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GIII BL0 AIRFOIL (giiia-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GIII BL0 AIRFOIL (giiia-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.16 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-giiia-il-1000000.txt
Download as CSV file: xf-giiia-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GIII BL0 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -1.0122   0.06265   0.06050  -0.0252   1.0000   0.0061
 -14.000  -1.0488   0.05275   0.05033  -0.0315   1.0000   0.0061
 -13.750  -1.0689   0.04708   0.04445  -0.0336   1.0000   0.0061
 -13.500  -1.0813   0.04312   0.04033  -0.0340   1.0000   0.0061
 -13.250  -1.0909   0.03991   0.03695  -0.0331   1.0000   0.0061
 -13.000  -1.0958   0.03743   0.03433  -0.0317   1.0000   0.0062
 -12.750  -1.0993   0.03524   0.03198  -0.0296   1.0000   0.0063
 -12.500  -1.1004   0.03334   0.02993  -0.0272   1.0000   0.0064
 -12.250  -1.0994   0.03166   0.02810  -0.0246   1.0000   0.0064
 -12.000  -1.0959   0.03017   0.02647  -0.0219   1.0000   0.0066
 -11.750  -1.0914   0.02870   0.02484  -0.0191   1.0000   0.0067
 -11.500  -1.0834   0.02729   0.02327  -0.0166   1.0000   0.0068
 -11.250  -1.0725   0.02592   0.02175  -0.0146   1.0000   0.0070
 -11.000  -1.0596   0.02467   0.02034  -0.0127   1.0000   0.0071
 -10.750  -1.0453   0.02349   0.01900  -0.0109   1.0000   0.0073
 -10.500  -1.0295   0.02244   0.01782  -0.0093   1.0000   0.0075
 -10.250  -1.0122   0.02155   0.01681  -0.0078   1.0000   0.0077
 -10.000  -0.9935   0.02084   0.01600  -0.0064   1.0000   0.0078
  -9.750  -0.9830   0.01904   0.01398  -0.0038   1.0000   0.0082
  -9.500  -0.9687   0.01796   0.01281  -0.0016   1.0000   0.0086
  -9.250  -0.9504   0.01749   0.01230   0.0000   1.0000   0.0090
  -9.000  -0.9324   0.01707   0.01185   0.0017   1.0000   0.0094
  -8.750  -0.9158   0.01662   0.01135   0.0037   1.0000   0.0098
  -8.500  -0.9012   0.01615   0.01082   0.0062   1.0000   0.0102
  -8.250  -0.8890   0.01569   0.01030   0.0091   1.0000   0.0105
  -8.000  -0.8628   0.01523   0.00978   0.0091   0.9989   0.0108
  -7.750  -0.8344   0.01406   0.00849   0.0085   0.9968   0.0117
  -7.500  -0.8013   0.01343   0.00784   0.0070   0.9950   0.0126
  -7.250  -0.7669   0.01298   0.00735   0.0053   0.9926   0.0135
  -7.000  -0.7330   0.01256   0.00690   0.0038   0.9893   0.0144
  -6.750  -0.6995   0.01203   0.00632   0.0023   0.9866   0.0155
  -6.500  -0.6668   0.01144   0.00571   0.0010   0.9842   0.0173
  -6.250  -0.6354   0.01110   0.00534   0.0000   0.9807   0.0188
  -6.000  -0.6059   0.01083   0.00505  -0.0004   0.9753   0.0200
  -5.750  -0.5770   0.01029   0.00449  -0.0008   0.9710   0.0233
  -5.500  -0.5490   0.01004   0.00423  -0.0009   0.9656   0.0260
  -5.250  -0.5230   0.00969   0.00386  -0.0006   0.9590   0.0303
  -5.000  -0.4963   0.00943   0.00360  -0.0004   0.9531   0.0349
  -4.750  -0.4719   0.00912   0.00333   0.0003   0.9457   0.0436
