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GOE 650 AIRFOIL (goe650-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 650 AIRFOIL (goe650-il)
Reynolds number: 500,000
Max Cl/Cd: 83.53 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe650-il-500000-n5.txt
Download as CSV file: xf-goe650-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7603   0.08785   0.08424  -0.0689   1.0000   0.0262
 -15.750  -0.7716   0.08300   0.07933  -0.0712   1.0000   0.0265
 -15.500  -0.7830   0.07825   0.07451  -0.0734   1.0000   0.0268
 -15.250  -0.7934   0.07388   0.07008  -0.0753   1.0000   0.0269
 -15.000  -0.8065   0.06928   0.06541  -0.0773   1.0000   0.0271
 -14.750  -0.8210   0.06481   0.06087  -0.0791   1.0000   0.0273
 -14.500  -0.8369   0.06058   0.05658  -0.0804   1.0000   0.0274
 -14.250  -0.8549   0.05641   0.05235  -0.0815   1.0000   0.0275
 -14.000  -0.8774   0.05216   0.04803  -0.0822   1.0000   0.0276
 -13.750  -0.8811   0.04711   0.04288  -0.0876   0.9978   0.0278
 -13.500  -0.8794   0.04198   0.03762  -0.0944   0.9936   0.0280
 -13.250  -0.8822   0.03673   0.03224  -0.1011   0.9866   0.0281
 -13.000  -0.8729   0.03096   0.02631  -0.1106   0.9800   0.0284
 -12.750  -0.8540   0.02703   0.02221  -0.1174   0.9742   0.0289
 -12.500  -0.8288   0.02504   0.02012  -0.1208   0.9713   0.0293
 -12.250  -0.8093   0.02372   0.01870  -0.1216   0.9658   0.0298
 -12.000  -0.7851   0.02252   0.01741  -0.1229   0.9618   0.0303
 -11.750  -0.7577   0.02145   0.01625  -0.1244   0.9593   0.0308
 -11.500  -0.7280   0.02048   0.01518  -0.1261   0.9575   0.0313
 -11.250  -0.7077   0.01974   0.01435  -0.1256   0.9510   0.0319
 -11.000  -0.6792   0.01900   0.01351  -0.1266   0.9476   0.0324
 -10.500  -0.6188   0.01725   0.01162  -0.1295   0.9421   0.0336
 -10.250  -0.5954   0.01661   0.01092  -0.1292   0.9356   0.0342
 -10.000  -0.5653   0.01598   0.01022  -0.1302   0.9315   0.0350
  -9.750  -0.5333   0.01539   0.00956  -0.1315   0.9282   0.0358
  -9.500  -0.5068   0.01493   0.00902  -0.1315   0.9226   0.0367
  -9.250  -0.4783   0.01449   0.00851  -0.1318   0.9172   0.0374
  -9.000  -0.4484   0.01392   0.00788  -0.1326   0.9127   0.0387
  -8.750  -0.4213   0.01347   0.00738  -0.1326   0.9070   0.0400
  -8.500  -0.3942   0.01309   0.00694  -0.1326   0.9008   0.0415
  -8.250  -0.3648   0.01270   0.00649  -0.1330   0.8955   0.0435
  -8.000  -0.3389   0.01231   0.00607  -0.1327   0.8890   0.0468
  -7.750  -0.3125   0.01193   0.00568  -0.1325   0.8821   0.0524
  -7.500  -0.2845   0.01154   0.00530  -0.1326   0.8763   0.0634
  -7.250  -0.2594   0.01125   0.00503  -0.1321   0.8689   0.0734
  -7.000  -0.2316   0.01103   0.00478  -0.1320   0.8618   0.0813
  -6.750  -0.2049   0.01083   0.00456  -0.1317   0.8545   0.0875
  -6.500  -0.1779   0.01066   0.00435  -0.1313   0.8468   0.0923
  -6.250  -0.1504   0.01050   0.00416  -0.1311   0.8401   0.0974
  -6.000  -0.1237   0.01038   0.00399  -0.1307   0.8322   0.1014
  -5.750  -0.0963   0.01023   0.00380  -0.1305   0.8254   0.1059
  -5.500  -0.0696   0.01010   0.00366  -0.1301   0.8187   0.1109
  -5.250  -0.0425   0.01000   0.00351  -0.1297   0.8115   0.1156
