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GOE 797 AIRFOIL (goe797-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 797 AIRFOIL (goe797-il)
Reynolds number: 200,000
Max Cl/Cd: 75.95 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe797-il-200000.txt
Download as CSV file: xf-goe797-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 797 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
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.0636   0.09149   0.08782  -0.0926   0.9584   0.0984
  -9.500  -0.0487   0.08761   0.08393  -0.0956   0.9555   0.1010
  -9.250  -0.3001   0.06431   0.06040  -0.1148   0.9553   0.0765
  -9.000  -0.2975   0.05893   0.05491  -0.1185   0.9458   0.0754
  -8.750  -0.3230   0.04751   0.04305  -0.1253   0.9367   0.0739
  -8.500  -0.3515   0.03790   0.03261  -0.1255   0.9231   0.0736
  -8.250  -0.3504   0.03328   0.02735  -0.1243   0.9128   0.0744
  -8.000  -0.3338   0.02998   0.02338  -0.1241   0.9068   0.0758
  -7.750  -0.3100   0.02827   0.02153  -0.1242   0.9012   0.0774
  -7.500  -0.2863   0.02768   0.02094  -0.1238   0.8932   0.0791
  -7.250  -0.2584   0.02669   0.01982  -0.1240   0.8887   0.0813
  -7.000  -0.2363   0.02540   0.01821  -0.1234   0.8816   0.0836
  -6.750  -0.2128   0.02406   0.01656  -0.1228   0.8748   0.0857
  -6.500  -0.1836   0.02335   0.01590  -0.1232   0.8705   0.0881
  -6.250  -0.1591   0.02293   0.01541  -0.1227   0.8634   0.0910
  -6.000  -0.1330   0.02224   0.01446  -0.1223   0.8573   0.0945
  -5.750  -0.1046   0.02134   0.01353  -0.1225   0.8532   0.0975
  -5.500  -0.0787   0.02106   0.01323  -0.1222   0.8467   0.1009
  -5.250  -0.0521   0.02066   0.01265  -0.1219   0.8406   0.1054
  -5.000  -0.0235   0.01999   0.01198  -0.1221   0.8363   0.1096
  -4.750   0.0040   0.01974   0.01170  -0.1220   0.8314   0.1144
  -4.500   0.0299   0.01937   0.01120  -0.1217   0.8251   0.1198
  -4.250   0.0584   0.01900   0.01088  -0.1218   0.8204   0.1252
  -4.000   0.0887   0.01878   0.01048  -0.1220   0.8168   0.1320
  -3.750   0.1131   0.01840   0.01021  -0.1217   0.8105   0.1382
  -3.500   0.1410   0.01824   0.00996  -0.1216   0.8055   0.1458
  -3.250   0.1701   0.01773   0.00947  -0.1218   0.8015   0.1534
  -3.000   0.1982   0.01759   0.00927  -0.1219   0.7971   0.1616
  -2.750   0.2239   0.01729   0.00902  -0.1216   0.7914   0.1694
  -2.500   0.2524   0.01708   0.00879  -0.1217   0.7866   0.1781
  -2.250   0.2824   0.01667   0.00836  -0.1220   0.7825   0.1869
  -2.000   0.3078   0.01659   0.00831  -0.1216   0.7757   0.1958
  -1.750   0.3354   0.01628   0.00803  -0.1214   0.7698   0.2053
  -1.500   0.3659   0.01607   0.00774  -0.1217   0.7651   0.2164
  -1.250   0.3910   0.01591   0.00771  -0.1213   0.7585   0.2277
  -1.000   0.4184   0.01571   0.00755  -0.1212   0.7525   0.2415
  -0.750   0.4486   0.01543   0.00729  -0.1214   0.7474   0.2599
  -0.500   0.4735   0.01528   0.00729  -0.1209   0.7405   0.2861
  -0.250   0.4998   0.01489   0.00720  -0.1207   0.7346   0.3469
   0.000   0.5221   0.01389   0.00720  -0.1197   0.7304   0.6080
   0.250   0.5403   0.01341   0.00752  -0.1162   0.7256   0.8808
   0.500   0.5958   0.01349   0.00761  -0.1214   0.7199   0.9778
   0.750   0.6536   0.01352   0.00750  -0.1276   0.7149   1.0000
   1.250   0.6996   0.01375   0.00757  -0.1258   0.7036   1.0000
   1.500   0.7238   0.01382   0.00755  -0.1251   0.6977   1.0000
   1.750   0.7517   0.01387   0.00746  -0.1250   0.6929   1.0000
   2.000   0.7721   0.01405   0.00765  -0.1236   0.6861   1.0000
   2.250   0.7969   0.01414   0.00768  -0.1230   0.6799   1.0000
   2.500   0.8258   0.01418   0.00760  -0.1230   0.6750   1.0000
   2.750   0.8469   0.01436   0.00780  -0.1218   0.6676   1.0000
   3.000   0.8730   0.01441   0.00780  -0.1214   0.6610   1.0000
   3.250   0.9010   0.01447   0.00777  -0.1213   0.6551   1.0000
   3.500   0.9230   0.01458   0.00791  -0.1202   0.6465   1.0000
   3.750   0.9518   0.01457   0.00780  -0.1202   0.6398   1.0000
   4.000   0.9738   0.01470   0.00796  -0.1191   0.6308   1.0000
