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GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: GEMINI (smoothed) (geminism-il)
Reynolds number: 50,000
Max Cl/Cd: 28.33 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-geminism-il-50000-n5.txt
Download as CSV file: xf-geminism-il-50000-n5.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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.5131   0.09824   0.09071  -0.0542   1.0000   0.0645
 -11.750  -0.5344   0.09013   0.08261  -0.0589   1.0000   0.0643
 -11.500  -0.5596   0.08261   0.07508  -0.0632   1.0000   0.0639
 -11.250  -0.5869   0.07621   0.06863  -0.0664   1.0000   0.0636
 -11.000  -0.6146   0.07109   0.06343  -0.0677   1.0000   0.0633
 -10.750  -0.6420   0.06713   0.05937  -0.0667   1.0000   0.0632
 -10.500  -0.6690   0.06413   0.05628  -0.0635   1.0000   0.0632
 -10.250  -0.6932   0.06138   0.05338  -0.0595   1.0000   0.0633
 -10.000  -0.7133   0.05864   0.05043  -0.0556   1.0000   0.0637
  -9.750  -0.7298   0.05603   0.04755  -0.0514   1.0000   0.0641
  -9.500  -0.7411   0.05355   0.04483  -0.0473   1.0000   0.0647
  -9.250  -0.7416   0.05129   0.04248  -0.0443   1.0000   0.0656
  -9.000  -0.7416   0.04927   0.04033  -0.0412   1.0000   0.0665
  -8.750  -0.7404   0.04747   0.03839  -0.0380   1.0000   0.0678
  -8.500  -0.7383   0.04584   0.03661  -0.0349   1.0000   0.0697
  -8.250  -0.7355   0.04419   0.03475  -0.0318   1.0000   0.0719
  -8.000  -0.7313   0.04249   0.03273  -0.0288   1.0000   0.0741
  -7.750  -0.7246   0.04082   0.03065  -0.0259   1.0000   0.0761
  -7.500  -0.7132   0.03919   0.02891  -0.0238   1.0000   0.0780
  -7.250  -0.7018   0.03796   0.02768  -0.0218   1.0000   0.0809
  -7.000  -0.6802   0.03665   0.02619  -0.0216   0.9973   0.0856
  -6.750  -0.6461   0.03509   0.02435  -0.0233   0.9911   0.0910
  -6.500  -0.6132   0.03376   0.02302  -0.0250   0.9846   0.0971
  -6.250  -0.5789   0.03256   0.02167  -0.0269   0.9783   0.1061
  -6.000  -0.5479   0.03146   0.02052  -0.0281   0.9705   0.1159
  -5.750  -0.5185   0.03041   0.01949  -0.0292   0.9625   0.1300
  -5.500  -0.4873   0.02932   0.01850  -0.0308   0.9551   0.1514
  -5.250  -0.4602   0.02826   0.01764  -0.0316   0.9463   0.1881
  -5.000  -0.4340   0.02721   0.01689  -0.0322   0.9376   0.2477
  -4.750  -0.4044   0.02632   0.01630  -0.0334   0.9300   0.3221
  -4.500  -0.3814   0.02576   0.01603  -0.0330   0.9202   0.3888
  -4.250  -0.3493   0.02535   0.01586  -0.0338   0.9133   0.4628
  -4.000  -0.3288   0.02518   0.01589  -0.0322   0.9028   0.5281
  -3.750  -0.3020   0.02513   0.01600  -0.0313   0.8946   0.5925
  -3.500  -0.2732   0.02513   0.01602  -0.0308   0.8862   0.6398
  -3.250  -0.2427   0.02511   0.01590  -0.0307   0.8779   0.6754
  -3.000  -0.2095   0.02509   0.01581  -0.0311   0.8700   0.7075
  -2.750  -0.1775   0.02514   0.01577  -0.0313   0.8616   0.7363
  -2.500  -0.1418   0.02516   0.01567  -0.0321   0.8539   0.7641
  -2.250  -0.1099   0.02522   0.01562  -0.0323   0.8452   0.7911
  -2.000  -0.0678   0.02531   0.01558  -0.0342   0.8379   0.8154
  -1.750  -0.0320   0.02540   0.01555  -0.0353   0.8294   0.8408
  -1.500   0.0170   0.02551   0.01553  -0.0386   0.8221   0.8626
  -1.250   0.0649   0.02561   0.01547  -0.0419   0.8144   0.8836
  -1.000   0.1133   0.02564   0.01536  -0.0456   0.8062   0.9024
  -0.750   0.1644   0.02561   0.01519  -0.0500   0.7979   0.9175
  -0.500   0.2147   0.02552   0.01496  -0.0544   0.7893   0.9311
  -0.250   0.2601   0.02546   0.01481  -0.0581   0.7795   0.9449
   0.000   0.3097   0.02524   0.01446  -0.0624   0.7713   0.9572
   0.250   0.3529   0.02520   0.01436  -0.0660   0.7601   0.9702
   0.500   0.3992   0.02503   0.01410  -0.0700   0.7506   0.9823
   0.750   0.4440   0.02488   0.01390  -0.0739   0.7404   0.9948
