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GOE 435 AIRFOIL (goe435-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 435 AIRFOIL (goe435-il)
Reynolds number: 200,000
Max Cl/Cd: 50.23 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe435-il-200000-n5.txt
Download as CSV file: xf-goe435-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 435 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.4273   0.09710   0.09093  -0.0739   0.8463   0.0813
 -14.750  -0.4214   0.09468   0.08845  -0.0748   0.8350   0.0820
 -14.500  -0.4178   0.09197   0.08566  -0.0757   0.8245   0.0826
 -14.250  -0.4161   0.08896   0.08262  -0.0770   0.8163   0.0834
 -14.000  -0.4261   0.08418   0.07777  -0.0792   0.8088   0.0843
 -13.750  -0.4618   0.07581   0.06921  -0.0832   0.8029   0.0850
 -13.500  -0.5037   0.06696   0.06010  -0.0876   0.7974   0.0856
 -13.250  -0.5282   0.06069   0.05365  -0.0909   0.7913   0.0864
 -13.000  -0.5434   0.05580   0.04861  -0.0935   0.7848   0.0875
 -12.750  -0.5539   0.05167   0.04436  -0.0957   0.7789   0.0888
 -12.500  -0.5632   0.04789   0.04046  -0.0976   0.7734   0.0906
 -12.250  -0.5736   0.04414   0.03663  -0.0996   0.7686   0.0936
 -12.000  -0.5856   0.04012   0.03269  -0.1022   0.7635   0.0995
 -11.750  -0.5928   0.03645   0.02924  -0.1058   0.7581   0.1251
 -11.500  -0.5781   0.03518   0.02778  -0.1063   0.7531   0.1357
 -11.250  -0.5656   0.03366   0.02615  -0.1074   0.7483   0.1401
 -11.000  -0.5511   0.03236   0.02467  -0.1083   0.7438   0.1439
 -10.750  -0.5359   0.03108   0.02331  -0.1095   0.7393   0.1466
 -10.500  -0.5208   0.02981   0.02200  -0.1107   0.7342   0.1490
 -10.250  -0.5053   0.02866   0.02075  -0.1118   0.7289   0.1517
 -10.000  -0.4918   0.02766   0.01960  -0.1125   0.7236   0.1543
  -9.750  -0.4756   0.02678   0.01854  -0.1133   0.7188   0.1562
  -9.500  -0.4554   0.02602   0.01775  -0.1144   0.7139   0.1579
  -9.250  -0.4336   0.02535   0.01707  -0.1155   0.7085   0.1597
  -9.000  -0.4105   0.02481   0.01649  -0.1163   0.7033   0.1615
  -8.750  -0.3866   0.02436   0.01596  -0.1169   0.6982   0.1633
  -8.500  -0.3621   0.02396   0.01544  -0.1174   0.6935   0.1650
  -8.250  -0.3369   0.02360   0.01499  -0.1178   0.6887   0.1667
  -8.000  -0.3115   0.02325   0.01457  -0.1183   0.6830   0.1682
  -7.750  -0.2855   0.02294   0.01417  -0.1187   0.6772   0.1692
  -7.500  -0.2596   0.02255   0.01377  -0.1188   0.6718   0.1704
  -7.250  -0.2334   0.02220   0.01338  -0.1189   0.6668   0.1716
  -7.000  -0.2073   0.02188   0.01308  -0.1191   0.6605   0.1728
  -6.750  -0.1808   0.02157   0.01278  -0.1193   0.6535   0.1741
  -6.500  -0.1539   0.02129   0.01245  -0.1195   0.6472   0.1756
  -6.250  -0.1266   0.02104   0.01213  -0.1197   0.6415   0.1772
  -6.000  -0.0995   0.02080   0.01189  -0.1199   0.6344   0.1787
  -5.750  -0.0721   0.02056   0.01160  -0.1201   0.6276   0.1799
  -5.500  -0.0444   0.02033   0.01129  -0.1203   0.6218   0.1809
