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GOE 650 AIRFOIL (goe650-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 650 AIRFOIL (goe650-il)
Reynolds number: 200,000
Max Cl/Cd: 70.47 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe650-il-200000-n5.txt
Download as CSV file: xf-goe650-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.6796   0.07874   0.07390  -0.0736   1.0000   0.0376
 -14.000  -0.6926   0.07417   0.06931  -0.0754   1.0000   0.0379
 -13.750  -0.7104   0.06915   0.06423  -0.0775   1.0000   0.0381
 -13.500  -0.7270   0.06464   0.05967  -0.0792   1.0000   0.0383
 -13.250  -0.7454   0.06023   0.05521  -0.0806   1.0000   0.0385
 -13.000  -0.7658   0.05602   0.05096  -0.0815   1.0000   0.0386
 -12.750  -0.7892   0.05203   0.04692  -0.0818   1.0000   0.0387
 -12.500  -0.8176   0.04833   0.04318  -0.0812   1.0000   0.0388
 -12.250  -0.8293   0.04414   0.03890  -0.0846   0.9966   0.0390
 -12.000  -0.8197   0.03942   0.03402  -0.0925   0.9891   0.0396
 -11.750  -0.7982   0.03538   0.02977  -0.1003   0.9835   0.0404
 -11.500  -0.7799   0.03293   0.02714  -0.1034   0.9772   0.0411
 -11.250  -0.7561   0.03092   0.02494  -0.1064   0.9726   0.0419
 -11.000  -0.7337   0.02928   0.02310  -0.1081   0.9674   0.0427
 -10.750  -0.7112   0.02780   0.02155  -0.1094   0.9620   0.0435
 -10.500  -0.6834   0.02644   0.02012  -0.1115   0.9587   0.0446
 -10.250  -0.6613   0.02534   0.01892  -0.1119   0.9532   0.0458
 -10.000  -0.6363   0.02429   0.01776  -0.1127   0.9483   0.0471
  -9.750  -0.6071   0.02328   0.01660  -0.1141   0.9453   0.0485
  -9.250  -0.5566   0.02146   0.01465  -0.1149   0.9356   0.0515
  -9.000  -0.5274   0.02065   0.01374  -0.1159   0.9320   0.0540
  -8.750  -0.4957   0.01984   0.01286  -0.1173   0.9294   0.0570
  -8.500  -0.4622   0.01911   0.01207  -0.1190   0.9274   0.0615
  -8.250  -0.4423   0.01857   0.01150  -0.1178   0.9200   0.0661
  -8.000  -0.4120   0.01800   0.01089  -0.1186   0.9164   0.0731
  -7.750  -0.3791   0.01751   0.01033  -0.1198   0.9137   0.0812
  -7.500  -0.3449   0.01709   0.00985  -0.1212   0.9115   0.0896
  -7.250  -0.3212   0.01681   0.00955  -0.1204   0.9050   0.0959
  -7.000  -0.2911   0.01651   0.00915  -0.1209   0.9005   0.1027
  -6.750  -0.2584   0.01621   0.00882  -0.1219   0.8972   0.1089
  -6.500  -0.2242   0.01592   0.00841  -0.1231   0.8947   0.1147
  -6.250  -0.1995   0.01569   0.00819  -0.1225   0.8888   0.1191
  -6.000  -0.1709   0.01547   0.00791  -0.1226   0.8838   0.1242
  -5.750  -0.1385   0.01521   0.00757  -0.1234   0.8799   0.1300
  -5.500  -0.1043   0.01496   0.00729  -0.1246   0.8762   0.1369
  -5.250  -0.0806   0.01484   0.00708  -0.1236   0.8682   0.1423
  -5.000  -0.0501   0.01453   0.00680  -0.1240   0.8629   0.1480
  -4.750  -0.0175   0.01430   0.00650  -0.1248   0.8582   0.1543
  -4.500   0.0069   0.01413   0.00628  -0.1239   0.8501   0.1592
  -4.250   0.0372   0.01384   0.00600  -0.1242   0.8447   0.1642
