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GOE 255 (MVA CA.6) AIRFOIL (goe255-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 255 (MVA CA.6) AIRFOIL (goe255-il)
Reynolds number: 500,000
Max Cl/Cd: 105.07 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe255-il-500000.txt
Download as CSV file: xf-goe255-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.5776   0.11408   0.11120  -0.0649   1.0000   0.0155
 -17.000  -0.6293   0.09985   0.09666  -0.0731   1.0000   0.0152
 -16.750  -0.6522   0.09179   0.08842  -0.0778   1.0000   0.0152
 -16.500  -0.6684   0.08525   0.08175  -0.0817   1.0000   0.0151
 -16.250  -0.6805   0.07975   0.07613  -0.0848   1.0000   0.0152
 -16.000  -0.6904   0.07487   0.07115  -0.0875   1.0000   0.0152
 -15.750  -0.6994   0.07045   0.06664  -0.0898   1.0000   0.0153
 -15.500  -0.7088   0.06648   0.06259  -0.0915   1.0000   0.0154
 -15.250  -0.7191   0.06289   0.05892  -0.0925   1.0000   0.0154
 -15.000  -0.7303   0.05962   0.05558  -0.0930   1.0000   0.0155
 -14.750  -0.7421   0.05656   0.05245  -0.0930   1.0000   0.0156
 -14.500  -0.7545   0.05369   0.04952  -0.0925   1.0000   0.0156
 -14.250  -0.7633   0.05075   0.04651  -0.0928   0.9996   0.0157
 -14.000  -0.7513   0.04698   0.04263  -0.0977   0.9967   0.0160
 -13.750  -0.7359   0.04338   0.03891  -0.1029   0.9940   0.0162
 -13.500  -0.7197   0.04008   0.03551  -0.1076   0.9901   0.0165
 -13.250  -0.7006   0.03696   0.03226  -0.1125   0.9861   0.0168
 -13.000  -0.6805   0.03409   0.02926  -0.1172   0.9813   0.0172
 -12.750  -0.6648   0.03164   0.02667  -0.1204   0.9721   0.0175
 -12.500  -0.6541   0.02956   0.02446  -0.1220   0.9593   0.0178
 -12.250  -0.6559   0.02721   0.02201  -0.1212   0.9427   0.0181
 -12.000  -0.6559   0.02554   0.02026  -0.1195   0.9222   0.0184
 -11.750  -0.6523   0.02433   0.01895  -0.1172   0.8971   0.0188
 -11.500  -0.6416   0.02324   0.01773  -0.1157   0.8726   0.0191
 -11.250  -0.6278   0.02230   0.01661  -0.1145   0.8526   0.0196
 -11.000  -0.6113   0.02146   0.01560  -0.1136   0.8375   0.0201
 -10.750  -0.5930   0.02069   0.01468  -0.1129   0.8260   0.0207
 -10.250  -0.5552   0.01903   0.01277  -0.1117   0.8086   0.0219
 -10.000  -0.5357   0.01819   0.01183  -0.1111   0.8016   0.0228
  -9.750  -0.5130   0.01758   0.01115  -0.1108   0.7953   0.0239
  -9.500  -0.4893   0.01706   0.01053  -0.1106   0.7891   0.0251
  -9.250  -0.4667   0.01640   0.00977  -0.1102   0.7836   0.0265
  -9.000  -0.4427   0.01580   0.00913  -0.1100   0.7782   0.0285
  -8.750  -0.4174   0.01535   0.00859  -0.1099   0.7728   0.0305
  -8.500  -0.3933   0.01473   0.00792  -0.1096   0.7677   0.0345
  -8.250  -0.3684   0.01414   0.00734  -0.1095   0.7629   0.0425
  -8.000  -0.3440   0.01345   0.00679  -0.1094   0.7577   0.0643
  -7.750  -0.3177   0.01307   0.00641  -0.1094   0.7526   0.0812
  -7.500  -0.2912   0.01270   0.00605  -0.1094   0.7478   0.0951
  -7.250  -0.2644   0.01232   0.00573  -0.1095   0.7424   0.1108
  -7.000  -0.2372   0.01201   0.00546  -0.1096   0.7372   0.1305
  -6.750  -0.2096   0.01178   0.00523  -0.1097   0.7323   0.1501