  -5.250  -0.0169   0.02013   0.01106  -0.1205   0.6149   0.1817
  -5.000   0.0108   0.01993   0.01082  -0.1206   0.6080   0.1826
  -4.750   0.0389   0.01977   0.01056  -0.1208   0.6020   0.1836
  -4.500   0.0659   0.01949   0.01032  -0.1209   0.5957   0.1851
  -4.250   0.0932   0.01924   0.01009  -0.1210   0.5889   0.1866
  -4.000   0.1208   0.01903   0.00986  -0.1212   0.5829   0.1878
  -3.750   0.1487   0.01886   0.00966  -0.1214   0.5776   0.1893
  -3.500   0.1767   0.01872   0.00952  -0.1216   0.5722   0.1910
  -3.250   0.2049   0.01859   0.00936  -0.1218   0.5673   0.1927
  -3.000   0.2333   0.01848   0.00920  -0.1220   0.5628   0.1943
  -2.750   0.2616   0.01839   0.00906  -0.1222   0.5583   0.1958
  -2.500   0.2897   0.01831   0.00898  -0.1224   0.5527   0.1969
  -2.250   0.3177   0.01824   0.00887  -0.1225   0.5468   0.1979
  -2.000   0.3458   0.01819   0.00874  -0.1226   0.5412   0.1989
  -1.750   0.3738   0.01811   0.00865  -0.1228   0.5357   0.2002
  -1.500   0.4016   0.01802   0.00858  -0.1230   0.5297   0.2018
  -1.250   0.4297   0.01796   0.00851  -0.1232   0.5244   0.2035
  -1.000   0.4583   0.01793   0.00843  -0.1235   0.5202   0.2053
  -0.750   0.4872   0.01793   0.00839  -0.1238   0.5165   0.2075
  -0.500   0.5154   0.01791   0.00841  -0.1240   0.5126   0.2099
  -0.250   0.5436   0.01791   0.00842  -0.1242   0.5086   0.2129
   0.250   0.6004   0.01787   0.00839  -0.1247   0.5003   0.2234
   0.500   0.6294   0.01784   0.00836  -0.1251   0.4966   0.2350
   0.750   0.6582   0.01766   0.00844  -0.1258   0.4930   0.2795
   1.000   0.6855   0.01772   0.00874  -0.1259   0.4889   0.3321
   1.250   0.7126   0.01787   0.00893  -0.1258   0.4845   0.3517
   1.500   0.7397   0.01804   0.00906  -0.1257   0.4801   0.3639
   1.750   0.7671   0.01823   0.00923  -0.1256   0.4761   0.3725
   2.000   0.7948   0.01845   0.00937  -0.1256   0.4722   0.3811
   2.250   0.8198   0.01860   0.00959  -0.1252   0.4678   0.3869
   2.500   0.8447   0.01877   0.00982  -0.1247   0.4629   0.3926
   2.750   0.8697   0.01896   0.01000  -0.1243   0.4579   0.3992
   3.000   0.8952   0.01917   0.01013  -0.1239   0.4534   0.4047
   3.250   0.9195   0.01935   0.01033  -0.1234   0.4489   0.4086
   3.500   0.9419   0.01952   0.01059  -0.1227   0.4432   0.4124
   3.750   0.9640   0.01971   0.01081  -0.1218   0.4374   0.4162
   4.000   0.9857   0.01993   0.01098  -0.1209   0.4321   0.4199
   4.250   1.0045   0.02016   0.01125  -0.1195   0.4264   0.4240
   4.500   1.0221   0.02042   0.01153  -0.1180   0.4199   0.4276
   4.750   1.0400   0.02074   0.01180  -0.1167   0.4135   0.4302
   5.000   1.0589   0.02108   0.01221  -0.1156   0.4063   0.4333
   5.250   1.0766   0.02149   0.01265  -0.1144   0.3984   0.4366
   5.500   1.0938   0.02195   0.01313  -0.1132   0.3910   0.4403
   5.750   1.1102   0.02249   0.01369  -0.1120   0.3824   0.4442
   6.000   1.1248   0.02313   0.01429  -0.1106   0.3744   0.4483
