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GOE 650 AIRFOIL (goe650-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 650 AIRFOIL (goe650-il)
Reynolds number: 200,000
Max Cl/Cd: 79 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe650-il-200000.txt
Download as CSV file: xf-goe650-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.6912   0.06033   0.05614  -0.0792   1.0000   0.0563
 -11.750  -0.7358   0.05492   0.05070  -0.0798   1.0000   0.0559
 -11.500  -0.7826   0.05129   0.04707  -0.0782   1.0000   0.0555
 -11.250  -0.8218   0.04651   0.04210  -0.0794   1.0000   0.0551
 -11.000  -0.8443   0.04272   0.03803  -0.0791   1.0000   0.0553
 -10.750  -0.8387   0.03852   0.03332  -0.0826   0.9967   0.0560
 -10.500  -0.8145   0.03509   0.02951  -0.0866   0.9921   0.0570
 -10.250  -0.7867   0.03338   0.02778  -0.0885   0.9876   0.0582
 -10.000  -0.7559   0.03187   0.02613  -0.0909   0.9838   0.0595
  -9.750  -0.7281   0.03035   0.02440  -0.0927   0.9795   0.0612
  -9.500  -0.7013   0.02884   0.02260  -0.0940   0.9745   0.0629
  -9.250  -0.6705   0.02726   0.02079  -0.0960   0.9711   0.0647
  -9.000  -0.6413   0.02631   0.01987  -0.0971   0.9673   0.0665
  -8.750  -0.6145   0.02545   0.01893  -0.0976   0.9618   0.0687
  -8.500  -0.5813   0.02449   0.01773  -0.0992   0.9583   0.0717
  -8.250  -0.5462   0.02360   0.01686  -0.1013   0.9560   0.0752
  -8.000  -0.5256   0.02304   0.01625  -0.1004   0.9494   0.0787
  -7.750  -0.4958   0.02223   0.01535  -0.1012   0.9454   0.0835
  -7.500  -0.4607   0.02172   0.01476  -0.1029   0.9427   0.0911
  -7.250  -0.4232   0.02130   0.01434  -0.1050   0.9408   0.1014
  -7.000  -0.4068   0.02109   0.01416  -0.1031   0.9327   0.1096
  -6.750  -0.3740   0.02090   0.01391  -0.1043   0.9293   0.1201
  -6.500  -0.3375   0.02081   0.01364  -0.1060   0.9270   0.1296
  -6.250  -0.2995   0.02061   0.01351  -0.1081   0.9252   0.1374
  -6.000  -0.2839   0.02061   0.01333  -0.1058   0.9163   0.1429
  -5.750  -0.2474   0.02014   0.01294  -0.1075   0.9130   0.1497
  -5.500  -0.2057   0.01984   0.01249  -0.1099   0.9106   0.1572
  -5.250  -0.1630   0.01925   0.01194  -0.1127   0.9090   0.1643
  -5.000  -0.1494   0.01929   0.01194  -0.1100   0.8996   0.1699
  -4.750  -0.1138   0.01891   0.01151  -0.1114   0.8968   0.1780
  -4.500  -0.0753   0.01863   0.01124  -0.1133   0.8948   0.1861
  -4.250  -0.0350   0.01811   0.01064  -0.1156   0.8934   0.1931
  -4.000  -0.0149   0.01795   0.01052  -0.1141   0.8869   0.1981
  -3.750   0.0151   0.01772   0.01023  -0.1143   0.8822   0.2052
  -3.500   0.0527   0.01723   0.00978  -0.1160   0.8797   0.2128
  -3.250   0.0914   0.01686   0.00939  -0.1179   0.8777   0.2219
  -3.000   0.1310   0.01640   0.00898  -0.1199   0.8759   0.2320
  -2.750   0.1473   0.01647   0.00901  -0.1175   0.8677   0.2407
  -2.500   0.1802   0.01612   0.00877  -0.1183   0.8636   0.2522
  -2.250   0.2173   0.01575   0.00845  -0.1198   0.8609   0.2664
  -2.000   0.2565   0.01540   0.00816  -0.1216   0.8587   0.2840
  -1.750   0.2737   0.01546   0.00827  -0.1194   0.8503   0.2986
  -1.500   0.3065   0.01522   0.00810  -0.1200   0.8457   0.3185
  -1.250   0.3460   0.01487   0.00779  -0.1217   0.8423   0.3416
  -1.000   0.3706   0.01477   0.00775  -0.1207   0.8341   0.3605
  -0.750   0.4055   0.01443   0.00742  -0.1214   0.8273   0.3815
  -0.500   0.4402   0.01413   0.00713  -0.1220   0.8204   0.4014
  -0.250   0.4667   0.01395   0.00699  -0.1212   0.8110   0.4183
   0.000   0.5035   0.01367   0.00671  -0.1224   0.8052   0.4368
   0.250   0.5244   0.01364   0.00676  -0.1206   0.7951   0.4513
   0.500   0.5602   0.01339   0.00650  -0.1216   0.7888   0.4691
   0.750   0.5812   0.01335   0.00654  -0.1199   0.7781   0.4837
   1.000   0.6156   0.01314   0.00632  -0.1206   0.7709   0.5015
   1.250   0.6371   0.01309   0.00634  -0.1190   0.7595   0.5174
   1.500   0.6655   0.01296   0.00625  -0.1186   0.7500   0.5354
   1.750   0.6921   0.01283   0.00617  -0.1179   0.7392   0.5544
   2.000   0.7161   0.01275   0.00616  -0.1167   0.7275   0.5750
