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GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GEMINI (smoothed) (geminism-il)
Reynolds number: 200,000
Max Cl/Cd: 65.44 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-geminism-il-200000-n5.txt
Download as CSV file: xf-geminism-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.7581   0.06691   0.06233  -0.0680   1.0000   0.0218
 -13.750  -0.7831   0.06012   0.05532  -0.0720   1.0000   0.0218
 -13.500  -0.8018   0.05493   0.04993  -0.0744   1.0000   0.0220
 -13.250  -0.8168   0.05071   0.04551  -0.0756   1.0000   0.0222
 -13.000  -0.8295   0.04719   0.04178  -0.0758   1.0000   0.0224
 -12.750  -0.8402   0.04421   0.03860  -0.0750   1.0000   0.0227
 -12.500  -0.8493   0.04166   0.03586  -0.0734   1.0000   0.0230
 -12.250  -0.8569   0.03948   0.03347  -0.0711   1.0000   0.0233
 -12.000  -0.8636   0.03761   0.03140  -0.0680   1.0000   0.0237
 -11.750  -0.8695   0.03604   0.02962  -0.0644   1.0000   0.0241
 -11.500  -0.8755   0.03476   0.02816  -0.0600   1.0000   0.0244
 -11.250  -0.8789   0.03364   0.02701  -0.0558   1.0000   0.0248
 -11.000  -0.8786   0.03277   0.02611  -0.0521   1.0000   0.0252
 -10.750  -0.8779   0.03203   0.02535  -0.0482   1.0000   0.0257
 -10.250  -0.8451   0.02998   0.02308  -0.0467   0.9941   0.0274
 -10.000  -0.8186   0.02863   0.02153  -0.0477   0.9880   0.0286
  -9.750  -0.7910   0.02732   0.01999  -0.0487   0.9828   0.0296
  -9.500  -0.7617   0.02599   0.01859  -0.0502   0.9791   0.0307
  -9.250  -0.7341   0.02510   0.01766  -0.0511   0.9728   0.0320
  -9.000  -0.7029   0.02419   0.01666  -0.0526   0.9684   0.0336
  -8.750  -0.6762   0.02329   0.01564  -0.0531   0.9603   0.0351
  -8.500  -0.6450   0.02240   0.01460  -0.0543   0.9548   0.0365
  -8.250  -0.6189   0.02141   0.01362  -0.0548   0.9468   0.0382
  -8.000  -0.5884   0.02068   0.01285  -0.0560   0.9404   0.0403
  -7.750  -0.5592   0.01997   0.01205  -0.0568   0.9327   0.0425
  -7.500  -0.5292   0.01930   0.01126  -0.0576   0.9253   0.0443
  -7.250  -0.5027   0.01850   0.01046  -0.0579   0.9162   0.0470
  -7.000  -0.4761   0.01796   0.00987  -0.0581   0.9064   0.0501
  -6.500  -0.4230   0.01682   0.00861  -0.0582   0.8870   0.0572
  -6.250  -0.3968   0.01637   0.00808  -0.0581   0.8771   0.0624
  -6.000  -0.3707   0.01586   0.00753  -0.0579   0.8677   0.0687
  -5.750  -0.3466   0.01547   0.00708  -0.0573   0.8570   0.0765
  -5.500  -0.3221   0.01500   0.00660  -0.0569   0.8474   0.0887
  -5.250  -0.2992   0.01450   0.00617  -0.0561   0.8372   0.1099
  -5.000  -0.2780   0.01396   0.00582  -0.0551   0.8271   0.1521
  -4.750  -0.2546   0.01353   0.00550  -0.0544   0.8180   0.1980
  -4.500  -0.2327   0.01319   0.00525  -0.0534   0.8077   0.2344
  -4.250  -0.2097   0.01287   0.00501  -0.0525   0.7986   0.2704
  -4.000  -0.1876   0.01254   0.00478  -0.0515   0.7891   0.3083
  -3.750  -0.1661   0.01223   0.00459  -0.0503   0.7797   0.3514
  -3.500  -0.1442   0.01194   0.00442  -0.0492   0.7710   0.3994
