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GOE 625 AIRFOIL (goe625-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 625 AIRFOIL (goe625-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.7 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe625-il-1000000-n5.txt
Download as CSV file: xf-goe625-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 625 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.6857   0.10182   0.09912  -0.0824   1.0000   0.0321
 -18.000  -0.7271   0.09164   0.08884  -0.0892   0.9960   0.0325
 -17.750  -1.0630   0.03764   0.03379  -0.1313   0.9635   0.0315
 -17.500  -1.0814   0.03194   0.02785  -0.1361   0.9409   0.0317
 -17.250  -1.0870   0.02897   0.02470  -0.1373   0.9238   0.0320
 -17.000  -1.0861   0.02697   0.02256  -0.1373   0.9108   0.0323
 -16.750  -1.0814   0.02548   0.02095  -0.1366   0.8999   0.0327
 -16.500  -1.0735   0.02429   0.01965  -0.1356   0.8914   0.0331
 -16.250  -1.0637   0.02332   0.01857  -0.1343   0.8828   0.0335
 -16.000  -1.0529   0.02252   0.01767  -0.1326   0.8754   0.0339
 -15.750  -1.0412   0.02178   0.01686  -0.1309   0.8681   0.0344
 -15.500  -1.0260   0.02100   0.01600  -0.1297   0.8618   0.0351
 -15.250  -1.0083   0.02031   0.01525  -0.1288   0.8567   0.0357
 -15.000  -0.9889   0.01969   0.01457  -0.1279   0.8507   0.0364
 -14.750  -0.9687   0.01914   0.01394  -0.1271   0.8435   0.0372
 -14.500  -0.9472   0.01864   0.01337  -0.1264   0.8369   0.0379
 -14.250  -0.9253   0.01812   0.01279  -0.1257   0.8304   0.0387
 -14.000  -0.9031   0.01761   0.01223  -0.1251   0.8245   0.0397
 -13.750  -0.8800   0.01716   0.01172  -0.1245   0.8192   0.0408
 -13.500  -0.8559   0.01674   0.01126  -0.1241   0.8131   0.0420
 -13.250  -0.8317   0.01635   0.01081  -0.1236   0.8063   0.0432
 -13.000  -0.8071   0.01598   0.01040  -0.1232   0.8005   0.0446
 -12.750  -0.7815   0.01563   0.01003  -0.1228   0.7954   0.0459
 -12.500  -0.7557   0.01533   0.00967  -0.1225   0.7892   0.0471
 -12.250  -0.7300   0.01504   0.00934  -0.1222   0.7831   0.0484
 -12.000  -0.7034   0.01476   0.00904  -0.1220   0.7776   0.0498
 -11.750  -0.6767   0.01452   0.00875  -0.1218   0.7703   0.0511
 -11.500  -0.6502   0.01431   0.00846  -0.1215   0.7622   0.0522
 -11.250  -0.6232   0.01407   0.00820  -0.1213   0.7541   0.0533
 -11.000  -0.5961   0.01388   0.00797  -0.1211   0.7460   0.0545
 -10.750  -0.5684   0.01370   0.00775  -0.1210   0.7405   0.0557
 -10.500  -0.5406   0.01351   0.00752  -0.1209   0.7346   0.0568
 -10.250  -0.5130   0.01334   0.00729  -0.1208   0.7282   0.0576
 -10.000  -0.4855   0.01314   0.00705  -0.1207   0.7225   0.0584
  -9.750  -0.4576   0.01295   0.00684  -0.1206   0.7160   0.0593
  -9.500  -0.4299   0.01280   0.00664  -0.1205   0.7083   0.0601
  -9.250  -0.4018   0.01265   0.00645  -0.1204   0.7008   0.0609
  -9.000  -0.3739   0.01252   0.00627  -0.1203   0.6915   0.0618
  -8.750  -0.3459   0.01240   0.00609  -0.1203   0.6827   0.0626
  -8.500  -0.3177   0.01229   0.00592  -0.1202   0.6729   0.0633
  -8.250  -0.2896   0.01219   0.00576  -0.1201   0.6636   0.0638
  -8.000  -0.2624   0.01201   0.00552  -0.1200   0.6522   0.0646
  -7.750  -0.2347   0.01187   0.00534  -0.1199   0.6407   0.0653