   2.250   0.7440   0.01262   0.00607  -0.1162   0.7166   0.6009
   2.500   0.7674   0.01249   0.00605  -0.1149   0.7035   0.6285
   2.750   0.7897   0.01234   0.00604  -0.1133   0.6896   0.6632
   3.000   0.8132   0.01209   0.00600  -0.1120   0.6752   0.7191
   3.250   0.8738   0.01163   0.00593  -0.1185   0.6561   1.0000
   3.500   0.8970   0.01171   0.00591  -0.1172   0.6382   1.0000
   3.750   0.9192   0.01181   0.00590  -0.1158   0.6184   1.0000
   4.000   0.9407   0.01196   0.00590  -0.1141   0.5967   1.0000
   4.250   0.9606   0.01216   0.00598  -0.1122   0.5724   1.0000
   4.500   0.9803   0.01245   0.00607  -0.1103   0.5478   1.0000
   4.750   0.9987   0.01279   0.00626  -0.1083   0.5222   1.0000
   5.000   1.0164   0.01320   0.00650  -0.1061   0.4969   1.0000
   5.250   1.0329   0.01360   0.00677  -0.1038   0.4709   1.0000
   5.500   1.0484   0.01402   0.00705  -0.1013   0.4448   1.0000
   5.750   1.0632   0.01445   0.00736  -0.0987   0.4192   1.0000
   6.000   1.0772   0.01492   0.00769  -0.0960   0.3955   1.0000
   6.250   1.0909   0.01543   0.00805  -0.0933   0.3756   1.0000
   6.500   1.1043   0.01595   0.00844  -0.0906   0.3581   1.0000
   6.750   1.1186   0.01648   0.00887  -0.0881   0.3423   1.0000
   7.000   1.1340   0.01701   0.00933  -0.0858   0.3282   1.0000
   7.250   1.1500   0.01756   0.00981  -0.0837   0.3154   1.0000
   7.500   1.1661   0.01817   0.01032  -0.0817   0.3042   1.0000
   7.750   1.1824   0.01869   0.01083  -0.0798   0.2929   1.0000
   8.000   1.1990   0.01925   0.01137  -0.0779   0.2823   1.0000
   8.250   1.2148   0.01992   0.01191  -0.0760   0.2720   1.0000
   8.500   1.2293   0.02039   0.01245  -0.0738   0.2614   1.0000
   8.750   1.2440   0.02101   0.01304  -0.0718   0.2516   1.0000
   9.000   1.2580   0.02159   0.01361  -0.0697   0.2422   1.0000
   9.250   1.2729   0.02223   0.01425  -0.0677   0.2334   1.0000
   9.500   1.2866   0.02289   0.01488  -0.0657   0.2252   1.0000
   9.750   1.3012   0.02356   0.01559  -0.0639   0.2173   1.0000
  10.000   1.3150   0.02425   0.01628  -0.0620   0.2101   1.0000
  10.250   1.3298   0.02501   0.01704  -0.0603   0.2036   1.0000
  10.500   1.3434   0.02571   0.01781  -0.0585   0.1970   1.0000
  10.750   1.3571   0.02659   0.01859  -0.0568   0.1909   1.0000
  11.000   1.3694   0.02730   0.01945  -0.0549   0.1848   1.0000
  11.250   1.3811   0.02814   0.02030  -0.0531   0.1792   1.0000
  11.500   1.3949   0.02906   0.02121  -0.0516   0.1743   1.0000
  11.750   1.4067   0.02990   0.02219  -0.0499   0.1692   1.0000
  12.000   1.4173   0.03085   0.02316  -0.0482   0.1643   1.0000
  12.250   1.4284   0.03188   0.02421  -0.0466   0.1595   1.0000
  12.500   1.4377   0.03289   0.02535  -0.0449   0.1543   1.0000
  12.750   1.4458   0.03404   0.02652  -0.0433   0.1494   1.0000
  13.000   1.4549   0.03524   0.02779  -0.0417   0.1449   1.0000
  13.250   1.4627   0.03647   0.02916  -0.0403   0.1397   1.0000
  13.500   1.4680   0.03793   0.03063  -0.0388   0.1348   1.0000
  13.750   1.4744   0.03939   0.03222  -0.0374   0.1293   1.0000
  14.000   1.4782   0.04106   0.03398  -0.0361   0.1232   1.0000
  14.250   1.4811   0.04293   0.03595  -0.0349   0.1166   1.0000
  14.500   1.4813   0.04513   0.03819  -0.0339   0.1091   1.0000
  14.750   1.4816   0.04747   0.04063  -0.0330   0.0997   1.0000
  15.000   1.4781   0.05030   0.04351  -0.0322   0.0898   1.0000
  15.250   1.4723   0.05354   0.04677  -0.0316   0.0806   1.0000
  15.500   1.4648   0.05711   0.05033  -0.0312   0.0741   1.0000
  15.750   1.4587   0.06066   0.05394  -0.0310   0.0685   1.0000
  16.000   1.4513   0.06451   0.05784  -0.0311   0.0647   1.0000
  16.250   1.4457   0.06828   0.06169  -0.0314   0.0615   1.0000
  16.500   1.4363   0.07265   0.06610  -0.0320   0.0592   1.0000
  16.750   1.4296   0.07677   0.07031  -0.0326   0.0571   1.0000
  17.000   1.4237   0.08089   0.07455  -0.0334   0.0552   1.0000
  17.250   1.4165   0.08528   0.07901  -0.0344   0.0536   1.0000
  17.500   1.4078   0.08989   0.08366  -0.0356   0.0522   1.0000
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