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GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GEMINI (smoothed) (geminism-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.58 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-geminism-il-1000000.txt
Download as CSV file: xf-geminism-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GEMINI (smoothed)                               
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.8964   0.11279   0.11036  -0.0356   1.0000   0.0122
 -18.250  -0.9293   0.10282   0.10024  -0.0409   1.0000   0.0122
 -18.000  -0.9582   0.09380   0.09109  -0.0458   1.0000   0.0122
 -17.750  -0.9839   0.08559   0.08274  -0.0502   1.0000   0.0122
 -17.500  -1.0066   0.07803   0.07506  -0.0543   1.0000   0.0122
 -17.250  -1.0261   0.07121   0.06811  -0.0581   1.0000   0.0123
 -17.000  -1.0428   0.06500   0.06177  -0.0615   1.0000   0.0123
 -16.750  -1.0564   0.05952   0.05615  -0.0644   1.0000   0.0124
 -16.500  -1.0666   0.05470   0.05121  -0.0669   1.0000   0.0124
 -16.250  -1.0742   0.05042   0.04680  -0.0690   1.0000   0.0125
 -16.000  -1.0786   0.04671   0.04299  -0.0707   1.0000   0.0125
 -15.750  -1.0805   0.04346   0.03963  -0.0720   1.0000   0.0126
 -15.500  -1.0942   0.03915   0.03516  -0.0731   1.0000   0.0128
 -15.250  -1.1049   0.03548   0.03135  -0.0736   1.0000   0.0130
 -15.000  -1.1091   0.03275   0.02852  -0.0734   1.0000   0.0132
 -14.750  -1.1082   0.03069   0.02639  -0.0728   1.0000   0.0134
 -14.500  -1.1044   0.02906   0.02469  -0.0719   1.0000   0.0136
 -14.250  -1.0987   0.02771   0.02328  -0.0707   1.0000   0.0138
 -14.000  -1.0923   0.02654   0.02205  -0.0692   1.0000   0.0141
 -13.750  -1.0857   0.02550   0.02095  -0.0674   1.0000   0.0143
 -13.500  -1.0793   0.02457   0.01996  -0.0652   1.0000   0.0146
 -13.250  -1.0734   0.02377   0.01909  -0.0626   1.0000   0.0149
 -13.000  -1.0682   0.02310   0.01836  -0.0595   1.0000   0.0151
 -12.750  -1.0652   0.02256   0.01776  -0.0557   1.0000   0.0154
 -12.500  -1.0673   0.02216   0.01731  -0.0507   1.0000   0.0156
 -12.250  -1.0702   0.02184   0.01694  -0.0454   1.0000   0.0157
 -12.000  -1.0498   0.02077   0.01577  -0.0452   0.9986   0.0162
 -11.750  -1.0232   0.01960   0.01455  -0.0464   0.9958   0.0169
 -11.500  -0.9942   0.01895   0.01389  -0.0474   0.9926   0.0175
 -11.250  -0.9644   0.01839   0.01328  -0.0485   0.9891   0.0180
 -11.000  -0.9341   0.01783   0.01268  -0.0497   0.9859   0.0187
 -10.750  -0.9033   0.01730   0.01210  -0.0509   0.9832   0.0193
 -10.500  -0.8706   0.01686   0.01161  -0.0523   0.9812   0.0197
 -10.250  -0.8411   0.01575   0.01043  -0.0537   0.9794   0.0208
 -10.000  -0.8084   0.01522   0.00989  -0.0553   0.9760   0.0217
  -9.750  -0.7744   0.01482   0.00947  -0.0571   0.9716   0.0226
  -9.500  -0.7372   0.01439   0.00900  -0.0595   0.9683   0.0236
  -9.250  -0.7061   0.01404   0.00860  -0.0605   0.9590   0.0242
  -9.000  -0.6763   0.01331   0.00780  -0.0616   0.9496   0.0254
  -8.750  -0.6441   0.01280   0.00726  -0.0629   0.9403   0.0266
  -8.500  -0.6128   0.01248   0.00689  -0.0640   0.9297   0.0278
  -8.250  -0.5860   0.01223   0.00658  -0.0639   0.9164   0.0290
