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GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GEMINI (smoothed) (geminism-il)
Reynolds number: 500,000
Max Cl/Cd: 92.73 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-geminism-il-500000.txt
Download as CSV file: xf-geminism-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7035   0.10249   0.09977  -0.0451   1.0000   0.0197
 -15.500  -0.7687   0.08536   0.08242  -0.0554   1.0000   0.0193
 -15.250  -0.8079   0.07440   0.07125  -0.0625   1.0000   0.0191
 -15.000  -0.8377   0.06600   0.06265  -0.0679   1.0000   0.0190
 -14.750  -0.8607   0.05935   0.05581  -0.0718   1.0000   0.0191
 -14.500  -0.8792   0.05391   0.05017  -0.0746   1.0000   0.0191
 -14.250  -0.8939   0.04944   0.04551  -0.0763   1.0000   0.0193
 -14.000  -0.9056   0.04574   0.04162  -0.0772   1.0000   0.0194
 -13.750  -0.9146   0.04274   0.03845  -0.0772   1.0000   0.0196
 -13.500  -0.9215   0.04033   0.03586  -0.0764   1.0000   0.0197
 -13.250  -0.9360   0.03703   0.03235  -0.0746   1.0000   0.0200
 -13.000  -0.9427   0.03451   0.02969  -0.0724   1.0000   0.0203
 -12.750  -0.9428   0.03295   0.02807  -0.0701   1.0000   0.0206
 -12.500  -0.9417   0.03179   0.02686  -0.0674   1.0000   0.0209
 -12.250  -0.9416   0.03083   0.02585  -0.0641   1.0000   0.0212
 -12.000  -0.9441   0.03003   0.02497  -0.0598   1.0000   0.0215
 -11.750  -0.9502   0.02935   0.02423  -0.0546   1.0000   0.0218
 -11.500  -0.9537   0.02864   0.02344  -0.0498   1.0000   0.0222
 -11.250  -0.9568   0.02797   0.02270  -0.0450   1.0000   0.0225
 -11.000  -0.9499   0.02712   0.02176  -0.0421   0.9993   0.0230
 -10.750  -0.9194   0.02595   0.02042  -0.0439   0.9966   0.0238
 -10.500  -0.8894   0.02489   0.01918  -0.0454   0.9933   0.0245
 -10.250  -0.8628   0.02309   0.01733  -0.0466   0.9896   0.0257
 -10.000  -0.8303   0.02233   0.01655  -0.0484   0.9865   0.0267
  -9.750  -0.7989   0.02151   0.01566  -0.0499   0.9828   0.0278
  -9.500  -0.7651   0.02067   0.01472  -0.0518   0.9804   0.0289
  -9.250  -0.7293   0.02001   0.01394  -0.0539   0.9786   0.0298
  -9.000  -0.7036   0.01849   0.01239  -0.0545   0.9729   0.0314
  -8.750  -0.6680   0.01784   0.01173  -0.0567   0.9699   0.0330
  -8.500  -0.6346   0.01722   0.01107  -0.0583   0.9648   0.0345
  -8.250  -0.6012   0.01662   0.01039  -0.0599   0.9588   0.0359
  -8.000  -0.5723   0.01567   0.00938  -0.0607   0.9510   0.0376
  -7.750  -0.5394   0.01499   0.00869  -0.0622   0.9442   0.0398
  -7.500  -0.5101   0.01452   0.00818  -0.0628   0.9344   0.0418
  -7.250  -0.4794   0.01410   0.00767  -0.0636   0.9252   0.0437
  -7.000  -0.4541   0.01344   0.00694  -0.0634   0.9141   0.0464
  -6.750  -0.4305   0.01304   0.00652  -0.0627   0.9013   0.0493
  -6.500  -0.4058   0.01273   0.00614  -0.0622   0.8894   0.0522
  -6.250  -0.3822   0.01232   0.00565  -0.0614   0.8780   0.0558
  -6.000  -0.3580   0.01196   0.00525  -0.0607   0.8670   0.0612
  -5.750  -0.3354   0.01164   0.00489  -0.0597   0.8553   0.0679
  -5.500  -0.3121   0.01133   0.00455  -0.0589   0.8446   0.0772
  -5.250  -0.2899   0.01090   0.00417  -0.0579   0.8345   0.0971
  -5.000  -0.2713   0.01032   0.00384  -0.0563   0.8235   0.1514