  -4.500  -0.4465   0.00885   0.00309   0.0008   0.9398   0.0561
  -4.250  -0.4223   0.00854   0.00286   0.0015   0.9327   0.0766
  -4.000  -0.3980   0.00823   0.00265   0.0022   0.9258   0.1052
  -3.750  -0.3741   0.00795   0.00248   0.0030   0.9165   0.1370
  -3.500  -0.3495   0.00771   0.00232   0.0037   0.9075   0.1664
  -3.250  -0.3248   0.00747   0.00216   0.0043   0.8981   0.1973
  -3.000  -0.3003   0.00720   0.00201   0.0050   0.8885   0.2352
  -2.750  -0.2768   0.00685   0.00184   0.0058   0.8795   0.2933
  -2.500  -0.2585   0.00605   0.00157   0.0075   0.8696   0.4393
  -2.250  -0.2399   0.00544   0.00143   0.0093   0.8598   0.5778
  -2.000  -0.2166   0.00521   0.00134   0.0103   0.8497   0.6313
  -1.750  -0.1933   0.00503   0.00127   0.0114   0.8373   0.6761
  -1.500  -0.1689   0.00491   0.00119   0.0122   0.8224   0.7077
  -1.000  -0.1204   0.00469   0.00108   0.0141   0.7852   0.7687
  -0.750  -0.0965   0.00464   0.00104   0.0151   0.7535   0.7968
  -0.500  -0.0734   0.00469   0.00101   0.0163   0.7090   0.8231
  -0.250  -0.0492   0.00479   0.00103   0.0172   0.6729   0.8451
   0.000  -0.0242   0.00490   0.00106   0.0179   0.6392   0.8637
   0.250   0.0013   0.00502   0.00110   0.0185   0.6095   0.8797
   0.500   0.0274   0.00514   0.00116   0.0190   0.5840   0.8934
   0.750   0.0540   0.00526   0.00122   0.0193   0.5609   0.9049
   1.000   0.0801   0.00539   0.00127   0.0198   0.5379   0.9153
   1.250   0.1066   0.00555   0.00135   0.0202   0.5145   0.9244
   1.500   0.1342   0.00570   0.00144   0.0203   0.4917   0.9323
   1.750   0.1595   0.00587   0.00153   0.0209   0.4681   0.9404
   2.000   0.1878   0.00606   0.00162   0.0208   0.4371   0.9449
   2.250   0.2154   0.00634   0.00172   0.0208   0.3882   0.9489
   2.500   0.2394   0.00668   0.00185   0.0215   0.3364   0.9543
   2.750   0.2649   0.00714   0.00202   0.0217   0.2619   0.9580
   3.000   0.2949   0.00749   0.00220   0.0210   0.2254   0.9604
   3.250   0.3253   0.00774   0.00236   0.0204   0.2074   0.9631
   3.500   0.3539   0.00792   0.00250   0.0201   0.1976   0.9665
   3.750   0.3798   0.00808   0.00264   0.0205   0.1910   0.9704
   4.000   0.4139   0.00825   0.00278   0.0190   0.1853   0.9715
   4.250   0.4478   0.00847   0.00297   0.0175   0.1791   0.9725
   4.500   0.4825   0.00860   0.00312   0.0159   0.1768   0.9734
   4.750   0.5165   0.00875   0.00328   0.0143   0.1741   0.9746
   5.000   0.5496   0.00892   0.00345   0.0130   0.1707   0.9760
   5.250   0.5812   0.00913   0.00364   0.0120   0.1639   0.9778
   5.500   0.6119   0.00922   0.00375   0.0112   0.1601   0.9800
   5.750   0.6379   0.00938   0.00390   0.0115   0.1549   0.9832
   6.000   0.6718   0.00953   0.00405   0.0099   0.1486   0.9839
   6.250   0.7058   0.00964   0.00416   0.0084   0.1421   0.9847
   6.500   0.7391   0.00979   0.00431   0.0070   0.1335   0.9856
   6.750   0.7716   0.01000   0.00444   0.0056   0.1155   0.9867