  -6.500  -0.1817   0.01153   0.00504  -0.1099   0.7271   0.1673
  -6.250  -0.1535   0.01134   0.00484  -0.1101   0.7217   0.1819
  -6.000  -0.1253   0.01120   0.00465  -0.1103   0.7166   0.1962
  -5.750  -0.0972   0.01098   0.00447  -0.1105   0.7112   0.2122
  -5.500  -0.0692   0.01075   0.00427  -0.1106   0.7054   0.2290
  -5.250  -0.0414   0.01055   0.00408  -0.1108   0.7000   0.2484
  -5.000  -0.0134   0.01032   0.00393  -0.1110   0.6938   0.2712
  -4.750   0.0147   0.01015   0.00384  -0.1111   0.6871   0.2992
  -4.500   0.0434   0.01011   0.00379  -0.1113   0.6806   0.3247
  -4.250   0.0722   0.01008   0.00376  -0.1115   0.6727   0.3421
  -4.000   0.1011   0.01013   0.00371  -0.1116   0.6655   0.3557
  -3.750   0.1301   0.01014   0.00371  -0.1118   0.6571   0.3673
  -3.500   0.1586   0.01018   0.00367  -0.1120   0.6498   0.3764
  -3.250   0.1877   0.01022   0.00366  -0.1122   0.6419   0.3847
  -3.000   0.2162   0.01024   0.00363  -0.1123   0.6350   0.3924
  -2.750   0.2451   0.01029   0.00364  -0.1126   0.6275   0.4005
  -2.500   0.2736   0.01032   0.00358  -0.1127   0.6203   0.4061
  -2.250   0.3022   0.01030   0.00355  -0.1129   0.6132   0.4109
  -2.000   0.3307   0.01033   0.00352  -0.1131   0.6061   0.4158
  -1.750   0.3593   0.01041   0.00350  -0.1133   0.6005   0.4205
  -1.500   0.3880   0.01036   0.00347  -0.1135   0.5951   0.4251
  -1.250   0.4165   0.01038   0.00346  -0.1137   0.5902   0.4293
  -1.000   0.4450   0.01045   0.00346  -0.1139   0.5860   0.4333
  -0.750   0.4740   0.01048   0.00347  -0.1142   0.5818   0.4372
  -0.500   0.5025   0.01047   0.00346  -0.1144   0.5777   0.4415
  -0.250   0.5309   0.01050   0.00348  -0.1147   0.5739   0.4458
   0.000   0.5593   0.01058   0.00351  -0.1149   0.5701   0.4505
   0.250   0.5881   0.01062   0.00354  -0.1151   0.5662   0.4554
   0.500   0.6163   0.01060   0.00357  -0.1153   0.5623   0.4610
   0.750   0.6447   0.01065   0.00361  -0.1156   0.5589   0.4665
   1.000   0.6732   0.01076   0.00367  -0.1158   0.5559   0.4720
   1.250   0.7015   0.01078   0.00373  -0.1161   0.5530   0.4780
   1.500   0.7299   0.01080   0.00380  -0.1163   0.5499   0.4839
   1.750   0.7582   0.01085   0.00386  -0.1165   0.5467   0.4893
   2.000   0.7862   0.01088   0.00393  -0.1167   0.5433   0.4955
   2.250   0.8142   0.01097   0.00401  -0.1169   0.5399   0.5030
   2.500   0.8424   0.01103   0.00411  -0.1172   0.5370   0.5119
   2.750   0.8702   0.01105   0.00421  -0.1174   0.5341   0.5241
   3.250   0.9251   0.01106   0.00444  -0.1176   0.5275   0.5709
   3.500   0.9519   0.01106   0.00458  -0.1176   0.5235   0.6217
   3.750   0.9772   0.01094   0.00475  -0.1173   0.5191   0.7047
   4.000   0.9978   0.01065   0.00491  -0.1157   0.5140   0.8315
   4.250   1.0304   0.01058   0.00502  -0.1166   0.5083   1.0000
   4.500   1.0564   0.01073   0.00515  -0.1164   0.5038   1.0000
   4.750   1.0821   0.01082   0.00527  -0.1162   0.4992   1.0000
   5.000   1.1076   0.01095   0.00539  -0.1159   0.4942   1.0000
   5.250   1.1326   0.01115   0.00554  -0.1156   0.4891   1.0000