  -4.000   0.0665   0.01365   0.00576  -0.1243   0.8396   0.1694
  -3.750   0.0920   0.01351   0.00558  -0.1237   0.8332   0.1745
  -3.500   0.1209   0.01329   0.00538  -0.1238   0.8281   0.1808
  -3.250   0.1516   0.01312   0.00517  -0.1241   0.8238   0.1882
  -3.000   0.1759   0.01300   0.00508  -0.1233   0.8173   0.1947
  -2.750   0.2039   0.01286   0.00494  -0.1231   0.8120   0.2031
  -2.500   0.2347   0.01270   0.00478  -0.1235   0.8076   0.2129
  -2.250   0.2593   0.01263   0.00472  -0.1227   0.8008   0.2239
  -2.000   0.2866   0.01252   0.00465  -0.1224   0.7952   0.2362
  -1.750   0.3167   0.01240   0.00455  -0.1226   0.7907   0.2505
  -1.500   0.3417   0.01235   0.00455  -0.1219   0.7838   0.2653
  -1.250   0.3693   0.01226   0.00448  -0.1216   0.7764   0.2818
  -1.000   0.3968   0.01220   0.00443  -0.1212   0.7683   0.2980
  -0.750   0.4235   0.01214   0.00437  -0.1206   0.7586   0.3144
  -0.500   0.4497   0.01210   0.00434  -0.1200   0.7484   0.3307
  -0.250   0.4777   0.01205   0.00427  -0.1197   0.7382   0.3461
   0.000   0.5022   0.01203   0.00430  -0.1187   0.7274   0.3602
   0.250   0.5300   0.01202   0.00427  -0.1184   0.7188   0.3748
   0.500   0.5545   0.01203   0.00431  -0.1174   0.7083   0.3884
   0.750   0.5808   0.01204   0.00432  -0.1168   0.6986   0.4026
   1.000   0.6058   0.01204   0.00435  -0.1160   0.6873   0.4159
   1.250   0.6303   0.01206   0.00440  -0.1150   0.6755   0.4288
   1.500   0.6553   0.01208   0.00442  -0.1142   0.6632   0.4423
   1.750   0.6798   0.01211   0.00445  -0.1132   0.6493   0.4568
   2.000   0.7032   0.01213   0.00451  -0.1121   0.6335   0.4719
   2.250   0.7263   0.01217   0.00456  -0.1108   0.6156   0.4893
   2.500   0.7489   0.01223   0.00462  -0.1095   0.5959   0.5082
   2.750   0.7710   0.01232   0.00469  -0.1081   0.5751   0.5272
   3.000   0.7924   0.01245   0.00478  -0.1066   0.5537   0.5465
   3.250   0.8132   0.01261   0.00490  -0.1050   0.5338   0.5677
   3.500   0.8335   0.01279   0.00506  -0.1033   0.5145   0.5929
   3.750   0.8536   0.01296   0.00524  -0.1016   0.4958   0.6243
   4.000   0.8741   0.01310   0.00544  -0.1000   0.4762   0.6682
   4.500   0.9408   0.01335   0.00598  -0.1024   0.4220   1.0000
   4.750   0.9576   0.01374   0.00622  -0.1003   0.3957   1.0000
   5.000   0.9730   0.01418   0.00649  -0.0979   0.3716   1.0000
   5.250   0.9887   0.01460   0.00679  -0.0955   0.3512   1.0000
   5.500   1.0038   0.01503   0.00710  -0.0931   0.3347   1.0000
   5.750   1.0190   0.01546   0.00744  -0.0907   0.3204   1.0000
   6.000   1.0350   0.01589   0.00780  -0.0885   0.3075   1.0000
   6.250   1.0522   0.01630   0.00816  -0.0866   0.2960   1.0000
   6.500   1.0685   0.01675   0.00855  -0.0845   0.2858   1.0000
   6.750   1.0861   0.01717   0.00895  -0.0827   0.2757   1.0000
   7.000   1.1031   0.01761   0.00936  -0.0809   0.2667   1.0000
   7.250   1.1199   0.01808   0.00979  -0.0790   0.2570   1.0000