   7.000   0.7960   0.01130   0.00524   0.0053   0.0329   0.9887
   7.250   0.8251   0.01188   0.00576   0.0046   0.0202   0.9905
   7.500   0.8546   0.01238   0.00628   0.0039   0.0162   0.9925
   7.750   0.8854   0.01282   0.00674   0.0029   0.0140   0.9944
   8.000   0.9190   0.01342   0.00741   0.0012   0.0121   0.9956
   8.250   0.9523   0.01385   0.00788  -0.0004   0.0111   0.9969
   8.500   0.9835   0.01434   0.00840  -0.0016   0.0102   0.9982
   8.750   1.0113   0.01518   0.00933  -0.0022   0.0092   0.9995
   9.000   1.0317   0.01594   0.01018  -0.0013   0.0088   1.0000
   9.250   1.0478   0.01641   0.01072   0.0006   0.0085   1.0000
   9.500   1.0625   0.01694   0.01132   0.0028   0.0082   1.0000
   9.750   1.0759   0.01751   0.01195   0.0052   0.0079   1.0000
  10.000   1.0883   0.01810   0.01261   0.0078   0.0077   1.0000
  10.250   1.1000   0.01869   0.01325   0.0105   0.0074   1.0000
  10.500   1.1110   0.01928   0.01389   0.0132   0.0071   1.0000
  10.750   1.1201   0.01995   0.01461   0.0162   0.0068   1.0000
  11.000   1.1222   0.02098   0.01574   0.0203   0.0066   1.0000
  11.250   1.1104   0.02280   0.01770   0.0263   0.0063   1.0000
  11.500   1.1175   0.02336   0.01832   0.0295   0.0062   1.0000
  11.750   1.1210   0.02412   0.01917   0.0331   0.0061   1.0000
  12.000   1.1258   0.02511   0.02025   0.0360   0.0060   1.0000
  12.250   1.1307   0.02630   0.02154   0.0384   0.0059   1.0000
  12.500   1.1348   0.02769   0.02303   0.0404   0.0058   1.0000
  12.750   1.1377   0.02932   0.02476   0.0422   0.0057   1.0000
  13.000   1.1396   0.03116   0.02672   0.0436   0.0056   1.0000
  13.250   1.1402   0.03328   0.02896   0.0446   0.0056   1.0000
  13.500   1.1398   0.03568   0.03149   0.0451   0.0055   1.0000
  13.750   1.1377   0.03847   0.03440   0.0452   0.0054   1.0000
  14.000   1.1346   0.04166   0.03772   0.0446   0.0054   1.0000
  14.250   1.1299   0.04530   0.04150   0.0435   0.0053   1.0000
  14.500   1.1239   0.04938   0.04572   0.0418   0.0053   1.0000
  14.750   1.1161   0.05391   0.05038   0.0397   0.0052   1.0000
  15.000   1.1069   0.05881   0.05542   0.0373   0.0052   1.0000
  15.250   1.0948   0.06428   0.06102   0.0345   0.0052   1.0000
  15.500   1.0813   0.07016   0.06703   0.0314   0.0052   1.0000
  15.750   1.0656   0.07658   0.07359   0.0281   0.0052   1.0000
  16.000   1.0497   0.08332   0.08045   0.0245   0.0052   1.0000
  16.250   1.0324   0.09045   0.08771   0.0208   0.0052   1.0000
  16.500   1.0136   0.09809   0.09548   0.0168   0.0052   1.0000
  16.750   0.9946   0.10599   0.10351   0.0127   0.0052   1.0000
  17.000   0.9737   0.11443   0.11207   0.0083   0.0053   1.0000
  17.250   0.9518   0.12337   0.12112   0.0037   0.0053   1.0000
  17.500   0.9295   0.13262   0.13050  -0.0011   0.0054   1.0000
  17.750   0.9032   0.14329   0.14130  -0.0066   0.0055   1.0000
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