   4.250   1.0012   0.01470   0.00789  -0.1188   0.6231   1.0000
   4.500   1.0239   0.01481   0.00802  -0.1179   0.6136   1.0000
   4.750   1.0507   0.01482   0.00796  -0.1175   0.6050   1.0000
   5.000   1.0724   0.01494   0.00810  -0.1163   0.5938   1.0000
   5.250   1.0973   0.01499   0.00810  -0.1157   0.5833   1.0000
   5.500   1.1201   0.01505   0.00811  -0.1146   0.5704   1.0000
   5.750   1.1403   0.01517   0.00822  -0.1131   0.5554   1.0000
   6.000   1.1605   0.01533   0.00833  -0.1116   0.5397   1.0000
   6.250   1.1803   0.01554   0.00848  -0.1101   0.5237   1.0000
   6.500   1.1996   0.01581   0.00868  -0.1085   0.5079   1.0000
   6.750   1.2185   0.01613   0.00892  -0.1069   0.4929   1.0000
   7.000   1.2377   0.01650   0.00921  -0.1054   0.4795   1.0000
   7.250   1.2568   0.01691   0.00950  -0.1039   0.4669   1.0000
   7.500   1.2736   0.01733   0.00989  -0.1020   0.4540   1.0000
   7.750   1.2914   0.01777   0.01030  -0.1004   0.4433   1.0000
   8.000   1.3108   0.01824   0.01067  -0.0991   0.4339   1.0000
   8.250   1.3260   0.01869   0.01115  -0.0970   0.4248   1.0000
   8.500   1.3461   0.01919   0.01155  -0.0958   0.4169   1.0000
   8.750   1.3611   0.01967   0.01211  -0.0938   0.4090   1.0000
   9.000   1.3802   0.02019   0.01257  -0.0925   0.4017   1.0000
   9.250   1.3970   0.02072   0.01314  -0.0909   0.3945   1.0000
   9.500   1.4132   0.02127   0.01370  -0.0893   0.3872   1.0000
   9.750   1.4329   0.02184   0.01423  -0.0882   0.3804   1.0000
  10.000   1.4457   0.02243   0.01491  -0.0861   0.3733   1.0000
  10.250   1.4657   0.02302   0.01542  -0.0852   0.3661   1.0000
  10.500   1.4762   0.02371   0.01623  -0.0828   0.3590   1.0000
  10.750   1.4901   0.02438   0.01691  -0.0810   0.3517   1.0000
  11.000   1.5033   0.02512   0.01768  -0.0792   0.3442   1.0000
  11.250   1.5125   0.02592   0.01856  -0.0769   0.3364   1.0000
  11.500   1.5254   0.02673   0.01936  -0.0752   0.3286   1.0000
  11.750   1.5309   0.02773   0.02046  -0.0726   0.3201   1.0000
  12.000   1.5410   0.02868   0.02139  -0.0707   0.3118   1.0000
  12.250   1.5443   0.02988   0.02271  -0.0681   0.3026   1.0000
  12.500   1.5499   0.03110   0.02396  -0.0659   0.2933   1.0000
  12.750   1.5526   0.03250   0.02542  -0.0636   0.2834   1.0000
  13.000   1.5543   0.03409   0.02710  -0.0614   0.2725   1.0000
  13.250   1.5556   0.03578   0.02878  -0.0594   0.2619   1.0000
  13.500   1.5554   0.03768   0.03071  -0.0574   0.2505   1.0000
  13.750   1.5561   0.03967   0.03277  -0.0557   0.2388   1.0000
  14.000   1.5565   0.04178   0.03488  -0.0541   0.2281   1.0000
  14.250   1.5554   0.04409   0.03713  -0.0526   0.2184   1.0000
  14.500   1.5568   0.04631   0.03941  -0.0514   0.2084   1.0000
  14.750   1.5572   0.04864   0.04172  -0.0502   0.2002   1.0000
  15.000   1.5574   0.05106   0.04413  -0.0490   0.1923   1.0000
  15.250   1.5585   0.05340   0.04649  -0.0480   0.1854   1.0000
  15.500   1.5595   0.05581   0.04891  -0.0470   0.1788   1.0000
  15.750   1.5612   0.05812   0.05119  -0.0460   0.1729   1.0000
  16.000   1.5628   0.06061   0.05378  -0.0454   0.1670   1.0000
  16.250   1.5646   0.06290   0.05597  -0.0444   0.1613   1.0000
  16.500   1.5650   0.06562   0.05884  -0.0440   0.1561   1.0000
  16.750   1.5651   0.06835   0.06163  -0.0435   0.1509   1.0000
  17.000   1.5676   0.07066   0.06389  -0.0428   0.1461   1.0000
  17.250   1.5665   0.07375   0.06716  -0.0427   0.1416   1.0000
  17.500   1.5657   0.07672   0.07020  -0.0426   0.1372   1.0000
  17.750   1.5678   0.07915   0.07258  -0.0422   0.1330   1.0000
  18.000   1.5643   0.08270   0.07634  -0.0424   0.1289   1.0000
  18.250   1.5615   0.08613   0.07987  -0.0427   0.1248   1.0000
  18.500   1.5619   0.08890   0.08257  -0.0426   0.1208   1.0000
  18.750   1.5563   0.09295   0.08686  -0.0434   0.1169   1.0000
  19.000   1.5514   0.09684   0.09086  -0.0441   0.1129   1.0000
  19.250   1.5484   0.10026   0.09424  -0.0446   0.1090   1.0000
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