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GOE 504 AIRFOIL (goe504-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 504 AIRFOIL (goe504-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.89 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe504-il-1000000.txt
Download as CSV file: xf-goe504-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 504 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.6202   0.08142   0.07912  -0.0855   0.9984   0.0135
 -16.000  -0.6380   0.07345   0.07102  -0.0921   0.9972   0.0136
 -15.750  -0.6461   0.06720   0.06467  -0.0980   0.9957   0.0137
 -15.500  -0.6633   0.05960   0.05691  -0.1050   0.9939   0.0137
 -15.250  -0.6683   0.05418   0.05139  -0.1101   0.9914   0.0138
 -15.000  -0.6586   0.05045   0.04760  -0.1147   0.9889   0.0140
 -14.750  -0.6675   0.04382   0.04078  -0.1218   0.9861   0.0140
 -14.500  -0.6514   0.04047   0.03734  -0.1272   0.9841   0.0142
 -14.250  -0.6413   0.03670   0.03345  -0.1325   0.9812   0.0145
 -14.000  -0.6358   0.03307   0.02968  -0.1367   0.9757   0.0146
 -13.750  -0.6167   0.03082   0.02733  -0.1407   0.9721   0.0150
 -13.500  -0.5995   0.02830   0.02465  -0.1447   0.9681   0.0153
 -13.250  -0.5772   0.02693   0.02316  -0.1474   0.9615   0.0157
 -13.000  -0.5491   0.02504   0.02111  -0.1516   0.9576   0.0158
 -12.750  -0.5314   0.02306   0.01898  -0.1539   0.9487   0.0164
 -12.500  -0.5004   0.02233   0.01822  -0.1565   0.9412   0.0167
 -12.250  -0.4819   0.02175   0.01756  -0.1563   0.9289   0.0170
 -12.000  -0.4671   0.02111   0.01682  -0.1552   0.9150   0.0173
 -11.750  -0.4549   0.02059   0.01619  -0.1533   0.8997   0.0175
 -11.500  -0.4450   0.02021   0.01570  -0.1507   0.8837   0.0179
 -11.250  -0.4374   0.01966   0.01502  -0.1476   0.8674   0.0182
 -11.000  -0.4290   0.01926   0.01449  -0.1445   0.8519   0.0185
 -10.750  -0.4160   0.01890   0.01400  -0.1421   0.8379   0.0189
 -10.500  -0.4019   0.01858   0.01354  -0.1399   0.8248   0.0192
 -10.250  -0.3863   0.01838   0.01320  -0.1379   0.8127   0.0195
 -10.000  -0.3765   0.01714   0.01186  -0.1353   0.8010   0.0201
  -9.750  -0.3592   0.01680   0.01148  -0.1337   0.7906   0.0205
  -9.500  -0.3415   0.01646   0.01107  -0.1321   0.7809   0.0209
  -9.250  -0.3220   0.01625   0.01079  -0.1307   0.7717   0.0214
  -9.000  -0.3026   0.01592   0.01038  -0.1293   0.7634   0.0219
  -8.750  -0.2833   0.01554   0.00992  -0.1279   0.7548   0.0224
  -8.500  -0.2627   0.01522   0.00953  -0.1266   0.7472   0.0229
  -8.250  -0.2415   0.01495   0.00918  -0.1255   0.7397   0.0233
  -8.000  -0.2184   0.01492   0.00906  -0.1246   0.7327   0.0237
  -7.750  -0.2043   0.01383   0.00793  -0.1224   0.7254   0.0245
  -7.500  -0.1845   0.01345   0.00751  -0.1211   0.7186   0.0252
  -7.250  -0.1627   0.01312   0.00715  -0.1201   0.7122   0.0257
  -7.000  -0.1414   0.01283   0.00680  -0.1189   0.7054   0.0263
