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GOE 547 AIRFOIL (goe547-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 547 AIRFOIL (goe547-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.69 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe547-il-1000000-n5.txt
Download as CSV file: xf-goe547-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 547 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -1.0109   0.03538   0.03284  -0.1011   0.9979   0.0072
 -14.250  -1.0061   0.03089   0.02809  -0.1065   0.9939   0.0073
 -14.000  -0.9941   0.02827   0.02528  -0.1084   0.9905   0.0076
 -13.750  -0.9760   0.02621   0.02303  -0.1100   0.9879   0.0078
 -13.500  -0.9537   0.02451   0.02115  -0.1117   0.9862   0.0081
 -13.250  -0.9357   0.02289   0.01940  -0.1121   0.9830   0.0086
 -13.000  -0.9150   0.02159   0.01797  -0.1125   0.9796   0.0091
 -12.750  -0.8907   0.02043   0.01670  -0.1133   0.9775   0.0098
 -12.500  -0.8641   0.01941   0.01556  -0.1143   0.9759   0.0104
 -12.250  -0.8435   0.01857   0.01461  -0.1138   0.9716   0.0108
 -12.000  -0.8189   0.01785   0.01383  -0.1140   0.9680   0.0117
 -11.750  -0.7911   0.01726   0.01320  -0.1147   0.9657   0.0128
 -11.500  -0.7618   0.01667   0.01254  -0.1156   0.9641   0.0137
 -11.250  -0.7402   0.01612   0.01191  -0.1149   0.9576   0.0143
 -11.000  -0.7089   0.01592   0.01173  -0.1159   0.9545   0.0154
 -10.500  -0.6414   0.01548   0.01124  -0.1190   0.9471   0.0172
 -10.250  -0.6062   0.01509   0.01078  -0.1210   0.9416   0.0179
 -10.000  -0.5692   0.01467   0.01027  -0.1233   0.9363   0.0185
  -9.750  -0.5355   0.01443   0.00995  -0.1248   0.9286   0.0188
  -9.500  -0.5041   0.01385   0.00928  -0.1262   0.9215   0.0196
  -9.250  -0.4751   0.01358   0.00895  -0.1267   0.9137   0.0201
  -9.000  -0.4460   0.01333   0.00864  -0.1273   0.9066   0.0206
  -8.750  -0.4190   0.01315   0.00840  -0.1273   0.8990   0.0211
  -8.500  -0.3917   0.01295   0.00813  -0.1273   0.8922   0.0217
  -8.250  -0.3660   0.01274   0.00787  -0.1271   0.8856   0.0223
  -8.000  -0.3400   0.01251   0.00756  -0.1269   0.8793   0.0229
  -7.750  -0.3149   0.01220   0.00716  -0.1265   0.8732   0.0233
  -7.500  -0.2892   0.01198   0.00687  -0.1262   0.8668   0.0238
  -7.250  -0.2639   0.01168   0.00649  -0.1258   0.8612   0.0241
  -7.000  -0.2385   0.01142   0.00617  -0.1254   0.8556   0.0244
  -6.750  -0.2129   0.01118   0.00586  -0.1250   0.8500   0.0246
  -6.500  -0.1875   0.01090   0.00551  -0.1246   0.8448   0.0248
  -6.250  -0.1621   0.01063   0.00518  -0.1242   0.8388   0.0249
  -5.750  -0.1124   0.00991   0.00431  -0.1232   0.8280   0.0253
  -5.500  -0.0881   0.00948   0.00378  -0.1225   0.8225   0.0258
  -5.250  -0.0630   0.00916   0.00339  -0.1220   0.8173   0.0266
  -5.000  -0.0373   0.00890   0.00310  -0.1216   0.8117   0.0274
  -4.750  -0.0115   0.00871   0.00286  -0.1212   0.8057   0.0279
  -4.500   0.0147   0.00854   0.00264  -0.1209   0.8001   0.0284
  -4.250   0.0410   0.00838   0.00245  -0.1205   0.7943   0.0288
