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GOE 650 AIRFOIL (goe650-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 650 AIRFOIL (goe650-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.36 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe650-il-1000000-n5.txt
Download as CSV file: xf-goe650-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 650 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.8270   0.08575   0.08279  -0.0698   1.0000   0.0222
 -16.250  -0.8425   0.08047   0.07745  -0.0723   1.0000   0.0223
 -16.000  -0.8591   0.07519   0.07211  -0.0748   1.0000   0.0225
 -15.750  -0.8795   0.06966   0.06651  -0.0774   1.0000   0.0226
 -15.500  -0.9115   0.06308   0.05985  -0.0804   1.0000   0.0226
 -15.250  -0.9441   0.05645   0.05313  -0.0838   0.9998   0.0226
 -15.000  -0.9703   0.04769   0.04423  -0.0927   0.9978   0.0226
 -14.500  -1.0124   0.02952   0.02566  -0.1155   0.9848   0.0227
 -14.250  -0.9889   0.02487   0.02080  -0.1247   0.9825   0.0230
 -14.000  -0.9733   0.02337   0.01920  -0.1254   0.9769   0.0233
 -13.750  -0.9488   0.02221   0.01795  -0.1270   0.9741   0.0236
 -13.500  -0.9220   0.02121   0.01687  -0.1285   0.9720   0.0239
 -13.250  -0.8940   0.02028   0.01585  -0.1301   0.9704   0.0241
 -13.000  -0.8766   0.01923   0.01473  -0.1297   0.9640   0.0245
 -12.750  -0.8496   0.01830   0.01375  -0.1309   0.9610   0.0250
 -12.250  -0.7874   0.01684   0.01217  -0.1341   0.9570   0.0259
 -12.000  -0.7629   0.01627   0.01155  -0.1340   0.9514   0.0263
 -11.750  -0.7328   0.01571   0.01093  -0.1351   0.9473   0.0267
 -11.500  -0.7005   0.01519   0.01034  -0.1365   0.9438   0.0272
 -11.250  -0.6728   0.01472   0.00980  -0.1369   0.9379   0.0275
 -11.000  -0.6436   0.01428   0.00930  -0.1375   0.9319   0.0278
 -10.750  -0.6135   0.01388   0.00883  -0.1382   0.9266   0.0281
 -10.500  -0.5887   0.01336   0.00824  -0.1380   0.9192   0.0287
 -10.250  -0.5616   0.01291   0.00772  -0.1382   0.9125   0.0292
 -10.000  -0.5360   0.01253   0.00729  -0.1379   0.9057   0.0297
  -9.750  -0.5101   0.01218   0.00689  -0.1376   0.8985   0.0302
  -9.500  -0.4839   0.01188   0.00652  -0.1374   0.8920   0.0308
  -9.250  -0.4585   0.01159   0.00618  -0.1369   0.8848   0.0313
  -9.000  -0.4322   0.01134   0.00586  -0.1366   0.8776   0.0320
  -8.750  -0.4065   0.01110   0.00557  -0.1361   0.8705   0.0324
  -8.500  -0.3809   0.01084   0.00525  -0.1357   0.8624   0.0331
  -8.250  -0.3555   0.01056   0.00493  -0.1351   0.8543   0.0342
  -8.000  -0.3301   0.01033   0.00464  -0.1346   0.8450   0.0353
  -7.750  -0.3043   0.01012   0.00438  -0.1341   0.8366   0.0365
  -7.500  -0.2785   0.00992   0.00413  -0.1336   0.8279   0.0381
  -7.250  -0.2529   0.00969   0.00387  -0.1330   0.8203   0.0409
  -7.000  -0.2274   0.00943   0.00360  -0.1325   0.8123   0.0463
  -6.750  -0.2026   0.00911   0.00331  -0.1319   0.8046   0.0597
  -6.500  -0.1769   0.00889   0.00311  -0.1314   0.7966   0.0711
  -6.250  -0.1509   0.00873   0.00294  -0.1308   0.7891   0.0786
  -6.000  -0.1242   0.00859   0.00280  -0.1305   0.7820   0.0839
