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GOE 255 (MVA CA.6) AIRFOIL (goe255-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 255 (MVA CA.6) AIRFOIL (goe255-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.2 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe255-il-1000000.txt
Download as CSV file: xf-goe255-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.6547   0.13828   0.13592  -0.0476   1.0000   0.0099
 -19.250  -0.6688   0.13132   0.12887  -0.0515   1.0000   0.0099
 -19.000  -0.6796   0.12516   0.12263  -0.0549   1.0000   0.0100
 -18.750  -0.6894   0.11933   0.11672  -0.0581   1.0000   0.0100
 -18.500  -0.6996   0.11355   0.11086  -0.0613   1.0000   0.0100
 -18.250  -0.7086   0.10805   0.10529  -0.0643   1.0000   0.0101
 -18.000  -0.7164   0.10287   0.10004  -0.0671   1.0000   0.0101
 -17.750  -0.7249   0.09767   0.09476  -0.0699   1.0000   0.0102
 -17.500  -0.7331   0.09254   0.08957  -0.0727   1.0000   0.0102
 -17.250  -0.7407   0.08759   0.08454  -0.0754   1.0000   0.0103
 -17.000  -0.7480   0.08280   0.07968  -0.0780   1.0000   0.0103
 -16.750  -0.7550   0.07812   0.07493  -0.0806   1.0000   0.0104
 -16.500  -0.7619   0.07359   0.07032  -0.0831   1.0000   0.0105
 -16.250  -0.7689   0.06920   0.06587  -0.0854   1.0000   0.0105
 -16.000  -0.7767   0.06499   0.06158  -0.0875   1.0000   0.0106
 -15.750  -0.7872   0.06104   0.05756  -0.0890   1.0000   0.0106
 -15.500  -0.7982   0.05719   0.05364  -0.0904   0.9994   0.0107
 -15.250  -0.7984   0.05286   0.04922  -0.0943   0.9970   0.0108
 -15.000  -0.7964   0.04867   0.04495  -0.0985   0.9943   0.0109
 -14.750  -0.7951   0.04475   0.04094  -0.1021   0.9893   0.0110
 -14.500  -0.7918   0.04100   0.03710  -0.1056   0.9834   0.0111
 -14.250  -0.7921   0.03760   0.03360  -0.1078   0.9747   0.0112
 -14.000  -0.7922   0.03442   0.03032  -0.1095   0.9657   0.0113
 -13.750  -0.7919   0.03143   0.02722  -0.1109   0.9556   0.0114
 -13.500  -0.7873   0.02862   0.02429  -0.1129   0.9447   0.0115
 -13.250  -0.7814   0.02613   0.02168  -0.1147   0.9308   0.0116
 -13.000  -0.7754   0.02431   0.01972  -0.1151   0.9080   0.0117
 -12.750  -0.7825   0.02257   0.01766  -0.1125   0.8513   0.0119
 -12.500  -0.7764   0.02117   0.01601  -0.1113   0.8222   0.0122
 -12.250  -0.7616   0.02022   0.01492  -0.1105   0.8069   0.0124
 -12.000  -0.7431   0.01948   0.01407  -0.1100   0.7964   0.0127
 -11.750  -0.7226   0.01882   0.01334  -0.1096   0.7881   0.0130
 -11.500  -0.7010   0.01824   0.01267  -0.1093   0.7813   0.0134
 -11.250  -0.6783   0.01768   0.01204  -0.1091   0.7751   0.0138
 -11.000  -0.6549   0.01720   0.01147  -0.1088   0.7692   0.0142
 -10.750  -0.6305   0.01676   0.01096  -0.1087   0.7642   0.0145
 -10.500  -0.6092   0.01594   0.01005  -0.1083   0.7592   0.0150
 -10.250  -0.5860   0.01531   0.00936  -0.1080   0.7543   0.0156
 -10.000  -0.5611   0.01488   0.00885  -0.1079   0.7495   0.0162
  -9.750  -0.5353   0.01444   0.00838  -0.1079   0.7456   0.0168
  -9.500  -0.5090   0.01407   0.00794  -0.1078   0.7411   0.0174
  -9.250  -0.4833   0.01364   0.00744  -0.1078   0.7365   0.0182
  -9.000  -0.4577   0.01319   0.00694  -0.1077   0.7320   0.0194
  -8.750  -0.4306   0.01283   0.00655  -0.1077   0.7281   0.0206
  -8.500  -0.4036   0.01248   0.00616  -0.1078   0.7237   0.0223