  -3.750   0.0936   0.00811   0.00210  -0.1199   0.7825   0.0298
  -3.500   0.1198   0.00800   0.00195  -0.1195   0.7757   0.0302
  -3.250   0.1463   0.00790   0.00181  -0.1192   0.7694   0.0306
  -3.000   0.1727   0.00780   0.00168  -0.1188   0.7626   0.0311
  -2.750   0.1991   0.00773   0.00156  -0.1185   0.7558   0.0315
  -2.500   0.2255   0.00765   0.00146  -0.1182   0.7481   0.0320
  -2.250   0.2518   0.00760   0.00137  -0.1178   0.7408   0.0324
  -2.000   0.2783   0.00755   0.00129  -0.1174   0.7327   0.0330
  -1.750   0.3045   0.00749   0.00121  -0.1170   0.7248   0.0358
  -1.500   0.3296   0.00745   0.00115  -0.1164   0.7121   0.0416
  -1.250   0.3542   0.00738   0.00112  -0.1157   0.6978   0.0665
  -1.000   0.3793   0.00737   0.00109  -0.1151   0.6841   0.0746
  -0.750   0.4048   0.00739   0.00106  -0.1146   0.6712   0.0787
  -0.500   0.4302   0.00739   0.00104  -0.1140   0.6590   0.0857
  -0.250   0.4551   0.00741   0.00103  -0.1134   0.6451   0.0954
   0.000   0.4784   0.00720   0.00104  -0.1126   0.6314   0.1882
   0.250   0.5031   0.00721   0.00106  -0.1119   0.6178   0.2120
   0.500   0.5281   0.00722   0.00108  -0.1113   0.6062   0.2319
   0.750   0.5526   0.00720   0.00112  -0.1106   0.5937   0.2690
   1.000   0.5777   0.00716   0.00116  -0.1101   0.5824   0.3076
   1.250   0.6026   0.00709   0.00121  -0.1096   0.5737   0.3615
   1.500   0.6263   0.00697   0.00129  -0.1088   0.5642   0.4497
   1.750   0.6513   0.00692   0.00136  -0.1082   0.5544   0.4986
   2.000   0.6759   0.00695   0.00143  -0.1076   0.5427   0.5309
   2.250   0.7001   0.00699   0.00151  -0.1068   0.5282   0.5598
   2.500   0.7213   0.00716   0.00163  -0.1055   0.4950   0.5916
   2.750   0.7415   0.00733   0.00177  -0.1039   0.4613   0.6376
   3.000   0.7602   0.00747   0.00194  -0.1021   0.4260   0.7010
   3.500   0.8386   0.00801   0.00263  -0.1080   0.3183   1.0000
   3.750   0.8580   0.00832   0.00282  -0.1063   0.2916   1.0000
   4.000   0.8770   0.00866   0.00302  -0.1046   0.2637   1.0000
   4.250   0.8962   0.00900   0.00323  -0.1029   0.2369   1.0000
   4.500   0.9159   0.00930   0.00343  -0.1013   0.2152   1.0000
   4.750   0.9354   0.00962   0.00364  -0.0997   0.1925   1.0000
   5.000   0.9473   0.01032   0.00402  -0.0967   0.1313   1.0000
   5.250   0.9664   0.01065   0.00429  -0.0950   0.1155   1.0000
   5.500   0.9863   0.01094   0.00453  -0.0935   0.1057   1.0000
   5.750   1.0074   0.01115   0.00474  -0.0922   0.1002   1.0000
   6.000   1.0257   0.01145   0.00499  -0.0904   0.0906   1.0000
   6.250   1.0405   0.01188   0.00529  -0.0879   0.0664   1.0000
   6.500   1.0566   0.01226   0.00561  -0.0857   0.0531   1.0000
   6.750   1.0740   0.01260   0.00592  -0.0838   0.0466   1.0000
   7.000   1.0922   0.01292   0.00622  -0.0820   0.0399   1.0000
   7.250   1.1050   0.01351   0.00670  -0.0793   0.0211   1.0000
   7.500   1.1210   0.01396   0.00711  -0.0773   0.0150   1.0000
   7.750   1.1386   0.01434   0.00750  -0.0755   0.0133   1.0000
