775   1.0000
   3.500   0.9399   0.00694   0.00299  -0.1397   0.6499   1.0000
   3.750   0.9368   0.00736   0.00324  -0.1329   0.6062   1.0000
   4.000   0.9199   0.00821   0.00372  -0.1233   0.5311   1.0000
   4.250   0.9131   0.00902   0.00422  -0.1161   0.4656   1.0000
   4.500   0.9058   0.00997   0.00478  -0.1091   0.3845   1.0000
   4.750   0.9013   0.01097   0.00538  -0.1028   0.2967   1.0000
   5.000   0.9003   0.01192   0.00598  -0.0974   0.2210   1.0000
   5.250   0.9112   0.01248   0.00638  -0.0944   0.1853   1.0000
   5.500   0.9196   0.01319   0.00686  -0.0909   0.1338   1.0000
   5.750   0.9253   0.01405   0.00745  -0.0871   0.0763   1.0000
   6.000   0.9416   0.01446   0.00782  -0.0852   0.0641   1.0000
   6.250   0.9572   0.01490   0.00822  -0.0832   0.0500   1.0000
   6.500   0.9698   0.01551   0.00870  -0.0807   0.0263   1.0000
   6.750   0.9854   0.01599   0.00915  -0.0788   0.0180   1.0000
   7.000   1.0016   0.01645   0.00960  -0.0770   0.0139   1.0000
   7.250   1.0180   0.01689   0.01005  -0.0752   0.0114   1.0000
   7.500   1.0343   0.01736   0.01053  -0.0735   0.0095   1.0000
   7.750   1.0505   0.01784   0.01103  -0.0717   0.0085   1.0000
   8.000   1.0669   0.01832   0.01154  -0.0701   0.0077   1.0000
   8.250   1.0829   0.01882   0.01208  -0.0684   0.0069   1.0000
   8.500   1.0975   0.01942   0.01270  -0.0665   0.0061   1.0000
   8.750   1.1138   0.01993   0.01326  -0.0649   0.0057   1.0000
   9.000   1.1292   0.02049   0.01386  -0.0631   0.0052   1.0000
   9.250   1.1439   0.02111   0.01452  -0.0613   0.0049   1.0000
   9.500   1.1575   0.02179   0.01523  -0.0594   0.0045   1.0000
   9.750   1.1728   0.02239   0.01588  -0.0578   0.0041   1.0000
  10.000   1.1859   0.02315   0.01670  -0.0558   0.0040   1.0000
  10.250   1.1999   0.02383   0.01745  -0.0541   0.0037   1.0000
  10.500   1.2134   0.02457   0.01824  -0.0523   0.0036   1.0000
  10.750   1.2254   0.02542   0.01914  -0.0503   0.0034   1.0000
  11.000   1.2378   0.02624   0.02001  -0.0485   0.0032   1.0000
  11.250   1.2462   0.02740   0.02124  -0.0460   0.0031   1.0000
  11.500   1.2587   0.02824   0.02217  -0.0443   0.0030   1.0000
  11.750   1.2702   0.02916   0.02316  -0.0425   0.0029   1.0000
  12.000   1.2814   0.03012   0.02421  -0.0406   0.0028   1.0000
  12.250   1.2907   0.03123   0.02542  -0.0386   0.0027   1.0000
  12.500   1.2987   0.03249   0.02678  -0.0365   0.0027   1.0000
  12.750   1.3096   0.03351   0.02787  -0.0348   0.0025   1.0000
  13.000   1.3182   0.03472   0.02917  -0.0329   0.0025   1.0000
  13.250   1.3277   0.03588   0.03040  -0.0312   0.0024   1.0000
  13.500   1.3382   0.03694   0.03152  -0.0297   0.0022   1.0000
  13.750   1.3444   0.03842   0.03309  -0.0278   0.0022   1.0000
  14.000   1.3494   0.04003   0.03481  -0.0258   0.0021   1.0000
  14.250   1.3490   0.04217   0.03709  -0.0234   0.0021   1.0000
  14.500   1.3531   0.04391   0.03894  -0.0216   0.0020   1.0000
  14.750   1.3530   0.04610   0.04129  -0.0195   0.0020   1.0000
  15.000   1.3562   0.04801   0.04331  -0.0179   0.0020   1.0000
  15.250   1.3586   0.05006   0.04550  -0.0163   0.0019   1.0000
  15.500   1.3546   0.05283   0.04844  -0.0144   0.0019   1.0000
  15.750   1.3509   0.05562   0.05140  -0.0128   0.0019   1.0000
  16.000   1.3474   0.05850   0.05444  -0.0115   0.0019   1.0000
  16.250   1.3471   0.06108   0.05716  -0.0105   0.0018   1.0000
  16.500   1.3329   0.06546   0.06174  -0.0092   0.0018   1.0000
  16.750   1.3250   0.06918   0.06563  -0.0085   0.0018   1.0000
  17.000   1.3122   0.07373   0.07034  -0.0081   0.0018   1.0000
  17.250   1.3029   0.07801   0.07478  -0.0082   0.0017   1.0000
  17.500   1.2991   0.08169   0.07857  -0.0087   0.0017   1.0000
  17.750   1.2719   0.08920   0.08631  -0.0100   0.0017   1.0000
  18.000   1.2575   0.09501   0.09228  -0.0117   0.0017   1.0000
  18.250   1.2542   0.09915   0.09651  -0.0132   0.0016   1.0000
  18.500   1.2275   0.10774   0.10529  -0.0165   0.0017   1.0000
  18.750   1.1896   0.11925   0.11703  -0.0219   0.0017   1.0000
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