   1.000   0.4719   0.02489   0.01387  -0.0748   0.7289   1.0000
   1.250   0.4896   0.02487   0.01378  -0.0734   0.7187   1.0000
   1.500   0.5063   0.02491   0.01378  -0.0718   0.7081   1.0000
   1.750   0.5191   0.02511   0.01395  -0.0696   0.6966   1.0000
   2.000   0.5378   0.02516   0.01395  -0.0681   0.6870   1.0000
   2.250   0.5542   0.02532   0.01407  -0.0664   0.6766   1.0000
   2.500   0.5679   0.02560   0.01434  -0.0642   0.6656   1.0000
   2.750   0.5912   0.02560   0.01428  -0.0633   0.6572   1.0000
   3.000   0.6039   0.02598   0.01466  -0.0609   0.6459   1.0000
   3.250   0.6201   0.02628   0.01495  -0.0591   0.6358   1.0000
   3.500   0.6435   0.02635   0.01501  -0.0581   0.6272   1.0000
   3.750   0.6561   0.02684   0.01551  -0.0558   0.6162   1.0000
   4.000   0.6776   0.02703   0.01569  -0.0546   0.6074   1.0000
   4.250   0.6952   0.02739   0.01607  -0.0529   0.5975   1.0000
   4.500   0.7109   0.02784   0.01656  -0.0510   0.5875   1.0000
   4.750   0.7366   0.02793   0.01664  -0.0504   0.5794   1.0000
   5.000   0.7481   0.02858   0.01735  -0.0479   0.5686   1.0000
   5.250   0.7710   0.02881   0.01761  -0.0469   0.5602   1.0000
   5.500   0.7873   0.02930   0.01816  -0.0451   0.5503   1.0000
   5.750   0.8034   0.02984   0.01876  -0.0433   0.5408   1.0000
   6.000   0.8282   0.03003   0.01898  -0.0425   0.5325   1.0000
   6.250   0.8391   0.03080   0.01987  -0.0401   0.5223   1.0000
   6.500   0.8677   0.03087   0.01997  -0.0398   0.5147   1.0000
   6.750   0.8766   0.03176   0.02098  -0.0372   0.5042   1.0000
   7.000   0.8959   0.03226   0.02156  -0.0358   0.4955   1.0000
   7.250   0.9151   0.03275   0.02216  -0.0345   0.4865   1.0000
   7.500   0.9270   0.03360   0.02313  -0.0323   0.4771   1.0000
   7.750   0.9540   0.03378   0.02340  -0.0319   0.4692   1.0000
   8.000   0.9590   0.03497   0.02474  -0.0290   0.4592   1.0000
   8.250   0.9910   0.03498   0.02485  -0.0291   0.4520   1.0000
   8.500   0.9905   0.03643   0.02648  -0.0257   0.4418   1.0000
   8.750   1.0126   0.03692   0.02710  -0.0247   0.4340   1.0000
   9.000   1.0215   0.03791   0.02825  -0.0223   0.4244   1.0000
   9.250   1.0285   0.03878   0.02924  -0.0196   0.4133   1.0000
   9.500   1.0409   0.03888   0.02943  -0.0169   0.3996   1.0000
   9.750   1.0475   0.03908   0.02968  -0.0136   0.3845   1.0000
  10.000   1.0505   0.03956   0.03021  -0.0102   0.3695   1.0000
  10.250   1.0532   0.04029   0.03100  -0.0072   0.3550   1.0000
  10.500   1.0538   0.04128   0.03207  -0.0044   0.3405   1.0000
  10.750   1.0527   0.04258   0.03346  -0.0018   0.3258   1.0000
  11.000   1.0472   0.04439   0.03539   0.0005   0.3098   1.0000
  11.250   1.0391   0.04666   0.03777   0.0024   0.2922   1.0000
  11.500   1.0314   0.04908   0.04026   0.0039   0.2715   1.0000
  11.750   1.0238   0.05174   0.04295   0.0050   0.2480   1.0000
  12.000   1.0162   0.05463   0.04582   0.0058   0.2218   1.0000
  12.250   1.0063   0.05805   0.04918   0.0064   0.1910   1.0000
  12.500   0.9947   0.06178   0.05272   0.0067   0.1552   1.0000
  12.750   0.9804   0.06606   0.05673   0.0068   0.1262   1.0000
  13.000   0.9659   0.07066   0.06111   0.0065   0.1079   1.0000
  13.250   0.9531   0.07527   0.06556   0.0061   0.0964   1.0000
  13.500   0.9429   0.07970   0.06990   0.0055   0.0882   1.0000
  13.750   0.9354   0.08384   0.07398   0.0050   0.0821   1.0000
  14.000   0.9300   0.08778   0.07790   0.0045   0.0771   1.0000
  14.250   0.9261   0.09144   0.08149   0.0041   0.0733   1.0000
  14.500   0.9262   0.09467   0.08483   0.0039   0.0691   1.0000
  14.750   0.9262   0.09786   0.08801   0.0036   0.0656   1.0000
  15.000   0.9284   0.10063   0.09073   0.0035   0.0627   1.0000
  15.250   0.9336   0.10320   0.09346   0.0036   0.0601   1.0000
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