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GOE 255 (MVA CA.6) AIRFOIL (goe255-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 255 (MVA CA.6) AIRFOIL (goe255-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.84 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe255-il-1000000-n5.txt
Download as CSV file: xf-goe255-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 255 (MVA CA.6) 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.7588   0.08449   0.08127  -0.0780   0.9851   0.0063
 -17.000  -0.7744   0.07822   0.07490  -0.0817   0.9805   0.0064
 -16.750  -0.7904   0.07218   0.06875  -0.0850   0.9753   0.0064
 -16.500  -0.8061   0.06647   0.06293  -0.0881   0.9702   0.0064
 -16.250  -0.8231   0.06112   0.05747  -0.0907   0.9637   0.0064
 -16.000  -0.8400   0.05604   0.05228  -0.0931   0.9579   0.0064
 -15.750  -0.8550   0.05123   0.04736  -0.0955   0.9513   0.0065
 -15.500  -0.8686   0.04672   0.04274  -0.0976   0.9442   0.0065
 -15.250  -0.8794   0.04239   0.03830  -0.0998   0.9335   0.0065
 -15.000  -0.8864   0.03829   0.03408  -0.1022   0.9205   0.0066
 -14.750  -0.8924   0.03453   0.03009  -0.1040   0.8726   0.0066
 -14.500  -0.8924   0.03115   0.02635  -0.1066   0.8180   0.0067
 -14.250  -0.8866   0.02804   0.02304  -0.1098   0.7989   0.0068
 -14.000  -0.8798   0.02549   0.02033  -0.1124   0.7868   0.0069
 -13.500  -0.8647   0.02278   0.01738  -0.1116   0.7686   0.0071
 -13.250  -0.8497   0.02187   0.01637  -0.1111   0.7612   0.0072
 -13.000  -0.8324   0.02106   0.01548  -0.1107   0.7553   0.0074
 -12.750  -0.8136   0.02032   0.01465  -0.1103   0.7493   0.0075
 -12.250  -0.7723   0.01905   0.01321  -0.1096   0.7376   0.0078
 -12.000  -0.7502   0.01849   0.01258  -0.1093   0.7320   0.0079
 -11.750  -0.7285   0.01786   0.01186  -0.1090   0.7270   0.0081
 -11.500  -0.7060   0.01724   0.01119  -0.1087   0.7229   0.0084
 -11.250  -0.6822   0.01672   0.01062  -0.1086   0.7186   0.0087
 -11.000  -0.6578   0.01627   0.01012  -0.1084   0.7143   0.0091
 -10.750  -0.6329   0.01586   0.00965  -0.1083   0.7103   0.0094
 -10.500  -0.6074   0.01546   0.00920  -0.1083   0.7069   0.0097
 -10.250  -0.5815   0.01507   0.00877  -0.1083   0.7032   0.0101
 -10.000  -0.5554   0.01472   0.00836  -0.1083   0.6991   0.0104
  -9.750  -0.5296   0.01432   0.00790  -0.1082   0.6951   0.0108
  -9.500  -0.5035   0.01394   0.00747  -0.1082   0.6914   0.0113
  -9.250  -0.4767   0.01359   0.00709  -0.1083   0.6877   0.0119
  -9.000  -0.4497   0.01328   0.00674  -0.1084   0.6834   0.0125
  -8.750  -0.4224   0.01301   0.00642  -0.1085   0.6789   0.0131
  -8.500  -0.3952   0.01273   0.00609  -0.1086   0.6749   0.0140
  -8.250  -0.3678   0.01241   0.00576  -0.1087   0.6705   0.0152
  -8.000  -0.3401   0.01215   0.00546  -0.1088   0.6655   0.0165
  -7.750  -0.3126   0.01190   0.00516  -0.1089   0.6603   0.0186
  -7.500  -0.2848   0.01161   0.00487  -0.1091   0.6552   0.0220
  -7.250  -0.2575   0.01128   0.00456  -0.1092   0.6487   0.0306
  -7.000  -0.2304   0.01094   0.00425  -0.1093   0.6424   0.0444
  -6.750  -0.2028   0.01062   0.00399  -0.1095   0.6350   0.0586
  -6.500  -0.1749   0.01041   0.00377  -0.1097   0.6275   0.0687