  -8.000  -0.5599   0.01203   0.00631  -0.0637   0.9028   0.0298
  -7.750  -0.5381   0.01155   0.00575  -0.0627   0.8883   0.0314
  -7.500  -0.5144   0.01128   0.00542  -0.0620   0.8746   0.0331
  -7.250  -0.4901   0.01108   0.00516  -0.0613   0.8617   0.0347
  -7.000  -0.4658   0.01092   0.00491  -0.0607   0.8493   0.0360
  -6.750  -0.4428   0.01065   0.00457  -0.0597   0.8373   0.0379
  -6.500  -0.4197   0.01039   0.00429  -0.0589   0.8262   0.0407
  -6.250  -0.3954   0.01024   0.00408  -0.0582   0.8157   0.0432
  -6.000  -0.3716   0.01003   0.00382  -0.0574   0.8050   0.0464
  -5.750  -0.3479   0.00981   0.00360  -0.0566   0.7952   0.0513
  -5.500  -0.3240   0.00964   0.00338  -0.0558   0.7856   0.0571
  -5.250  -0.2998   0.00944   0.00319  -0.0551   0.7762   0.0645
  -5.000  -0.2764   0.00921   0.00298  -0.0543   0.7673   0.0783
  -4.750  -0.2539   0.00891   0.00276  -0.0533   0.7580   0.1013
  -4.500  -0.2331   0.00850   0.00253  -0.0520   0.7494   0.1501
  -4.250  -0.2109   0.00821   0.00237  -0.0510   0.7406   0.1917
  -4.000  -0.1873   0.00800   0.00224  -0.0502   0.7322   0.2211
  -3.750  -0.1636   0.00784   0.00212  -0.0494   0.7235   0.2463
  -3.500  -0.1395   0.00766   0.00201  -0.0486   0.7153   0.2736
  -3.250  -0.1166   0.00746   0.00190  -0.0477   0.7069   0.3088
  -3.000  -0.0933   0.00724   0.00180  -0.0468   0.6989   0.3498
  -2.750  -0.0706   0.00705   0.00171  -0.0458   0.6907   0.3909
  -2.500  -0.0474   0.00685   0.00164  -0.0449   0.6827   0.4358
  -2.250  -0.0251   0.00668   0.00159  -0.0437   0.6746   0.4830
  -2.000  -0.0014   0.00654   0.00155  -0.0428   0.6666   0.5203
  -1.750   0.0218   0.00645   0.00152  -0.0418   0.6584   0.5540
  -1.500   0.0463   0.00636   0.00150  -0.0411   0.6504   0.5823
  -1.250   0.0699   0.00632   0.00148  -0.0402   0.6421   0.6094
  -0.750   0.1199   0.00627   0.00145  -0.0389   0.6256   0.6449
  -0.500   0.1454   0.00624   0.00144  -0.0383   0.6171   0.6610
   0.000   0.1954   0.00622   0.00144  -0.0370   0.5996   0.6927
   0.500   0.2445   0.00621   0.00146  -0.0356   0.5814   0.7273
   0.750   0.2690   0.00620   0.00148  -0.0348   0.5724   0.7460
   1.250   0.3177   0.00620   0.00154  -0.0333   0.5532   0.7843
   1.500   0.3419   0.00622   0.00158  -0.0324   0.5438   0.8052
   1.750   0.3658   0.00622   0.00164  -0.0315   0.5338   0.8319
   2.000   0.3907   0.00621   0.00171  -0.0308   0.5242   0.8629
   2.250   0.4168   0.00626   0.00178  -0.0304   0.5142   0.8892
   2.500   0.4465   0.00631   0.00186  -0.0309   0.5040   0.9075
   2.750   0.4785   0.00639   0.00194  -0.0318   0.4943   0.9234
   3.250   0.5536   0.00661   0.00213  -0.0365   0.4734   0.9471
   3.500   0.5949   0.00675   0.00224  -0.0397   0.4633   0.9544
   4.000   0.6784   0.00706   0.00249  -0.0463   0.4427   0.9638
   4.250   0.7175   0.00723   0.00263  -0.0489   0.4332   0.9668
   4.750   0.7894   0.00762   0.00295  -0.0529   0.4098   0.9736
   5.000   0.8227   0.00781   0.00311  -0.0542   0.3987   0.9777
   5.250   0.8565   0.00803   0.00328  -0.0558   0.3867   0.9815
   5.750   0.9212   0.00846   0.00363  -0.0582   0.3621   0.9911
   6.000   0.9539   0.00869   0.00383  -0.0595   0.3504   0.9946