  -6.750  -0.1193   0.01253   0.00647  -0.1179   0.6992   0.0269
  -6.500  -0.0968   0.01228   0.00616  -0.1169   0.6927   0.0276
  -6.250  -0.0736   0.01211   0.00593  -0.1160   0.6865   0.0282
  -6.000  -0.0493   0.01193   0.00571  -0.1153   0.6804   0.0286
  -5.750  -0.0296   0.01151   0.00521  -0.1138   0.6739   0.0291
  -5.500  -0.0093   0.01107   0.00472  -0.1124   0.6681   0.0299
  -5.250   0.0132   0.01078   0.00439  -0.1114   0.6617   0.0306
  -5.000   0.0360   0.01060   0.00414  -0.1104   0.6554   0.0315
  -4.750   0.0603   0.01039   0.00391  -0.1098   0.6493   0.0323
  -4.500   0.0839   0.01023   0.00370  -0.1089   0.6429   0.0330
  -4.250   0.1081   0.01009   0.00350  -0.1082   0.6369   0.0337
  -4.000   0.1326   0.00995   0.00333  -0.1075   0.6302   0.0342
  -3.750   0.1559   0.00984   0.00314  -0.1066   0.6237   0.0350
  -3.500   0.1807   0.00967   0.00295  -0.1059   0.6177   0.0367
  -3.250   0.2044   0.00956   0.00280  -0.1051   0.6109   0.0384
  -3.000   0.2289   0.00947   0.00268  -0.1044   0.6047   0.0402
  -2.750   0.2532   0.00938   0.00257  -0.1037   0.5979   0.0456
  -2.500   0.2737   0.00908   0.00243  -0.1023   0.5916   0.0955
  -2.250   0.2923   0.00855   0.00226  -0.1007   0.5856   0.1975
  -2.000   0.3147   0.00844   0.00224  -0.0997   0.5792   0.2352
  -1.750   0.3389   0.00840   0.00224  -0.0990   0.5732   0.2546
  -1.500   0.3632   0.00838   0.00223  -0.0983   0.5669   0.2701
  -1.250   0.3862   0.00840   0.00223  -0.0974   0.5606   0.2810
  -1.000   0.4115   0.00838   0.00222  -0.0969   0.5550   0.2911
  -0.750   0.4349   0.00838   0.00223  -0.0960   0.5488   0.3028
  -0.500   0.4582   0.00840   0.00224  -0.0951   0.5432   0.3129
   0.000   0.5047   0.00841   0.00226  -0.0934   0.5317   0.3362
   0.250   0.5274   0.00840   0.00227  -0.0924   0.5263   0.3494
   0.500   0.5492   0.00838   0.00229  -0.0912   0.5208   0.3681
   0.750   0.5682   0.00836   0.00231  -0.0894   0.5151   0.3943
   1.000   0.5880   0.00826   0.00235  -0.0879   0.5102   0.4407
   1.250   0.6064   0.00811   0.00240  -0.0861   0.5050   0.5099
   1.500   0.6204   0.00795   0.00248  -0.0834   0.4993   0.6039
   1.750   0.6345   0.00777   0.00259  -0.0806   0.4946   0.7011
   2.000   0.6468   0.00758   0.00270  -0.0773   0.4897   0.8006
   2.250   0.6724   0.00750   0.00290  -0.0768   0.4836   0.9051
   2.500   0.7624   0.00775   0.00316  -0.0906   0.4759   0.9539
   2.750   0.8135   0.00798   0.00334  -0.0960   0.4691   0.9675
   3.000   0.8541   0.00818   0.00350  -0.0989   0.4634   0.9774
   3.250   0.8899   0.00835   0.00364  -0.1009   0.4570   0.9849
   3.500   0.9254   0.00857   0.00380  -0.1029   0.4504   0.9904
   3.750   0.9617   0.00871   0.00393  -0.1050   0.4450   0.9947
   4.000   1.0007   0.00889   0.00407  -0.1077   0.4385   0.9980
   4.250   1.0404   0.00907   0.00421  -0.1107   0.4325   1.0000
   4.500   1.0501   0.00914   0.00428  -0.1071   0.4273   1.0000
