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GOE 625 AIRFOIL (goe625-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 625 AIRFOIL (goe625-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.41 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe625-il-1000000.txt
Download as CSV file: xf-goe625-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.8062   0.08434   0.08151  -0.0931   1.0000   0.0373
 -18.000  -0.8871   0.07048   0.06747  -0.1020   1.0000   0.0374
 -17.750  -1.0531   0.04508   0.04164  -0.1187   1.0000   0.0369
 -17.500  -1.0866   0.03545   0.03174  -0.1285   0.9968   0.0370
 -17.250  -1.0781   0.03121   0.02735  -0.1347   0.9930   0.0375
 -17.000  -1.0664   0.02861   0.02462  -0.1379   0.9852   0.0380
 -16.750  -1.0518   0.02679   0.02268  -0.1397   0.9763   0.0384
 -16.500  -1.0502   0.02484   0.02064  -0.1393   0.9616   0.0391
 -16.250  -1.0465   0.02356   0.01926  -0.1376   0.9476   0.0397
 -16.000  -1.0395   0.02260   0.01821  -0.1356   0.9352   0.0403
 -15.750  -1.0302   0.02184   0.01737  -0.1335   0.9248   0.0409
 -15.250  -0.9990   0.02060   0.01595  -0.1308   0.9092   0.0423
 -15.000  -0.9806   0.02003   0.01528  -0.1297   0.9020   0.0430
 -14.750  -0.9632   0.01934   0.01455  -0.1286   0.8949   0.0441
 -14.500  -0.9423   0.01884   0.01402  -0.1278   0.8878   0.0451
 -14.250  -0.9202   0.01843   0.01354  -0.1271   0.8810   0.0462
 -14.000  -0.8967   0.01805   0.01308  -0.1265   0.8751   0.0473
 -13.750  -0.8744   0.01756   0.01255  -0.1258   0.8690   0.0484
 -13.500  -0.8506   0.01720   0.01216  -0.1253   0.8627   0.0496
 -13.250  -0.8254   0.01693   0.01184  -0.1249   0.8569   0.0508
 -13.000  -0.7995   0.01665   0.01152  -0.1246   0.8515   0.0520
 -12.750  -0.7742   0.01635   0.01114  -0.1242   0.8459   0.0531
 -12.500  -0.7491   0.01607   0.01083  -0.1238   0.8399   0.0543
 -12.250  -0.7218   0.01588   0.01065  -0.1236   0.8352   0.0555
 -12.000  -0.6945   0.01572   0.01045  -0.1235   0.8295   0.0567
 -11.750  -0.6673   0.01558   0.01022  -0.1232   0.8233   0.0577
 -11.500  -0.6411   0.01531   0.00988  -0.1230   0.8172   0.0587
 -11.250  -0.6151   0.01500   0.00957  -0.1227   0.8108   0.0598
 -11.000  -0.5877   0.01486   0.00939  -0.1225   0.8047   0.0608
 -10.750  -0.5601   0.01472   0.00921  -0.1224   0.7997   0.0618
 -10.500  -0.5320   0.01456   0.00902  -0.1223   0.7951   0.0628
 -10.250  -0.5039   0.01444   0.00883  -0.1223   0.7898   0.0637
 -10.000  -0.4756   0.01438   0.00868  -0.1222   0.7845   0.0643
  -9.750  -0.4505   0.01387   0.00817  -0.1219   0.7795   0.0657
  -9.500  -0.4227   0.01367   0.00796  -0.1218   0.7740   0.0666
  -9.250  -0.3949   0.01350   0.00777  -0.1217   0.7679   0.0674
  -9.000  -0.3672   0.01336   0.00756  -0.1216   0.7619   0.0684
  -8.750  -0.3389   0.01318   0.00736  -0.1216   0.7564   0.0693
  -8.500  -0.3105   0.01305   0.00717  -0.1216   0.7503   0.0701
  -8.250  -0.2821   0.01299   0.00702  -0.1216   0.7439   0.0707
  -8.000  -0.2557   0.01252   0.00654  -0.1214   0.7383   0.0719
  -7.750  -0.2283   0.01224   0.00625  -0.1213   0.7314   0.0729
  -7.500  -0.2007   0.01207   0.00604  -0.1211   0.7243   0.0737
  -7.250  -0.1722   0.01190   0.00585  -0.1212   0.7176   0.0747
  -7.000  -0.1441   0.01176   0.00567  -0.1211   0.7095   0.0757
  -6.750  -0.1158   0.01163   0.00549  -0.1211   0.7017   0.0766
  -6.500  -0.0873   0.01154   0.00535  -0.1211   0.6923   0.0775