  -4.750  -0.2501   0.00991   0.00362  -0.0551   0.8139   0.2077
  -4.500  -0.2273   0.00964   0.00342  -0.0542   0.8044   0.2431
  -4.250  -0.2048   0.00937   0.00325  -0.0532   0.7949   0.2765
  -4.000  -0.1819   0.00912   0.00307  -0.0523   0.7863   0.3149
  -3.750  -0.1604   0.00884   0.00293  -0.0510   0.7769   0.3579
  -3.500  -0.1382   0.00860   0.00280  -0.0499   0.7685   0.4040
  -3.250  -0.1167   0.00837   0.00271  -0.0487   0.7594   0.4506
  -3.000  -0.0945   0.00819   0.00262  -0.0475   0.7511   0.4950
  -2.750  -0.0723   0.00805   0.00256  -0.0462   0.7422   0.5330
  -2.500  -0.0496   0.00793   0.00252  -0.0451   0.7340   0.5677
  -2.250  -0.0267   0.00784   0.00247  -0.0439   0.7254   0.5987
  -2.000  -0.0036   0.00778   0.00245  -0.0428   0.7171   0.6278
  -1.750   0.0197   0.00771   0.00242  -0.0417   0.7087   0.6526
  -1.500   0.0441   0.00767   0.00239  -0.0409   0.7003   0.6715
  -1.250   0.0687   0.00765   0.00235  -0.0401   0.6920   0.6891
  -1.000   0.0933   0.00761   0.00233  -0.0394   0.6834   0.7058
  -0.750   0.1179   0.00760   0.00230  -0.0386   0.6751   0.7235
  -0.500   0.1424   0.00756   0.00230  -0.0378   0.6663   0.7417
   0.000   0.1918   0.00751   0.00230  -0.0362   0.6488   0.7788
   0.250   0.2169   0.00752   0.00231  -0.0355   0.6405   0.7980
   0.500   0.2423   0.00750   0.00234  -0.0349   0.6310   0.8173
   0.750   0.2681   0.00752   0.00237  -0.0344   0.6222   0.8376
   1.000   0.2948   0.00754   0.00241  -0.0340   0.6128   0.8600
   1.250   0.3239   0.00757   0.00249  -0.0342   0.6032   0.8848
   1.500   0.3534   0.00765   0.00256  -0.0344   0.5938   0.9065
   1.750   0.3866   0.00772   0.00263  -0.0355   0.5834   0.9219
   2.000   0.4241   0.00783   0.00272  -0.0377   0.5731   0.9337
   2.250   0.4631   0.00797   0.00280  -0.0402   0.5625   0.9433
   2.500   0.5007   0.00809   0.00290  -0.0424   0.5513   0.9528
   2.750   0.5445   0.00825   0.00303  -0.0460   0.5400   0.9568
   3.000   0.5824   0.00843   0.00315  -0.0483   0.5292   0.9629
   3.250   0.6211   0.00861   0.00330  -0.0508   0.5179   0.9669
   3.500   0.6595   0.00879   0.00345  -0.0532   0.5069   0.9705
   3.750   0.6942   0.00899   0.00360  -0.0548   0.4966   0.9763
   4.000   0.7329   0.00918   0.00376  -0.0574   0.4856   0.9797
   4.250   0.7689   0.00936   0.00392  -0.0594   0.4752   0.9849
   4.500   0.8059   0.00955   0.00408  -0.0616   0.4652   0.9894
   4.750   0.8422   0.00976   0.00426  -0.0637   0.4541   0.9940
   5.000   0.8805   0.00991   0.00439  -0.0663   0.4410   0.9973
   5.250   0.9184   0.01007   0.00454  -0.0688   0.4283   1.0000
   5.500   0.9364   0.01022   0.00465  -0.0671   0.4176   1.0000
   5.750   0.9543   0.01037   0.00477  -0.0653   0.4068   1.0000
   6.000   0.9730   0.01050   0.00491  -0.0637   0.3970   1.0000
   6.250   0.9904   0.01068   0.00507  -0.0618   0.3869   1.0000
   6.500   1.0074   0.01088   0.00524  -0.0598   0.3749   1.0000
   6.750   1.0254   0.01106   0.00542  -0.0580   0.3624   1.0000
   7.000   1.0431   0.01128   0.00562  -0.0561   0.3499   1.0000
   7.250   1.0603   0.01154   0.00584  -0.0542   0.3353   1.0000