  -5.000  -0.0156   0.00987   0.00336  -0.1294   0.8046   0.1201
  -4.750   0.0112   0.00977   0.00324  -0.1290   0.7971   0.1246
  -4.500   0.0387   0.00971   0.00310  -0.1287   0.7910   0.1279
  -4.250   0.0655   0.00958   0.00298  -0.1283   0.7854   0.1326
  -4.000   0.0925   0.00949   0.00288  -0.1279   0.7795   0.1384
  -3.750   0.1200   0.00944   0.00278  -0.1276   0.7739   0.1431
  -3.500   0.1469   0.00932   0.00268  -0.1273   0.7687   0.1491
  -3.250   0.1740   0.00925   0.00260  -0.1269   0.7634   0.1549
  -3.000   0.2014   0.00919   0.00251  -0.1266   0.7584   0.1596
  -2.750   0.2285   0.00911   0.00243  -0.1263   0.7532   0.1657
  -2.500   0.2552   0.00905   0.00237  -0.1258   0.7463   0.1722
  -2.250   0.2818   0.00900   0.00229  -0.1253   0.7383   0.1792
  -2.000   0.3082   0.00894   0.00224  -0.1248   0.7304   0.1872
  -1.750   0.3347   0.00889   0.00219  -0.1243   0.7224   0.1956
  -1.500   0.3611   0.00885   0.00215  -0.1238   0.7145   0.2061
  -1.250   0.3870   0.00880   0.00212  -0.1232   0.7048   0.2192
  -1.000   0.4129   0.00876   0.00210  -0.1226   0.6953   0.2336
  -0.750   0.4386   0.00874   0.00208  -0.1219   0.6851   0.2476
  -0.500   0.4648   0.00871   0.00208  -0.1213   0.6757   0.2631
  -0.250   0.4903   0.00870   0.00209  -0.1206   0.6652   0.2793
   0.000   0.5159   0.00870   0.00210  -0.1199   0.6532   0.2939
   0.250   0.5411   0.00871   0.00212  -0.1192   0.6396   0.3081
   0.500   0.5656   0.00874   0.00214  -0.1183   0.6235   0.3219
   0.750   0.5889   0.00882   0.00217  -0.1171   0.6021   0.3344
   1.000   0.6114   0.00894   0.00221  -0.1158   0.5797   0.3460
   1.250   0.6335   0.00908   0.00229  -0.1144   0.5573   0.3578
   1.500   0.6556   0.00925   0.00238  -0.1131   0.5369   0.3695
   1.750   0.6783   0.00940   0.00249  -0.1118   0.5197   0.3806
   2.000   0.7011   0.00955   0.00260  -0.1107   0.5040   0.3914
   2.250   0.7240   0.00971   0.00272  -0.1095   0.4886   0.4032
   2.500   0.7468   0.00985   0.00284  -0.1083   0.4736   0.4144
   2.750   0.7692   0.01001   0.00297  -0.1071   0.4560   0.4247
   3.000   0.7908   0.01020   0.00311  -0.1057   0.4349   0.4376
   3.250   0.8106   0.01043   0.00327  -0.1040   0.4087   0.4531
   3.500   0.8289   0.01071   0.00347  -0.1021   0.3779   0.4707
   3.750   0.8467   0.01102   0.00369  -0.1000   0.3503   0.4872
   4.000   0.8651   0.01130   0.00390  -0.0981   0.3295   0.5025
   4.250   0.8838   0.01152   0.00410  -0.0962   0.3143   0.5190
   4.500   0.9024   0.01173   0.00431  -0.0943   0.3016   0.5378
   4.750   0.9209   0.01194   0.00453  -0.0924   0.2892   0.5612
   5.000   0.9406   0.01210   0.00475  -0.0907   0.2796   0.5876
   5.250   0.9588   0.01230   0.00500  -0.0888   0.2696   0.6221
   5.500   0.9770   0.01240   0.00524  -0.0869   0.2601   0.6771
   6.000   1.0566   0.01265   0.00595  -0.0924   0.2381   1.0000
   6.250   1.0765   0.01292   0.00619  -0.0909   0.2295   1.0000
   6.500   1.0947   0.01327   0.00647  -0.0890   0.2190   1.0000
   6.750   1.1142   0.01356   0.00674  -0.0875   0.2104   1.0000
   7.000   1.1328   0.01391   0.00705  -0.0858   0.2025   1.0000