  -6.250  -0.0590   0.01148   0.00523  -0.1211   0.6826   0.0781
  -6.000  -0.0329   0.01111   0.00481  -0.1208   0.6709   0.0796
  -5.750  -0.0055   0.01093   0.00459  -0.1206   0.6586   0.0806
  -5.500   0.0218   0.01082   0.00443  -0.1205   0.6446   0.0816
  -5.250   0.0488   0.01075   0.00428  -0.1202   0.6286   0.0825
  -5.000   0.0758   0.01070   0.00414  -0.1200   0.6104   0.0833
  -4.750   0.1024   0.01067   0.00402  -0.1197   0.5900   0.0842
  -4.500   0.1289   0.01069   0.00393  -0.1193   0.5677   0.0850
  -4.250   0.1551   0.01075   0.00386  -0.1189   0.5450   0.0857
  -4.000   0.1808   0.01072   0.00373  -0.1185   0.5246   0.0868
  -3.750   0.2069   0.01070   0.00363  -0.1181   0.5074   0.0883
  -3.500   0.2333   0.01070   0.00357  -0.1178   0.4934   0.0897
  -3.250   0.2600   0.01072   0.00352  -0.1175   0.4817   0.0910
  -3.000   0.2874   0.01071   0.00347  -0.1174   0.4732   0.0925
  -2.750   0.3145   0.01073   0.00344  -0.1172   0.4653   0.0940
  -2.500   0.3415   0.01072   0.00339  -0.1170   0.4584   0.0966
  -2.250   0.3692   0.01067   0.00336  -0.1170   0.4536   0.0999
  -2.000   0.3966   0.01067   0.00334  -0.1168   0.4487   0.1037
  -1.750   0.4233   0.01067   0.00335  -0.1166   0.4439   0.1123
  -1.500   0.4504   0.01066   0.00338  -0.1165   0.4400   0.1265
  -1.250   0.4785   0.01063   0.00341  -0.1165   0.4375   0.1396
  -1.000   0.5063   0.01064   0.00345  -0.1165   0.4347   0.1492
  -0.750   0.5337   0.01067   0.00349  -0.1164   0.4318   0.1565
  -0.500   0.5607   0.01072   0.00354  -0.1162   0.4288   0.1629
  -0.250   0.5872   0.01082   0.00361  -0.1160   0.4255   0.1665
   0.000   0.6132   0.01090   0.00368  -0.1157   0.4219   0.1731
   0.250   0.6411   0.01090   0.00371  -0.1157   0.4204   0.1785
   0.500   0.6689   0.01093   0.00375  -0.1157   0.4184   0.1825
   0.750   0.6962   0.01094   0.00379  -0.1156   0.4161   0.1892
   1.000   0.7229   0.01098   0.00384  -0.1154   0.4135   0.1965
   1.250   0.7491   0.01104   0.00391  -0.1152   0.4108   0.2040
   1.500   0.7744   0.01112   0.00400  -0.1148   0.4075   0.2157
   1.750   0.7986   0.01123   0.00413  -0.1142   0.4038   0.2331
   2.000   0.8254   0.01115   0.00420  -0.1141   0.4024   0.2757
   2.250   0.8515   0.01091   0.00431  -0.1141   0.4008   0.3976
   2.500   0.8771   0.01062   0.00443  -0.1140   0.3988   0.5450
   2.750   0.9015   0.01031   0.00460  -0.1135   0.3967   0.7103
   3.000   0.9219   0.01009   0.00479  -0.1120   0.3947   0.8479
   3.250   0.9377   0.01008   0.00497  -0.1092   0.3927   0.9422
   3.500   0.9741   0.01027   0.00516  -0.1111   0.3901   0.9917
   3.750   1.0024   0.01048   0.00533  -0.1115   0.3874   1.0000
   4.000   1.0228   0.01069   0.00550  -0.1102   0.3851   1.0000
   4.250   1.0466   0.01079   0.00561  -0.1095   0.3841   1.0000
   4.500   1.0706   0.01091   0.00573  -0.1089   0.3828   1.0000
   4.750   1.0947   0.01105   0.00586  -0.1084   0.3813   1.0000
   5.000   1.1188   0.01120   0.00601  -0.1079   0.3794   1.0000
   5.250   1.1428   0.01136   0.00616  -0.1073   0.3773   1.0000
   5.500   1.1661   0.01155   0.00634  -0.1067   0.3750   1.0000
   5.750   1.1888   0.01178   0.00655  -0.1061   0.3727   1.0000
   6.000   1.2107   0.01206   0.00679  -0.1053   0.3700   1.0000
   6.250   1.2328   0.01234   0.00706  -0.1046   0.3672   1.0000
   6.500   1.2577   0.01250   0.00724  -0.1043   0.3656   1.0000