  -7.500  -0.2073   0.01178   0.00518  -0.1197   0.6272   0.0660
  -7.250  -0.1799   0.01171   0.00505  -0.1195   0.6115   0.0668
  -7.000  -0.1525   0.01167   0.00492  -0.1193   0.5941   0.0676
  -6.750  -0.1253   0.01166   0.00482  -0.1191   0.5751   0.0685
  -6.500  -0.0982   0.01168   0.00474  -0.1189   0.5553   0.0694
  -6.250  -0.0712   0.01171   0.00466  -0.1187   0.5352   0.0701
  -6.000  -0.0442   0.01174   0.00458  -0.1184   0.5157   0.0705
  -5.750  -0.0180   0.01167   0.00442  -0.1181   0.4982   0.0713
  -5.500   0.0090   0.01161   0.00429  -0.1179   0.4837   0.0720
  -5.250   0.0363   0.01155   0.00419  -0.1177   0.4732   0.0727
  -5.000   0.0637   0.01152   0.00410  -0.1176   0.4638   0.0735
  -4.750   0.0915   0.01147   0.00401  -0.1175   0.4568   0.0742
  -4.500   0.1195   0.01142   0.00393  -0.1175   0.4505   0.0748
  -4.250   0.1472   0.01140   0.00386  -0.1174   0.4443   0.0754
  -4.000   0.1752   0.01136   0.00379  -0.1173   0.4396   0.0761
  -3.750   0.2034   0.01132   0.00373  -0.1173   0.4357   0.0768
  -3.500   0.2315   0.01129   0.00367  -0.1173   0.4318   0.0774
  -3.250   0.2594   0.01128   0.00363  -0.1173   0.4279   0.0779
  -2.750   0.3148   0.01119   0.00351  -0.1171   0.4211   0.0801
  -2.500   0.3430   0.01115   0.00347  -0.1172   0.4189   0.0812
  -2.250   0.3711   0.01112   0.00344  -0.1172   0.4163   0.0824
  -2.000   0.3989   0.01110   0.00341  -0.1171   0.4134   0.0837
  -1.750   0.4266   0.01110   0.00340  -0.1171   0.4106   0.0850
  -1.500   0.4541   0.01111   0.00340  -0.1170   0.4080   0.0866
  -1.250   0.4813   0.01111   0.00340  -0.1169   0.4053   0.0900
  -1.000   0.5085   0.01112   0.00341  -0.1167   0.4029   0.0941
  -0.750   0.5363   0.01107   0.00342  -0.1167   0.4017   0.1037
  -0.500   0.5639   0.01102   0.00345  -0.1167   0.4004   0.1211
  -0.250   0.5915   0.01101   0.00348  -0.1167   0.3989   0.1318
   0.000   0.6190   0.01104   0.00352  -0.1166   0.3972   0.1385
   0.250   0.6461   0.01106   0.00357  -0.1165   0.3949   0.1451
   0.500   0.6729   0.01111   0.00362  -0.1164   0.3922   0.1504
   0.750   0.6993   0.01118   0.00368  -0.1161   0.3893   0.1543
   1.000   0.7251   0.01125   0.00375  -0.1158   0.3864   0.1604
   1.250   0.7512   0.01132   0.00383  -0.1155   0.3841   0.1651
   1.500   0.7782   0.01135   0.00388  -0.1154   0.3826   0.1693
   1.750   0.8048   0.01138   0.00395  -0.1152   0.3809   0.1756
   2.000   0.8310   0.01143   0.00402  -0.1150   0.3786   0.1813
   2.250   0.8567   0.01150   0.00410  -0.1146   0.3762   0.1878
   2.500   0.8815   0.01156   0.00419  -0.1141   0.3737   0.1989
   2.750   0.9044   0.01164   0.00428  -0.1132   0.3711   0.2090
   3.000   0.9257   0.01172   0.00439  -0.1121   0.3684   0.2231
   3.250   0.9479   0.01176   0.00452  -0.1111   0.3662   0.2553
   3.500   0.9729   0.01168   0.00466  -0.1109   0.3649   0.3379
   3.750   0.9984   0.01162   0.00483  -0.1107   0.3633   0.4206
   4.000   1.0241   0.01153   0.00502  -0.1106   0.3616   0.5287
   4.250   1.0495   0.01133   0.00526  -0.1106   0.3597   0.6894
   4.500   1.0714   0.01113   0.00553  -0.1095   0.3577   0.8511
   4.750   1.0919   0.01114   0.00577  -0.1079   0.3557   0.9782
   5.000   1.1185   0.01132   0.00593  -0.1080   0.3533   1.0000