  -8.250  -0.3768   0.01212   0.00577  -0.1078   0.7193   0.0249
  -8.000  -0.3501   0.01174   0.00537  -0.1078   0.7151   0.0299
  -7.750  -0.3238   0.01120   0.00493  -0.1079   0.7113   0.0458
  -7.500  -0.2968   0.01077   0.00460  -0.1080   0.7069   0.0644
  -7.250  -0.2691   0.01051   0.00434  -0.1082   0.7023   0.0758
  -7.000  -0.2410   0.01027   0.00411  -0.1084   0.6980   0.0860
  -6.750  -0.2128   0.00998   0.00387  -0.1086   0.6936   0.0990
  -6.500  -0.1848   0.00970   0.00365  -0.1088   0.6886   0.1180
  -6.250  -0.1568   0.00946   0.00346  -0.1090   0.6836   0.1388
  -6.000  -0.1280   0.00925   0.00331  -0.1093   0.6786   0.1558
  -5.750  -0.0992   0.00909   0.00316  -0.1096   0.6722   0.1698
  -5.500  -0.0706   0.00897   0.00303  -0.1098   0.6657   0.1832
  -5.250  -0.0415   0.00883   0.00291  -0.1102   0.6587   0.1957
  -5.000  -0.0130   0.00871   0.00278  -0.1104   0.6507   0.2090
  -4.750   0.0159   0.00855   0.00265  -0.1107   0.6424   0.2247
  -4.500   0.0441   0.00841   0.00252  -0.1109   0.6338   0.2437
  -4.250   0.0727   0.00821   0.00240  -0.1112   0.6250   0.2707
  -4.000   0.1010   0.00809   0.00234  -0.1114   0.6155   0.3045
  -3.750   0.1297   0.00806   0.00232  -0.1116   0.6046   0.3261
  -3.500   0.1587   0.00808   0.00231  -0.1119   0.5941   0.3401
  -3.250   0.1875   0.00813   0.00231  -0.1121   0.5844   0.3517
  -3.000   0.2165   0.00816   0.00231  -0.1123   0.5760   0.3602
  -2.750   0.2454   0.00823   0.00232  -0.1126   0.5686   0.3666
  -2.500   0.2746   0.00828   0.00232  -0.1129   0.5622   0.3720
  -2.250   0.3033   0.00833   0.00235  -0.1131   0.5567   0.3793
  -2.000   0.3326   0.00840   0.00237  -0.1134   0.5523   0.3846
  -1.750   0.3619   0.00844   0.00238  -0.1137   0.5483   0.3875
  -1.500   0.3907   0.00845   0.00237  -0.1140   0.5442   0.3918
  -1.250   0.4194   0.00850   0.00240  -0.1142   0.5401   0.3953
  -1.000   0.4484   0.00855   0.00242  -0.1145   0.5367   0.3990
  -0.750   0.4778   0.00858   0.00244  -0.1149   0.5339   0.4022
  -0.500   0.5070   0.00863   0.00246  -0.1152   0.5311   0.4045
  -0.250   0.5357   0.00864   0.00247  -0.1155   0.5281   0.4082
   0.000   0.5641   0.00869   0.00251  -0.1157   0.5248   0.4114
   0.250   0.5926   0.00876   0.00256  -0.1159   0.5217   0.4154
   0.500   0.6219   0.00879   0.00260  -0.1163   0.5198   0.4189
   0.750   0.6510   0.00882   0.00263  -0.1166   0.5175   0.4220
   1.000   0.6798   0.00882   0.00266  -0.1169   0.5151   0.4267
   1.250   0.7084   0.00886   0.00271  -0.1172   0.5125   0.4305
   1.500   0.7367   0.00893   0.00277  -0.1174   0.5097   0.4346
   1.750   0.7646   0.00903   0.00285  -0.1176   0.5065   0.4388
   2.000   0.7933   0.00903   0.00290  -0.1179   0.5041   0.4443
   2.250   0.8221   0.00905   0.00295  -0.1182   0.5014   0.4486
   2.500   0.8506   0.00908   0.00300  -0.1184   0.4982   0.4527
   2.750   0.8784   0.00915   0.00307  -0.1186   0.4940   0.4572
   3.000   0.9053   0.00924   0.00316  -0.1186   0.4891   0.4635
   3.250   0.9341   0.00924   0.00322  -0.1189   0.4857   0.4705
   3.500   0.9622   0.00926   0.00329  -0.1191   0.4818   0.4802
   3.750   0.9895   0.00931   0.00338  -0.1192   0.4774   0.4941
   4.000   1.0161   0.00937   0.00350  -0.1192   0.4729   0.5176
   4.250   1.0443   0.00931   0.00359  -0.1195   0.4684   0.5599
   4.500   1.0710   0.00926   0.00372  -0.1195   0.4618   0.6238