   6.750   1.2823   0.01267   0.00743  -0.1041   0.3633   1.0000
   7.000   1.3062   0.01288   0.00764  -0.1037   0.3610   1.0000
   7.250   1.3291   0.01313   0.00789  -0.1032   0.3585   1.0000
   7.500   1.3512   0.01342   0.00817  -0.1026   0.3557   1.0000
   7.750   1.3715   0.01381   0.00853  -0.1018   0.3521   1.0000
   8.000   1.3938   0.01411   0.00884  -0.1012   0.3491   1.0000
   8.250   1.4180   0.01433   0.00908  -0.1010   0.3459   1.0000
   8.500   1.4404   0.01463   0.00939  -0.1006   0.3419   1.0000
   8.750   1.4608   0.01503   0.00977  -0.0999   0.3381   1.0000
   9.000   1.4794   0.01552   0.01025  -0.0990   0.3338   1.0000
   9.250   1.5025   0.01582   0.01057  -0.0987   0.3308   1.0000
   9.500   1.5239   0.01620   0.01096  -0.0982   0.3265   1.0000
   9.750   1.5429   0.01670   0.01145  -0.0974   0.3212   1.0000
  10.000   1.5609   0.01726   0.01200  -0.0965   0.3160   1.0000
  10.250   1.5807   0.01773   0.01249  -0.0959   0.3103   1.0000
  10.500   1.5965   0.01843   0.01315  -0.0948   0.3030   1.0000
  10.750   1.6135   0.01909   0.01380  -0.0939   0.2961   1.0000
  11.000   1.6266   0.01997   0.01464  -0.0926   0.2871   1.0000
  11.250   1.6400   0.02085   0.01550  -0.0914   0.2780   1.0000
  11.500   1.6497   0.02197   0.01656  -0.0898   0.2681   1.0000
  11.750   1.6599   0.02309   0.01766  -0.0883   0.2594   1.0000
  12.000   1.6707   0.02419   0.01874  -0.0870   0.2526   1.0000
  12.250   1.6816   0.02532   0.01987  -0.0857   0.2466   1.0000
  12.500   1.6890   0.02670   0.02123  -0.0842   0.2401   1.0000
  12.750   1.7013   0.02779   0.02234  -0.0832   0.2356   1.0000
  13.000   1.7110   0.02909   0.02364  -0.0820   0.2307   1.0000
  13.250   1.7170   0.03071   0.02525  -0.0806   0.2258   1.0000
  13.500   1.7294   0.03185   0.02643  -0.0798   0.2230   1.0000
  13.750   1.7398   0.03317   0.02778  -0.0789   0.2199   1.0000
  14.000   1.7485   0.03465   0.02928  -0.0780   0.2167   1.0000
  14.250   1.7537   0.03646   0.03111  -0.0768   0.2132   1.0000
  14.500   1.7594   0.03827   0.03294  -0.0758   0.2102   1.0000
  14.750   1.7709   0.03960   0.03434  -0.0752   0.2083   1.0000
  15.000   1.7796   0.04118   0.03595  -0.0745   0.2057   1.0000
  15.250   1.7848   0.04310   0.03791  -0.0736   0.2026   1.0000
  15.500   1.7860   0.04544   0.04028  -0.0727   0.1993   1.0000
  15.750   1.7863   0.04790   0.04277  -0.0717   0.1962   1.0000
  16.000   1.7952   0.04958   0.04452  -0.0713   0.1943   1.0000
  16.250   1.8008   0.05157   0.04656  -0.0707   0.1917   1.0000
  16.500   1.8024   0.05399   0.04902  -0.0701   0.1887   1.0000
  16.750   1.7992   0.05696   0.05203  -0.0693   0.1856   1.0000
  17.000   1.7936   0.06023   0.05535  -0.0686   0.1825   1.0000
  17.250   1.7989   0.06235   0.05753  -0.0683   0.1800   1.0000
  17.500   1.7967   0.06531   0.06055  -0.0679   0.1764   1.0000
  17.750   1.7887   0.06894   0.06422  -0.0674   0.1726   1.0000
  18.000   1.7781   0.07293   0.06826  -0.0670   0.1689   1.0000
  18.250   1.7760   0.07599   0.07137  -0.0668   0.1648   1.0000
  18.500   1.7635   0.08024   0.07566  -0.0665   0.1596   1.0000
  18.750   1.7503   0.08465   0.08011  -0.0664   0.1552   1.0000
  19.000   1.7381   0.08899   0.08450  -0.0664   0.1492   1.0000
  19.250   1.7190   0.09421   0.08975  -0.0665   0.1428   1.0000
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