   7.500   1.0768   0.01184   0.00609  -0.0521   0.3183   1.0000
   7.750   1.0919   0.01221   0.00638  -0.0499   0.2984   1.0000
   8.000   1.1062   0.01263   0.00671  -0.0475   0.2742   1.0000
   8.250   1.1171   0.01319   0.00713  -0.0445   0.2441   1.0000
   8.500   1.1218   0.01404   0.00771  -0.0405   0.2012   1.0000
   8.750   1.1140   0.01525   0.00855  -0.0344   0.1435   1.0000
   9.000   1.0921   0.01701   0.00982  -0.0262   0.0687   1.0000
   9.250   1.0905   0.01816   0.01085  -0.0217   0.0478   1.0000
   9.500   1.0981   0.01900   0.01171  -0.0187   0.0415   1.0000
   9.750   1.1057   0.01990   0.01263  -0.0160   0.0376   1.0000
  10.000   1.1127   0.02090   0.01367  -0.0134   0.0346   1.0000
  10.250   1.1228   0.02179   0.01463  -0.0114   0.0322   1.0000
  10.500   1.1289   0.02298   0.01585  -0.0091   0.0300   1.0000
  10.750   1.1324   0.02442   0.01735  -0.0068   0.0281   1.0000
  11.000   1.1424   0.02551   0.01851  -0.0053   0.0266   1.0000
  11.250   1.1499   0.02683   0.01989  -0.0037   0.0252   1.0000
  11.500   1.1537   0.02851   0.02161  -0.0021   0.0241   1.0000
  11.750   1.1474   0.03108   0.02427  -0.0001   0.0230   1.0000
  12.000   1.1549   0.03265   0.02592   0.0009   0.0224   1.0000
  12.250   1.1604   0.03445   0.02780   0.0019   0.0217   1.0000
  12.500   1.1644   0.03643   0.02986   0.0027   0.0210   1.0000
  12.750   1.1676   0.03856   0.03206   0.0035   0.0204   1.0000
  13.000   1.1696   0.04085   0.03440   0.0042   0.0198   1.0000
  13.250   1.1699   0.04336   0.03697   0.0047   0.0193   1.0000
  13.500   1.1662   0.04634   0.04001   0.0053   0.0188   1.0000
  13.750   1.1571   0.04988   0.04363   0.0060   0.0184   1.0000
  14.000   1.1623   0.05212   0.04596   0.0061   0.0181   1.0000
  14.250   1.1660   0.05457   0.04849   0.0062   0.0177   1.0000
  14.500   1.1686   0.05715   0.05116   0.0062   0.0172   1.0000
  14.750   1.1706   0.05983   0.05391   0.0063   0.0169   1.0000
  15.000   1.1724   0.06255   0.05670   0.0062   0.0165   1.0000
  15.250   1.1744   0.06528   0.05950   0.0061   0.0162   1.0000
  15.500   1.1765   0.06804   0.06231   0.0059   0.0159   1.0000
  15.750   1.1784   0.07084   0.06516   0.0057   0.0156   1.0000
  16.000   1.1803   0.07359   0.06797   0.0055   0.0153   1.0000
  16.250   1.1821   0.07629   0.07071   0.0055   0.0151   1.0000
  16.500   1.1849   0.07852   0.07297   0.0062   0.0148   1.0000
  16.750   1.1887   0.08073   0.07525   0.0068   0.0145   1.0000
  17.000   1.1910   0.08362   0.07825   0.0063   0.0144   1.0000
  17.250   1.1925   0.08664   0.08137   0.0058   0.0142   1.0000
  17.500   1.1936   0.08974   0.08459   0.0052   0.0140   1.0000
  17.750   1.1942   0.09295   0.08791   0.0045   0.0138   1.0000
  18.000   1.1940   0.09632   0.09139   0.0037   0.0135   1.0000
  18.250   1.1934   0.09978   0.09495   0.0028   0.0133   1.0000
  18.500   1.1922   0.10335   0.09864   0.0017   0.0131   1.0000
  18.750   1.1905   0.10704   0.10243   0.0005   0.0129   1.0000
  19.000   1.1887   0.11078   0.10627  -0.0008   0.0128   1.0000
  19.250   1.1859   0.11475   0.11034  -0.0022   0.0126   1.0000
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