   6.250   1.1394   0.02383   0.01498  -0.1094   0.3655   0.4524
   6.500   1.1518   0.02466   0.01575  -0.1079   0.3575   0.4559
   6.750   1.1655   0.02546   0.01659  -0.1068   0.3493   0.4598
   7.250   1.1904   0.02735   0.01849  -0.1044   0.3355   0.4666
   7.500   1.2022   0.02840   0.01953  -0.1033   0.3290   0.4701
   7.750   1.2133   0.02952   0.02063  -0.1021   0.3234   0.4741
   8.000   1.2266   0.03057   0.02170  -0.1012   0.3177   0.4788
   8.250   1.2381   0.03174   0.02287  -0.1002   0.3124   0.4836
   8.500   1.2494   0.03290   0.02403  -0.0992   0.3079   0.4894
   8.750   1.2630   0.03399   0.02520  -0.0985   0.3038   0.4962
   9.000   1.2759   0.03515   0.02641  -0.0977   0.2995   0.5031
   9.500   1.2981   0.03769   0.02898  -0.0960   0.2912   0.5172
   9.750   1.3105   0.03893   0.03028  -0.0954   0.2874   0.5257
  10.000   1.3221   0.04027   0.03171  -0.0947   0.2833   0.5349
  10.250   1.3327   0.04168   0.03319  -0.0940   0.2794   0.5457
  10.500   1.3433   0.04308   0.03461  -0.0933   0.2758   0.5587
  10.750   1.3548   0.04439   0.03593  -0.0926   0.2725   0.5736
  11.000   1.3653   0.04594   0.03763  -0.0921   0.2693   0.5911
  11.250   1.3758   0.04748   0.03930  -0.0916   0.2659   0.6116
  11.500   1.3856   0.04906   0.04098  -0.0910   0.2626   0.6337
  11.750   1.3947   0.05068   0.04268  -0.0904   0.2595   0.6572
  12.000   1.4054   0.05213   0.04416  -0.0898   0.2568   0.6820
  12.250   1.4155   0.05369   0.04581  -0.0892   0.2542   0.7062
  12.500   1.4237   0.05553   0.04778  -0.0887   0.2515   0.7282
  12.750   1.4321   0.05732   0.04967  -0.0882   0.2489   0.7486
  13.000   1.4404   0.05912   0.05154  -0.0877   0.2463   0.7682
  13.250   1.4485   0.06090   0.05337  -0.0872   0.2439   0.7879
  13.500   1.4579   0.06248   0.05499  -0.0867   0.2416   0.8095
  13.750   1.4678   0.06389   0.05645  -0.0859   0.2393   0.8384
  14.000   1.4657   0.06586   0.05866  -0.0846   0.2369   1.0000
  14.250   1.4709   0.06825   0.06113  -0.0845   0.2341   1.0000
  14.500   1.4753   0.07073   0.06365  -0.0845   0.2314   1.0000
  14.750   1.4817   0.07295   0.06589  -0.0844   0.2288   1.0000
  15.000   1.4903   0.07488   0.06779  -0.0843   0.2266   1.0000
  15.250   1.5021   0.07637   0.06922  -0.0841   0.2245   1.0000
  15.500   1.5024   0.07943   0.07241  -0.0843   0.2222   1.0000
  15.750   1.5038   0.08234   0.07541  -0.0844   0.2198   1.0000
  16.000   1.5058   0.08518   0.07832  -0.0846   0.2175   1.0000
  16.250   1.5097   0.08775   0.08094  -0.0847   0.2154   1.0000
  16.500   1.5154   0.09009   0.08330  -0.0849   0.2135   1.0000
  16.750   1.5247   0.09192   0.08512  -0.0849   0.2118   1.0000
  17.000   1.5383   0.09316   0.08631  -0.0849   0.2102   1.0000
  17.250   1.5331   0.09697   0.09027  -0.0854   0.2082   1.0000
  17.500   1.5271   0.10092   0.09435  -0.0860   0.2060   1.0000
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