   4.750   1.0967   0.00920   0.00387  -0.1194   0.4545   0.7046
   5.000   1.1204   0.00910   0.00403  -0.1187   0.4429   0.8077
   5.250   1.1435   0.00899   0.00421  -0.1177   0.4253   1.0000
   5.500   1.1597   0.00954   0.00452  -0.1158   0.3774   1.0000
   5.750   1.1721   0.01026   0.00500  -0.1132   0.3417   1.0000
   6.000   1.1895   0.01070   0.00536  -0.1116   0.3276   1.0000
   6.250   1.2061   0.01110   0.00571  -0.1097   0.3177   1.0000
   6.500   1.2251   0.01144   0.00601  -0.1083   0.3108   1.0000
   6.750   1.2421   0.01187   0.00640  -0.1067   0.3031   1.0000
   7.000   1.2640   0.01212   0.00667  -0.1059   0.2987   1.0000
   7.250   1.2833   0.01249   0.00702  -0.1047   0.2929   1.0000
   7.500   1.3007   0.01295   0.00745  -0.1032   0.2868   1.0000
   7.750   1.3235   0.01319   0.00771  -0.1027   0.2834   1.0000
   8.000   1.3436   0.01355   0.00807  -0.1017   0.2782   1.0000
   8.250   1.3613   0.01402   0.00852  -0.1004   0.2728   1.0000
   8.500   1.3821   0.01437   0.00888  -0.0996   0.2681   1.0000
   8.750   1.4015   0.01478   0.00930  -0.0987   0.2617   1.0000
   9.000   1.4178   0.01535   0.00984  -0.0973   0.2546   1.0000
   9.250   1.4369   0.01580   0.01029  -0.0964   0.2466   1.0000
   9.500   1.4516   0.01649   0.01093  -0.0949   0.2346   1.0000
   9.750   1.4583   0.01762   0.01193  -0.0924   0.2109   1.0000
  10.000   1.4514   0.01964   0.01372  -0.0885   0.1739   1.0000
  10.250   1.4474   0.02167   0.01562  -0.0854   0.1517   1.0000
  10.500   1.4476   0.02359   0.01746  -0.0830   0.1341   1.0000
  10.750   1.4426   0.02598   0.01971  -0.0804   0.1104   1.0000
  11.000   1.4263   0.02935   0.02287  -0.0771   0.0777   1.0000
  11.250   1.4130   0.03263   0.02602  -0.0743   0.0530   1.0000
  11.500   1.3900   0.03691   0.03017  -0.0711   0.0184   1.0000
  11.750   1.3945   0.03892   0.03221  -0.0700   0.0154   1.0000
  12.000   1.4014   0.04077   0.03411  -0.0691   0.0145   1.0000
  12.250   1.4070   0.04276   0.03616  -0.0682   0.0137   1.0000
  12.500   1.4111   0.04493   0.03839  -0.0673   0.0129   1.0000
  12.750   1.4171   0.04696   0.04047  -0.0666   0.0124   1.0000
  13.000   1.4231   0.04902   0.04259  -0.0659   0.0120   1.0000
  13.250   1.4282   0.05119   0.04482  -0.0652   0.0116   1.0000
  13.500   1.4319   0.05357   0.04725  -0.0646   0.0112   1.0000
  13.750   1.4345   0.05609   0.04984  -0.0640   0.0109   1.0000
  14.000   1.4346   0.05892   0.05274  -0.0634   0.0105   1.0000
  14.250   1.4327   0.06201   0.05591  -0.0628   0.0102   1.0000
  14.500   1.4364   0.06455   0.05851  -0.0625   0.0101   1.0000
  14.750   1.4394   0.06717   0.06119  -0.0622   0.0099   1.0000
  15.000   1.4414   0.06994   0.06404  -0.0620   0.0097   1.0000
  15.250   1.4420   0.07290   0.06707  -0.0618   0.0095   1.0000
  15.500   1.4423   0.07591   0.07014  -0.0616   0.0093   1.0000
  15.750   1.4419   0.07903   0.07334  -0.0615   0.0091   1.0000
  16.000   1.4403   0.08235   0.07672  -0.0615   0.0088   1.0000
  16.250   1.4387   0.08570   0.08014  -0.0615   0.0087   1.0000
  16.500   1.4339   0.08948   0.08400  -0.0616   0.0085   1.0000
  16.750   1.4262   0.09367   0.08828  -0.0619   0.0083   1.0000
  17.000   1.4146   0.09849   0.09321  -0.0622   0.0082   1.0000
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