  -6.250  -0.1464   0.01026   0.00360  -0.1099   0.6191   0.0757
  -6.000  -0.1184   0.01008   0.00341  -0.1101   0.6083   0.0850
  -5.500  -0.0636   0.00968   0.00304  -0.1103   0.5794   0.1251
  -5.250  -0.0357   0.00953   0.00291  -0.1105   0.5681   0.1451
  -5.000  -0.0074   0.00942   0.00280  -0.1108   0.5600   0.1608
  -4.750   0.0211   0.00935   0.00272  -0.1110   0.5518   0.1727
  -4.500   0.0496   0.00925   0.00263  -0.1112   0.5452   0.1863
  -4.250   0.0783   0.00919   0.00255  -0.1115   0.5387   0.1956
  -3.750   0.1359   0.00908   0.00242  -0.1120   0.5290   0.2149
  -3.500   0.1648   0.00900   0.00235  -0.1123   0.5254   0.2266
  -3.250   0.1936   0.00893   0.00229  -0.1126   0.5219   0.2411
  -2.750   0.2504   0.00867   0.00222  -0.1132   0.5150   0.3077
  -2.500   0.2796   0.00864   0.00223  -0.1135   0.5122   0.3269
  -2.250   0.3089   0.00864   0.00223  -0.1139   0.5097   0.3362
  -2.000   0.3381   0.00866   0.00224  -0.1142   0.5072   0.3453
  -1.750   0.3672   0.00867   0.00225  -0.1145   0.5047   0.3530
  -1.500   0.3961   0.00871   0.00227  -0.1148   0.5023   0.3594
  -1.250   0.4251   0.00877   0.00229  -0.1151   0.4996   0.3631
  -1.000   0.4544   0.00877   0.00230  -0.1154   0.4975   0.3667
  -0.750   0.4836   0.00878   0.00232  -0.1158   0.4949   0.3702
  -0.500   0.5127   0.00881   0.00234  -0.1161   0.4925   0.3735
  -0.250   0.5416   0.00886   0.00237  -0.1164   0.4899   0.3769
   0.000   0.5703   0.00891   0.00240  -0.1167   0.4871   0.3802
   0.250   0.5987   0.00896   0.00245  -0.1169   0.4842   0.3843
   0.500   0.6276   0.00899   0.00249  -0.1172   0.4819   0.3877
   0.750   0.6566   0.00902   0.00252  -0.1175   0.4799   0.3911
   1.000   0.6855   0.00906   0.00257  -0.1178   0.4775   0.3947
   1.250   0.7142   0.00910   0.00261  -0.1181   0.4747   0.3980
   1.500   0.7424   0.00915   0.00267  -0.1183   0.4710   0.4014
   1.750   0.7702   0.00922   0.00274  -0.1185   0.4674   0.4056
   2.000   0.7988   0.00926   0.00279  -0.1188   0.4644   0.4094
   2.250   0.8272   0.00932   0.00285  -0.1190   0.4594   0.4117
   2.500   0.8545   0.00941   0.00292  -0.1191   0.4528   0.4143
   2.750   0.8823   0.00947   0.00299  -0.1192   0.4472   0.4178
   3.000   0.9098   0.00955   0.00307  -0.1193   0.4396   0.4211
   3.250   0.9364   0.00967   0.00317  -0.1193   0.4288   0.4243
   3.500   0.9561   0.01014   0.00341  -0.1180   0.3800   0.4273
   4.000   0.9917   0.01124   0.00416  -0.1149   0.3156   0.4344
   4.250   1.0156   0.01145   0.00437  -0.1144   0.3083   0.4392
   4.500   1.0395   0.01165   0.00456  -0.1138   0.3030   0.4444
   4.750   1.0629   0.01185   0.00477  -0.1133   0.2983   0.4506
   5.000   1.0872   0.01200   0.00496  -0.1128   0.2954   0.4589
   5.250   1.1107   0.01213   0.00514  -0.1122   0.2930   0.4689
   5.500   1.1321   0.01227   0.00533  -0.1112   0.2905   0.4836
   5.750   1.1532   0.01241   0.00555  -0.1102   0.2879   0.5082
   6.000   1.1749   0.01258   0.00583  -0.1094   0.2848   0.5466
   6.250   1.1960   0.01281   0.00616  -0.1085   0.2796   0.5935
   6.500   1.2188   0.01296   0.00646  -0.1080   0.2739   0.6456