   7.500   1.1372   0.01853   0.01023  -0.0773   0.2484   1.0000
   7.750   1.1535   0.01903   0.01071  -0.0754   0.2399   1.0000
   8.000   1.1704   0.01952   0.01120  -0.0737   0.2321   1.0000
   8.250   1.1861   0.02006   0.01172  -0.0719   0.2234   1.0000
   8.500   1.2024   0.02059   0.01226  -0.0701   0.2158   1.0000
   8.750   1.2175   0.02118   0.01284  -0.0683   0.2075   1.0000
   9.000   1.2330   0.02178   0.01344  -0.0666   0.1998   1.0000
   9.250   1.2475   0.02242   0.01407  -0.0648   0.1920   1.0000
   9.500   1.2622   0.02309   0.01474  -0.0631   0.1850   1.0000
   9.750   1.2766   0.02377   0.01545  -0.0614   0.1779   1.0000
  10.000   1.2899   0.02454   0.01621  -0.0596   0.1720   1.0000
  10.250   1.3048   0.02523   0.01695  -0.0580   0.1659   1.0000
  10.500   1.3169   0.02609   0.01781  -0.0563   0.1602   1.0000
  10.750   1.3307   0.02689   0.01865  -0.0547   0.1546   1.0000
  11.000   1.3437   0.02774   0.01954  -0.0532   0.1494   1.0000
  11.250   1.3544   0.02875   0.02056  -0.0515   0.1450   1.0000
  11.500   1.3679   0.02962   0.02151  -0.0500   0.1410   1.0000
  11.750   1.3803   0.03058   0.02253  -0.0486   0.1366   1.0000
  12.000   1.3897   0.03174   0.02370  -0.0470   0.1320   1.0000
  12.250   1.4012   0.03280   0.02483  -0.0457   0.1275   1.0000
  12.500   1.4120   0.03393   0.02603  -0.0443   0.1228   1.0000
  12.750   1.4201   0.03527   0.02740  -0.0429   0.1189   1.0000
  13.000   1.4300   0.03652   0.02873  -0.0416   0.1148   1.0000
  13.250   1.4391   0.03785   0.03014  -0.0404   0.1099   1.0000
  13.500   1.4442   0.03955   0.03185  -0.0391   0.1053   1.0000
  13.750   1.4536   0.04093   0.03334  -0.0381   0.1005   1.0000
  14.000   1.4589   0.04270   0.03516  -0.0370   0.0953   1.0000
  14.250   1.4648   0.04449   0.03703  -0.0360   0.0899   1.0000
  14.500   1.4680   0.04656   0.03915  -0.0351   0.0839   1.0000
  14.750   1.4717   0.04865   0.04132  -0.0343   0.0771   1.0000
  15.000   1.4722   0.05115   0.04385  -0.0335   0.0692   1.0000
  15.250   1.4709   0.05393   0.04666  -0.0330   0.0611   1.0000
  15.500   1.4664   0.05716   0.04991  -0.0326   0.0538   1.0000
  15.750   1.4604   0.06070   0.05348  -0.0325   0.0489   1.0000
  16.000   1.4537   0.06447   0.05732  -0.0326   0.0457   1.0000
  16.250   1.4454   0.06861   0.06154  -0.0330   0.0435   1.0000
  16.500   1.4382   0.07275   0.06579  -0.0337   0.0420   1.0000
  16.750   1.4297   0.07721   0.07037  -0.0345   0.0407   1.0000
  17.000   1.4185   0.08221   0.07548  -0.0358   0.0395   1.0000
  17.250   1.4063   0.08752   0.08092  -0.0374   0.0387   1.0000
  17.750   1.3804   0.09878   0.09243  -0.0413   0.0373   1.0000
  18.000   1.3684   0.10445   0.09826  -0.0435   0.0367   1.0000
  18.250   1.3554   0.11041   0.10436  -0.0460   0.0361   1.0000
  18.500   1.3425   0.11646   0.11053  -0.0486   0.0356   1.0000
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