   5.500   1.1573   0.01122   0.00568  -0.1152   0.4830   1.0000
   5.750   1.1808   0.01138   0.00582  -0.1145   0.4757   1.0000
   6.000   1.2044   0.01152   0.00598  -0.1139   0.4679   1.0000
   6.250   1.2260   0.01170   0.00614  -0.1130   0.4582   1.0000
   6.500   1.2472   0.01187   0.00632  -0.1119   0.4451   1.0000
   6.750   1.2632   0.01214   0.00654  -0.1099   0.4254   1.0000
   7.000   1.2710   0.01264   0.00690  -0.1064   0.3906   1.0000
   7.250   1.2738   0.01353   0.00757  -0.1024   0.3598   1.0000
   7.500   1.2820   0.01435   0.00827  -0.0994   0.3429   1.0000
   7.750   1.2935   0.01509   0.00894  -0.0972   0.3326   1.0000
   8.000   1.3075   0.01575   0.00958  -0.0953   0.3245   1.0000
   8.250   1.3208   0.01647   0.01027  -0.0935   0.3175   1.0000
   8.500   1.3364   0.01710   0.01091  -0.0921   0.3106   1.0000
   8.750   1.3475   0.01797   0.01174  -0.0901   0.3037   1.0000
   9.000   1.3656   0.01851   0.01234  -0.0891   0.2987   1.0000
   9.250   1.3808   0.01922   0.01306  -0.0878   0.2932   1.0000
   9.500   1.3916   0.02021   0.01403  -0.0861   0.2873   1.0000
   9.750   1.4100   0.02080   0.01468  -0.0853   0.2813   1.0000
  10.000   1.4226   0.02175   0.01563  -0.0840   0.2742   1.0000
  10.250   1.4368   0.02265   0.01656  -0.0829   0.2663   1.0000
  10.500   1.4488   0.02373   0.01764  -0.0817   0.2575   1.0000
  10.750   1.4625   0.02474   0.01867  -0.0808   0.2479   1.0000
  11.000   1.4718   0.02608   0.02000  -0.0795   0.2354   1.0000
  11.250   1.4769   0.02780   0.02164  -0.0780   0.2151   1.0000
  11.500   1.4697   0.03051   0.02418  -0.0757   0.1849   1.0000
  11.750   1.4576   0.03370   0.02719  -0.0732   0.1604   1.0000
  12.000   1.4497   0.03665   0.03005  -0.0711   0.1434   1.0000
  12.250   1.4445   0.03944   0.03277  -0.0694   0.1270   1.0000
  12.500   1.4354   0.04266   0.03587  -0.0676   0.1034   1.0000
  12.750   1.4190   0.04668   0.03971  -0.0656   0.0776   1.0000
  13.000   1.4069   0.05045   0.04339  -0.0641   0.0587   1.0000
  13.500   1.3756   0.05920   0.05201  -0.0615   0.0200   1.0000
  13.750   1.3769   0.06196   0.05484  -0.0610   0.0184   1.0000
  14.000   1.3788   0.06469   0.05766  -0.0606   0.0176   1.0000
  14.250   1.3798   0.06757   0.06062  -0.0602   0.0169   1.0000
  14.500   1.3790   0.07067   0.06382  -0.0599   0.0162   1.0000
  14.750   1.3761   0.07407   0.06731  -0.0596   0.0155   1.0000
  15.000   1.3770   0.07706   0.07039  -0.0595   0.0152   1.0000
  15.250   1.3769   0.08018   0.07361  -0.0594   0.0148   1.0000
  15.500   1.3748   0.08363   0.07715  -0.0594   0.0145   1.0000
  15.750   1.3716   0.08722   0.08084  -0.0595   0.0142   1.0000
  16.000   1.3675   0.09097   0.08469  -0.0596   0.0139   1.0000
  16.250   1.3616   0.09503   0.08884  -0.0599   0.0137   1.0000
  16.500   1.3543   0.09935   0.09325  -0.0603   0.0135   1.0000
  16.750   1.3465   0.10379   0.09780  -0.0609   0.0133   1.0000
  17.000   1.3366   0.10860   0.10271  -0.0617   0.0131   1.0000
  17.250   1.3247   0.11379   0.10801  -0.0627   0.0129   1.0000
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