  -5.750  -0.0976   0.00849   0.00267  -0.1300   0.7754   0.0885
  -5.500  -0.0707   0.00838   0.00255  -0.1296   0.7696   0.0930
  -5.250  -0.0438   0.00827   0.00243  -0.1293   0.7627   0.0977
  -4.750   0.0100   0.00810   0.00223  -0.1285   0.7507   0.1065
  -4.500   0.0374   0.00802   0.00214  -0.1282   0.7456   0.1111
  -4.250   0.0647   0.00796   0.00206  -0.1279   0.7409   0.1146
  -4.000   0.0918   0.00788   0.00198  -0.1275   0.7367   0.1195
  -3.750   0.1195   0.00780   0.00190  -0.1273   0.7325   0.1238
  -3.500   0.1468   0.00775   0.00184  -0.1269   0.7265   0.1277
  -3.000   0.2006   0.00764   0.00172  -0.1261   0.7125   0.1383
  -2.750   0.2274   0.00762   0.00167  -0.1257   0.7051   0.1425
  -2.500   0.2543   0.00756   0.00162  -0.1252   0.6985   0.1496
  -2.250   0.2813   0.00752   0.00157  -0.1248   0.6906   0.1552
  -2.000   0.3078   0.00752   0.00153  -0.1243   0.6816   0.1592
  -1.750   0.3341   0.00747   0.00150  -0.1238   0.6707   0.1667
  -1.500   0.3605   0.00747   0.00147  -0.1232   0.6594   0.1730
  -1.250   0.3862   0.00746   0.00144  -0.1226   0.6470   0.1809
  -1.000   0.4119   0.00747   0.00142  -0.1219   0.6326   0.1890
  -0.750   0.4369   0.00748   0.00141  -0.1211   0.6143   0.1992
  -0.500   0.4613   0.00754   0.00142  -0.1202   0.5915   0.2111
   0.000   0.5078   0.00775   0.00150  -0.1180   0.5427   0.2392
   0.250   0.5322   0.00783   0.00155  -0.1171   0.5262   0.2541
   0.500   0.5566   0.00791   0.00162  -0.1163   0.5109   0.2696
   0.750   0.5815   0.00798   0.00168  -0.1155   0.4972   0.2825
   1.250   0.6314   0.00814   0.00181  -0.1140   0.4712   0.3095
   1.500   0.6558   0.00824   0.00189  -0.1131   0.4560   0.3214
   1.750   0.6802   0.00836   0.00197  -0.1122   0.4401   0.3312
   2.000   0.7035   0.00851   0.00207  -0.1112   0.4174   0.3432
   2.250   0.7251   0.00874   0.00220  -0.1098   0.3878   0.3541
   2.500   0.7460   0.00901   0.00235  -0.1083   0.3578   0.3640
   2.750   0.7673   0.00926   0.00251  -0.1069   0.3327   0.3741
   3.000   0.7891   0.00949   0.00266  -0.1056   0.3124   0.3845
   3.250   0.8116   0.00966   0.00280  -0.1044   0.2984   0.3948
   3.750   0.8571   0.00998   0.00308  -0.1021   0.2754   0.4154
   4.000   0.8794   0.01013   0.00323  -0.1009   0.2647   0.4327
   4.250   0.9010   0.01028   0.00339  -0.0996   0.2551   0.4500
   4.500   0.9224   0.01041   0.00353  -0.0982   0.2465   0.4644
   5.000   0.9638   0.01070   0.00383  -0.0951   0.2307   0.4928
   5.250   0.9835   0.01089   0.00401  -0.0934   0.2211   0.5081
   5.500   1.0037   0.01107   0.00420  -0.0918   0.2118   0.5264
   5.750   1.0229   0.01127   0.00442  -0.0900   0.2028   0.5484
   6.000   1.0430   0.01144   0.00463  -0.0885   0.1957   0.5724
   6.250   1.0619   0.01163   0.00487  -0.0867   0.1882   0.6055
   6.500   1.0805   0.01178   0.00511  -0.0849   0.1805   0.6530
   6.750   1.0927   0.01174   0.00539  -0.0817   0.1733   0.7896
   7.250   1.1843   0.01229   0.00614  -0.0901   0.1515   1.0000
   7.500   1.2030   0.01263   0.00643  -0.0884   0.1438   1.0000