   4.750   1.0592   0.00928   0.00438  -0.1035   0.4218   1.0000
   5.000   1.0723   0.00941   0.00450  -0.1007   0.4164   1.0000
   5.250   1.0870   0.00954   0.00462  -0.0983   0.4107   1.0000
   5.500   1.0995   0.00975   0.00479  -0.0955   0.4048   1.0000
   5.750   1.1168   0.00989   0.00493  -0.0936   0.3998   1.0000
   6.000   1.1327   0.01009   0.00511  -0.0916   0.3932   1.0000
   6.250   1.1480   0.01033   0.00533  -0.0894   0.3869   1.0000
   6.500   1.1651   0.01055   0.00553  -0.0877   0.3792   1.0000
   6.750   1.1804   0.01085   0.00579  -0.0856   0.3708   1.0000
   7.000   1.1978   0.01111   0.00604  -0.0841   0.3640   1.0000
   7.250   1.2132   0.01145   0.00634  -0.0821   0.3550   1.0000
   7.500   1.2292   0.01180   0.00667  -0.0804   0.3464   1.0000
   7.750   1.2458   0.01214   0.00699  -0.0788   0.3392   1.0000
   8.000   1.2620   0.01253   0.00735  -0.0772   0.3313   1.0000
   8.250   1.2777   0.01294   0.00775  -0.0756   0.3231   1.0000
   8.750   1.3077   0.01390   0.00865  -0.0723   0.3052   1.0000
   9.000   1.3210   0.01449   0.00920  -0.0705   0.2956   1.0000
   9.250   1.3329   0.01516   0.00982  -0.0685   0.2840   1.0000
   9.500   1.3453   0.01584   0.01047  -0.0668   0.2720   1.0000
   9.750   1.3558   0.01664   0.01122  -0.0648   0.2591   1.0000
  10.000   1.3645   0.01758   0.01209  -0.0628   0.2451   1.0000
  10.250   1.3653   0.01899   0.01336  -0.0599   0.2235   1.0000
  10.500   1.3607   0.02079   0.01501  -0.0566   0.1967   1.0000
  10.750   1.3499   0.02311   0.01713  -0.0530   0.1638   1.0000
  11.000   1.3277   0.02639   0.02016  -0.0487   0.1236   1.0000
  11.250   1.2944   0.03079   0.02432  -0.0442   0.0768   1.0000
  11.500   1.2716   0.03475   0.02814  -0.0411   0.0394   1.0000
  11.750   1.2623   0.03781   0.03116  -0.0392   0.0186   1.0000
  12.000   1.2665   0.03980   0.03320  -0.0383   0.0163   1.0000
  12.250   1.2723   0.04169   0.03513  -0.0375   0.0151   1.0000
  12.500   1.2778   0.04362   0.03712  -0.0368   0.0144   1.0000
  12.750   1.2828   0.04566   0.03921  -0.0361   0.0139   1.0000
  13.000   1.2851   0.04799   0.04160  -0.0354   0.0132   1.0000
  13.250   1.2865   0.05047   0.04415  -0.0348   0.0127   1.0000
  13.500   1.2874   0.05303   0.04678  -0.0342   0.0123   1.0000
  13.750   1.2909   0.05537   0.04919  -0.0338   0.0121   1.0000
  14.000   1.2931   0.05789   0.05176  -0.0335   0.0117   1.0000
  14.250   1.2945   0.06053   0.05448  -0.0332   0.0113   1.0000
  14.500   1.2955   0.06326   0.05727  -0.0329   0.0113   1.0000
  14.750   1.2940   0.06628   0.06037  -0.0327   0.0110   1.0000
  15.000   1.2928   0.06935   0.06350  -0.0326   0.0107   1.0000
  15.250   1.2897   0.07268   0.06690  -0.0325   0.0104   1.0000
  15.500   1.2846   0.07629   0.07059  -0.0325   0.0102   1.0000
  15.750   1.2769   0.08026   0.07466  -0.0326   0.0101   1.0000
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