   8.000   1.1554   0.01476   0.00794  -0.0736   0.0115   1.0000
   8.250   1.1732   0.01514   0.00835  -0.0719   0.0109   1.0000
   8.500   1.1908   0.01553   0.00877  -0.0703   0.0102   1.0000
   8.750   1.2080   0.01595   0.00922  -0.0686   0.0097   1.0000
   9.000   1.2242   0.01643   0.00972  -0.0668   0.0090   1.0000
   9.250   1.2397   0.01696   0.01027  -0.0649   0.0084   1.0000
   9.500   1.2546   0.01753   0.01088  -0.0630   0.0079   1.0000
   9.750   1.2706   0.01805   0.01143  -0.0613   0.0076   1.0000
  10.000   1.2862   0.01860   0.01202  -0.0596   0.0073   1.0000
  10.250   1.3013   0.01918   0.01265  -0.0579   0.0069   1.0000
  10.500   1.3156   0.01983   0.01335  -0.0561   0.0067   1.0000
  10.750   1.3297   0.02050   0.01405  -0.0544   0.0064   1.0000
  11.000   1.3428   0.02125   0.01484  -0.0526   0.0061   1.0000
  11.250   1.3549   0.02209   0.01572  -0.0507   0.0059   1.0000
  11.500   1.3648   0.02310   0.01679  -0.0487   0.0056   1.0000
  11.750   1.3772   0.02396   0.01770  -0.0470   0.0055   1.0000
  12.000   1.3899   0.02480   0.01861  -0.0455   0.0053   1.0000
  12.250   1.4008   0.02580   0.01967  -0.0438   0.0052   1.0000
  12.500   1.4116   0.02683   0.02076  -0.0422   0.0051   1.0000
  12.750   1.4214   0.02795   0.02195  -0.0406   0.0049   1.0000
  13.000   1.4324   0.02901   0.02305  -0.0392   0.0047   1.0000
  13.250   1.4419   0.03019   0.02430  -0.0377   0.0046   1.0000
  13.500   1.4494   0.03157   0.02575  -0.0361   0.0045   1.0000
  13.750   1.4586   0.03283   0.02706  -0.0349   0.0043   1.0000
  14.000   1.4643   0.03444   0.02877  -0.0334   0.0043   1.0000
  14.250   1.4704   0.03604   0.03043  -0.0320   0.0042   1.0000
  14.500   1.4759   0.03774   0.03219  -0.0308   0.0041   1.0000
  14.750   1.4790   0.03972   0.03427  -0.0296   0.0041   1.0000
  15.000   1.4791   0.04207   0.03670  -0.0284   0.0039   1.0000
  15.250   1.4782   0.04459   0.03933  -0.0273   0.0039   1.0000
  15.500   1.4775   0.04719   0.04203  -0.0265   0.0038   1.0000
  15.750   1.4790   0.04965   0.04458  -0.0258   0.0038   1.0000
  16.000   1.4797   0.05227   0.04730  -0.0254   0.0037   1.0000
  16.250   1.4798   0.05502   0.05015  -0.0250   0.0037   1.0000
  16.500   1.4790   0.05797   0.05320  -0.0248   0.0036   1.0000
  16.750   1.4738   0.06155   0.05690  -0.0249   0.0036   1.0000
  17.000   1.4723   0.06478   0.06023  -0.0250   0.0036   1.0000
  17.250   1.4657   0.06873   0.06430  -0.0254   0.0035   1.0000
  17.500   1.4624   0.07236   0.06803  -0.0260   0.0035   1.0000
  17.750   1.4519   0.07716   0.07297  -0.0269   0.0035   1.0000
  18.000   1.4478   0.08115   0.07705  -0.0279   0.0034   1.0000
  18.250   1.4356   0.08647   0.08250  -0.0294   0.0034   1.0000
  18.500   1.4228   0.09213   0.08829  -0.0313   0.0034   1.0000
  18.750   1.4104   0.09788   0.09417  -0.0335   0.0034   1.0000
  19.000   1.3989   0.10368   0.10009  -0.0358   0.0034   1.0000
  19.250   1.3836   0.11029   0.10683  -0.0388   0.0033   1.0000
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