   7.750   1.2229   0.01291   0.00670  -0.0870   0.1380   1.0000
   8.000   1.2413   0.01327   0.00702  -0.0853   0.1314   1.0000
   8.250   1.2610   0.01358   0.00733  -0.0839   0.1266   1.0000
   8.500   1.2792   0.01397   0.00768  -0.0822   0.1199   1.0000
   8.750   1.2981   0.01433   0.00802  -0.0807   0.1154   1.0000
   9.000   1.3165   0.01472   0.00840  -0.0792   0.1101   1.0000
   9.250   1.3340   0.01517   0.00882  -0.0776   0.1044   1.0000
   9.500   1.3528   0.01554   0.00920  -0.0762   0.1013   1.0000
   9.750   1.3702   0.01602   0.00965  -0.0746   0.0965   1.0000
  10.000   1.3876   0.01649   0.01012  -0.0731   0.0925   1.0000
  10.250   1.4048   0.01698   0.01061  -0.0716   0.0875   1.0000
  10.500   1.4204   0.01757   0.01117  -0.0699   0.0824   1.0000
  10.750   1.4371   0.01811   0.01171  -0.0685   0.0778   1.0000
  11.000   1.4513   0.01881   0.01238  -0.0667   0.0709   1.0000
  11.250   1.4618   0.01975   0.01323  -0.0646   0.0579   1.0000
  11.500   1.4624   0.02135   0.01468  -0.0614   0.0367   1.0000
  11.750   1.4732   0.02234   0.01566  -0.0595   0.0325   1.0000
  12.000   1.4864   0.02319   0.01653  -0.0580   0.0307   1.0000
  12.250   1.4983   0.02414   0.01750  -0.0564   0.0291   1.0000
  12.500   1.5109   0.02505   0.01845  -0.0549   0.0281   1.0000
  12.750   1.5241   0.02595   0.01938  -0.0535   0.0275   1.0000
  13.000   1.5363   0.02693   0.02041  -0.0521   0.0268   1.0000
  13.250   1.5472   0.02801   0.02153  -0.0507   0.0259   1.0000
  13.500   1.5572   0.02920   0.02275  -0.0493   0.0252   1.0000
  13.750   1.5665   0.03045   0.02405  -0.0479   0.0245   1.0000
  14.000   1.5763   0.03171   0.02535  -0.0466   0.0239   1.0000
  14.250   1.5864   0.03296   0.02665  -0.0454   0.0236   1.0000
  14.500   1.5961   0.03427   0.02802  -0.0443   0.0230   1.0000
  14.750   1.6047   0.03569   0.02950  -0.0432   0.0226   1.0000
  15.000   1.6121   0.03727   0.03113  -0.0421   0.0221   1.0000
  15.250   1.6188   0.03894   0.03284  -0.0410   0.0216   1.0000
  15.500   1.6243   0.04075   0.03471  -0.0400   0.0211   1.0000
  15.750   1.6287   0.04273   0.03675  -0.0391   0.0208   1.0000
  16.000   1.6325   0.04481   0.03889  -0.0383   0.0203   1.0000
  16.250   1.6383   0.04673   0.04089  -0.0376   0.0200   1.0000
  16.500   1.6427   0.04883   0.04305  -0.0370   0.0196   1.0000
  16.750   1.6455   0.05115   0.04545  -0.0364   0.0193   1.0000
  17.000   1.6475   0.05363   0.04800  -0.0360   0.0189   1.0000
  17.250   1.6483   0.05631   0.05075  -0.0357   0.0186   1.0000
  17.500   1.6482   0.05915   0.05365  -0.0355   0.0181   1.0000
  17.750   1.6463   0.06226   0.05684  -0.0355   0.0178   1.0000
  18.000   1.6425   0.06569   0.06036  -0.0356   0.0175   1.0000
  18.250   1.6377   0.06934   0.06408  -0.0360   0.0171   1.0000
  18.500   1.6330   0.07305   0.06789  -0.0364   0.0170   1.0000
  18.750   1.6287   0.07673   0.07166  -0.0369   0.0167   1.0000
  19.000   1.6218   0.08080   0.07583  -0.0376   0.0164   1.0000
  19.250   1.6135   0.08515   0.08028  -0.0385   0.0162   1.0000
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