   5.250   1.1410   0.01155   0.00614  -0.1073   0.3508   1.0000
   5.500   1.1644   0.01176   0.00634  -0.1067   0.3487   1.0000
   5.750   1.1887   0.01195   0.00652  -0.1063   0.3465   1.0000
   6.000   1.2124   0.01216   0.00673  -0.1059   0.3431   1.0000
   6.250   1.2353   0.01241   0.00696  -0.1053   0.3394   1.0000
   6.500   1.2564   0.01274   0.00725  -0.1045   0.3346   1.0000
   6.750   1.2789   0.01302   0.00752  -0.1040   0.3311   1.0000
   7.000   1.3020   0.01328   0.00778  -0.1035   0.3272   1.0000
   7.250   1.3240   0.01360   0.00808  -0.1029   0.3228   1.0000
   7.500   1.3442   0.01400   0.00845  -0.1021   0.3180   1.0000
   7.750   1.3661   0.01433   0.00879  -0.1015   0.3140   1.0000
   8.000   1.3869   0.01472   0.00916  -0.1008   0.3080   1.0000
   8.250   1.4050   0.01525   0.00965  -0.0998   0.3007   1.0000
   8.500   1.4239   0.01576   0.01012  -0.0989   0.2921   1.0000
   8.750   1.4397   0.01644   0.01074  -0.0977   0.2824   1.0000
   9.000   1.4542   0.01720   0.01144  -0.0963   0.2714   1.0000
   9.250   1.4700   0.01790   0.01211  -0.0951   0.2629   1.0000
   9.500   1.4843   0.01870   0.01287  -0.0938   0.2550   1.0000
   9.750   1.5007   0.01941   0.01357  -0.0928   0.2491   1.0000
  10.000   1.5151   0.02024   0.01437  -0.0916   0.2429   1.0000
  10.250   1.5303   0.02103   0.01515  -0.0906   0.2381   1.0000
  10.500   1.5460   0.02180   0.01593  -0.0896   0.2338   1.0000
  10.750   1.5604   0.02266   0.01679  -0.0886   0.2295   1.0000
  11.000   1.5731   0.02365   0.01777  -0.0874   0.2253   1.0000
  11.250   1.5889   0.02446   0.01860  -0.0866   0.2222   1.0000
  11.500   1.6020   0.02546   0.01961  -0.0855   0.2181   1.0000
  11.750   1.6127   0.02663   0.02077  -0.0843   0.2132   1.0000
  12.000   1.6235   0.02784   0.02199  -0.0832   0.2087   1.0000
  12.250   1.6366   0.02891   0.02307  -0.0823   0.2050   1.0000
  12.500   1.6472   0.03018   0.02436  -0.0813   0.2014   1.0000
  12.750   1.6568   0.03155   0.02573  -0.0802   0.1979   1.0000
  13.000   1.6664   0.03295   0.02716  -0.0793   0.1948   1.0000
  13.250   1.6789   0.03415   0.02839  -0.0786   0.1922   1.0000
  13.500   1.6889   0.03557   0.02984  -0.0777   0.1894   1.0000
  13.750   1.6977   0.03711   0.03140  -0.0769   0.1864   1.0000
  14.000   1.7030   0.03900   0.03331  -0.0759   0.1831   1.0000
  14.250   1.7108   0.04066   0.03501  -0.0751   0.1802   1.0000
  14.500   1.7175   0.04248   0.03686  -0.0743   0.1765   1.0000
  14.750   1.7204   0.04468   0.03908  -0.0734   0.1719   1.0000
  15.000   1.7213   0.04710   0.04152  -0.0724   0.1679   1.0000
  15.250   1.7250   0.04932   0.04378  -0.0717   0.1643   1.0000
  15.500   1.7236   0.05204   0.04653  -0.0709   0.1591   1.0000
  15.750   1.7184   0.05522   0.04973  -0.0700   0.1538   1.0000
  16.000   1.7108   0.05872   0.05325  -0.0692   0.1465   1.0000
  16.250   1.6991   0.06275   0.05730  -0.0684   0.1397   1.0000
  16.500   1.6791   0.06775   0.06232  -0.0675   0.1303   1.0000
  16.750   1.6423   0.07482   0.06937  -0.0666   0.1137   1.0000
  17.000   1.6071   0.08191   0.07646  -0.0661   0.1004   1.0000
  17.250   1.5808   0.08807   0.08265  -0.0659   0.0918   1.0000
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