   6.750   1.2393   0.01319   0.00683  -0.1071   0.2674   0.7072
   7.000   1.2601   0.01334   0.00720  -0.1062   0.2623   0.7896
   7.250   1.2754   0.01324   0.00750  -0.1039   0.2583   1.0000
   7.500   1.2947   0.01364   0.00787  -0.1028   0.2519   1.0000
   7.750   1.3134   0.01407   0.00827  -0.1016   0.2432   1.0000
   8.000   1.3299   0.01461   0.00876  -0.1002   0.2326   1.0000
   8.250   1.3439   0.01529   0.00936  -0.0985   0.2159   1.0000
   8.500   1.3444   0.01668   0.01054  -0.0949   0.1805   1.0000
   8.750   1.3460   0.01810   0.01183  -0.0918   0.1573   1.0000
   9.000   1.3542   0.01926   0.01293  -0.0897   0.1446   1.0000
   9.250   1.3632   0.02043   0.01406  -0.0879   0.1342   1.0000
   9.500   1.3699   0.02181   0.01539  -0.0859   0.1204   1.0000
   9.750   1.3632   0.02424   0.01763  -0.0829   0.0896   1.0000
  10.000   1.3599   0.02655   0.01984  -0.0805   0.0692   1.0000
  10.250   1.3440   0.02995   0.02308  -0.0772   0.0348   1.0000
  10.500   1.3398   0.03254   0.02563  -0.0751   0.0146   1.0000
  10.750   1.3493   0.03407   0.02719  -0.0742   0.0126   1.0000
  11.000   1.3596   0.03555   0.02871  -0.0734   0.0116   1.0000
  11.250   1.3689   0.03712   0.03032  -0.0725   0.0108   1.0000
  11.500   1.3769   0.03884   0.03208  -0.0716   0.0100   1.0000
  11.750   1.3865   0.04043   0.03371  -0.0709   0.0097   1.0000
  12.000   1.3951   0.04214   0.03547  -0.0702   0.0092   1.0000
  12.250   1.4030   0.04395   0.03732  -0.0695   0.0087   1.0000
  12.500   1.4102   0.04583   0.03924  -0.0688   0.0083   1.0000
  12.750   1.4159   0.04790   0.04135  -0.0681   0.0079   1.0000
  13.000   1.4219   0.04996   0.04347  -0.0674   0.0076   1.0000
  13.250   1.4287   0.05200   0.04555  -0.0669   0.0074   1.0000
  13.500   1.4348   0.05413   0.04774  -0.0664   0.0071   1.0000
  13.750   1.4408   0.05629   0.04994  -0.0659   0.0069   1.0000
  14.000   1.4455   0.05860   0.05231  -0.0655   0.0067   1.0000
  14.250   1.4500   0.06096   0.05472  -0.0651   0.0064   1.0000
  14.500   1.4542   0.06340   0.05721  -0.0647   0.0062   1.0000
  14.750   1.4569   0.06604   0.05990  -0.0644   0.0060   1.0000
  15.000   1.4588   0.06878   0.06271  -0.0641   0.0058   1.0000
  15.250   1.4607   0.07154   0.06552  -0.0639   0.0056   1.0000
  15.500   1.4632   0.07425   0.06829  -0.0637   0.0055   1.0000
  15.750   1.4661   0.07693   0.07103  -0.0636   0.0054   1.0000
  16.000   1.4670   0.07990   0.07406  -0.0635   0.0052   1.0000
  16.250   1.4687   0.08275   0.07698  -0.0635   0.0051   1.0000
  16.500   1.4683   0.08591   0.08021  -0.0635   0.0050   1.0000
  16.750   1.4687   0.08895   0.08331  -0.0636   0.0049   1.0000
  17.000   1.4677   0.09222   0.08665  -0.0638   0.0048   1.0000
  17.250   1.4666   0.09552   0.09002  -0.0640   0.0047   1.0000
  17.500   1.4648   0.09896   0.09353  -0.0643   0.0046   1.0000
  17.750   1.4621   0.10255   0.09719  -0.0647   0.0045   1.0000
  18.000   1.4593   0.10616   0.10086  -0.0652   0.0044   1.0000
  18.250   1.4541   0.11015   0.10493  -0.0658   0.0043   1.0000
  18.500   1.4486   0.11423   0.10909  -0.0665   0.0042   1.0000
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