   6.250   0.9886   0.00894   0.00402  -0.0614   0.3327   0.9968
   6.500   1.0225   0.00925   0.00423  -0.0632   0.3125   0.9988
   6.750   1.0533   0.00955   0.00445  -0.0642   0.2922   1.0000
   7.000   1.0682   0.00983   0.00465  -0.0619   0.2729   1.0000
   7.250   1.0814   0.01020   0.00490  -0.0592   0.2500   1.0000
   7.500   1.0931   0.01068   0.00523  -0.0562   0.2208   1.0000
   7.750   1.1017   0.01136   0.00568  -0.0528   0.1820   1.0000
   8.000   1.1053   0.01231   0.00633  -0.0486   0.1321   1.0000
   8.250   1.0938   0.01396   0.00750  -0.0417   0.0525   1.0000
   8.500   1.1033   0.01455   0.00803  -0.0385   0.0404   1.0000
   8.750   1.1118   0.01500   0.00847  -0.0349   0.0351   1.0000
   9.000   1.1230   0.01539   0.00887  -0.0320   0.0323   1.0000
   9.250   1.1322   0.01592   0.00940  -0.0288   0.0288   1.0000
   9.500   1.1462   0.01632   0.00983  -0.0266   0.0272   1.0000
   9.750   1.1587   0.01683   0.01035  -0.0243   0.0252   1.0000
  10.000   1.1684   0.01753   0.01107  -0.0216   0.0229   1.0000
  10.250   1.1831   0.01803   0.01160  -0.0199   0.0217   1.0000
  10.500   1.1961   0.01866   0.01224  -0.0180   0.0202   1.0000
  10.750   1.2046   0.01957   0.01318  -0.0156   0.0186   1.0000
  11.000   1.2175   0.02029   0.01395  -0.0140   0.0178   1.0000
  11.250   1.2301   0.02107   0.01477  -0.0124   0.0169   1.0000
  11.500   1.2417   0.02195   0.01567  -0.0108   0.0161   1.0000
  11.750   1.2507   0.02305   0.01681  -0.0092   0.0153   1.0000
  12.000   1.2551   0.02455   0.01837  -0.0072   0.0145   1.0000
  12.250   1.2669   0.02557   0.01944  -0.0061   0.0141   1.0000
  12.500   1.2770   0.02678   0.02071  -0.0049   0.0137   1.0000
  12.750   1.2856   0.02813   0.02212  -0.0038   0.0132   1.0000
  13.000   1.2936   0.02960   0.02363  -0.0028   0.0129   1.0000
  13.250   1.3003   0.03122   0.02530  -0.0018   0.0125   1.0000
  13.500   1.3046   0.03311   0.02725  -0.0008   0.0122   1.0000
  13.750   1.3044   0.03546   0.02967   0.0002   0.0118   1.0000
  14.000   1.2984   0.03848   0.03279   0.0011   0.0115   1.0000
  14.250   1.2992   0.04093   0.03533   0.0017   0.0114   1.0000
  14.750   1.3043   0.04571   0.04027   0.0024   0.0111   1.0000
  15.000   1.3052   0.04840   0.04303   0.0025   0.0109   1.0000
  15.250   1.3048   0.05126   0.04598   0.0026   0.0107   1.0000
  15.500   1.3037   0.05429   0.04909   0.0025   0.0106   1.0000
  15.750   1.3026   0.05740   0.05227   0.0023   0.0104   1.0000
  16.000   1.3012   0.06061   0.05556   0.0020   0.0103   1.0000
  16.250   1.2996   0.06387   0.05889   0.0016   0.0101   1.0000
  16.500   1.2974   0.06727   0.06236   0.0012   0.0099   1.0000
  16.750   1.2947   0.07079   0.06596   0.0006   0.0098   1.0000
  17.000   1.2914   0.07445   0.06969  -0.0001   0.0096   1.0000
  17.250   1.2870   0.07826   0.07357  -0.0009   0.0095   1.0000
  17.500   1.2813   0.08229   0.07767  -0.0017   0.0094   1.0000
  17.750   1.2745   0.08651   0.08197  -0.0027   0.0093   1.0000
  18.000   1.2669   0.09088   0.08641  -0.0038   0.0092   1.0000
  18.250   1.2583   0.09534   0.09096  -0.0048   0.0090   1.0000
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