   7.250   1.1520   0.01423   0.00735  -0.0842   0.1947   1.0000
   7.500   1.1701   0.01461   0.00769  -0.0825   0.1874   1.0000
   7.750   1.1887   0.01497   0.00803  -0.0810   0.1787   1.0000
   8.000   1.2062   0.01539   0.00841  -0.0792   0.1705   1.0000
   8.250   1.2241   0.01580   0.00879  -0.0776   0.1628   1.0000
   8.500   1.2415   0.01624   0.00922  -0.0759   0.1563   1.0000
   8.750   1.2591   0.01668   0.00964  -0.0743   0.1498   1.0000
   9.000   1.2758   0.01717   0.01011  -0.0727   0.1440   1.0000
   9.250   1.2934   0.01762   0.01057  -0.0711   0.1389   1.0000
   9.500   1.3096   0.01816   0.01110  -0.0695   0.1330   1.0000
   9.750   1.3257   0.01871   0.01164  -0.0678   0.1272   1.0000
  10.000   1.3417   0.01928   0.01221  -0.0662   0.1219   1.0000
  10.250   1.3567   0.01992   0.01284  -0.0645   0.1172   1.0000
  10.500   1.3731   0.02048   0.01343  -0.0631   0.1136   1.0000
  10.750   1.3882   0.02113   0.01410  -0.0615   0.1094   1.0000
  11.000   1.4022   0.02187   0.01483  -0.0599   0.1054   1.0000
  11.250   1.4173   0.02255   0.01555  -0.0584   0.1008   1.0000
  11.500   1.4301   0.02340   0.01638  -0.0568   0.0953   1.0000
  11.750   1.4438   0.02420   0.01721  -0.0553   0.0913   1.0000
  12.000   1.4568   0.02507   0.01809  -0.0538   0.0861   1.0000
  12.250   1.4683   0.02605   0.01908  -0.0522   0.0809   1.0000
  12.500   1.4786   0.02716   0.02017  -0.0506   0.0736   1.0000
  12.750   1.4866   0.02845   0.02142  -0.0489   0.0629   1.0000
  13.250   1.4889   0.03221   0.02503  -0.0449   0.0382   1.0000
  13.500   1.4939   0.03388   0.02673  -0.0433   0.0350   1.0000
  13.750   1.4995   0.03554   0.02844  -0.0419   0.0333   1.0000
  14.000   1.5063   0.03715   0.03012  -0.0407   0.0321   1.0000
  14.250   1.5126   0.03884   0.03188  -0.0395   0.0311   1.0000
  14.500   1.5174   0.04070   0.03380  -0.0384   0.0302   1.0000
  14.750   1.5211   0.04272   0.03590  -0.0374   0.0294   1.0000
  15.000   1.5222   0.04508   0.03832  -0.0365   0.0284   1.0000
  15.250   1.5256   0.04726   0.04059  -0.0357   0.0279   1.0000
  15.500   1.5288   0.04950   0.04292  -0.0351   0.0274   1.0000
  15.750   1.5308   0.05196   0.04547  -0.0345   0.0268   1.0000
  16.000   1.5311   0.05466   0.04827  -0.0341   0.0263   1.0000
  16.250   1.5299   0.05764   0.05134  -0.0339   0.0258   1.0000
  16.500   1.5272   0.06087   0.05465  -0.0339   0.0253   1.0000
  16.750   1.5224   0.06447   0.05835  -0.0340   0.0249   1.0000
  17.000   1.5155   0.06848   0.06247  -0.0345   0.0245   1.0000
  17.250   1.5061   0.07293   0.06702  -0.0352   0.0241   1.0000
  17.500   1.5022   0.07669   0.07090  -0.0358   0.0238   1.0000
  17.750   1.4959   0.08087   0.07519  -0.0366   0.0235   1.0000
  18.000   1.4886   0.08527   0.07971  -0.0377   0.0232   1.0000
  18.250   1.4792   0.09008   0.08464  -0.0390   0.0229   1.0000
  18.500   1.4684   0.09515   0.08983  -0.0405   0.0227   1.0000
  18.750   1.4571   0.10041   0.09521  -0.0422   0.0224   1.0000
  19.000   1.4445   0.10601   0.10092  -0.0443   0.0221   1.0000
  19.250   1.4321   0.11168   0.10671  -0.0464   0.0219   1.0000
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