  -3.250  -0.1239   0.01167   0.00432  -0.0476   0.7615   0.4510
  -3.000  -0.1027   0.01144   0.00423  -0.0462   0.7532   0.5049
  -2.750  -0.0814   0.01127   0.00419  -0.0448   0.7439   0.5494
  -2.500  -0.0580   0.01116   0.00411  -0.0437   0.7356   0.5822
  -2.250  -0.0339   0.01109   0.00403  -0.0428   0.7267   0.6047
  -2.000  -0.0090   0.01103   0.00396  -0.0421   0.7183   0.6250
  -1.750   0.0157   0.01098   0.00389  -0.0413   0.7095   0.6449
  -1.500   0.0406   0.01093   0.00384  -0.0406   0.7009   0.6639
  -1.250   0.0658   0.01089   0.00378  -0.0399   0.6922   0.6827
  -1.000   0.0910   0.01086   0.00376  -0.0392   0.6835   0.7013
  -0.750   0.1167   0.01084   0.00371  -0.0386   0.6750   0.7196
  -0.500   0.1421   0.01082   0.00371  -0.0380   0.6659   0.7382
  -0.250   0.1683   0.01082   0.00369  -0.0375   0.6576   0.7582
   0.000   0.1948   0.01080   0.00373  -0.0371   0.6480   0.7806
   0.250   0.2220   0.01082   0.00377  -0.0367   0.6394   0.8074
   0.500   0.2518   0.01086   0.00384  -0.0369   0.6299   0.8313
   0.750   0.2821   0.01091   0.00389  -0.0373   0.6207   0.8500
   1.000   0.3137   0.01099   0.00393  -0.0380   0.6114   0.8663
   1.250   0.3466   0.01107   0.00401  -0.0391   0.6014   0.8815
   1.500   0.3805   0.01118   0.00407  -0.0404   0.5920   0.8954
   1.750   0.4142   0.01129   0.00415  -0.0416   0.5817   0.9085
   2.000   0.4491   0.01141   0.00425  -0.0432   0.5715   0.9202
   2.250   0.4859   0.01155   0.00433  -0.0452   0.5616   0.9295
   2.500   0.5200   0.01168   0.00444  -0.0466   0.5510   0.9398
   2.750   0.5567   0.01183   0.00456  -0.0486   0.5406   0.9478
   3.000   0.5932   0.01199   0.00466  -0.0506   0.5305   0.9549
   3.250   0.6294   0.01215   0.00481  -0.0526   0.5195   0.9617
   3.500   0.6653   0.01232   0.00496  -0.0545   0.5093   0.9678
   3.750   0.7003   0.01251   0.00511  -0.0562   0.4992   0.9743
   4.000   0.7357   0.01269   0.00529  -0.0581   0.4885   0.9808
   4.250   0.7694   0.01289   0.00548  -0.0596   0.4786   0.9884
   4.500   0.8036   0.01311   0.00567  -0.0613   0.4687   0.9953
   4.750   0.8397   0.01330   0.00588  -0.0634   0.4583   1.0000
   5.000   0.8581   0.01347   0.00604  -0.0618   0.4501   1.0000
   5.250   0.8768   0.01364   0.00622  -0.0602   0.4413   1.0000
   5.500   0.8954   0.01384   0.00642  -0.0585   0.4332   1.0000
   5.750   0.9141   0.01404   0.00663  -0.0569   0.4248   1.0000
   6.000   0.9325   0.01426   0.00685  -0.0553   0.4155   1.0000
   6.250   0.9496   0.01451   0.00707  -0.0533   0.4043   1.0000
   6.500   0.9664   0.01477   0.00732  -0.0514   0.3909   1.0000
   6.750   0.9832   0.01503   0.00758  -0.0494   0.3772   1.0000
   7.000   1.0003   0.01531   0.00787  -0.0475   0.3650   1.0000
   7.250   1.0164   0.01562   0.00817  -0.0454   0.3517   1.0000
   7.500   1.0316   0.01595   0.00849  -0.0432   0.3368   1.0000
   7.750   1.0465   0.01631   0.00884  -0.0409   0.3226   1.0000
   8.000   1.0602   0.01670   0.00921  -0.0385   0.3062   1.0000
   8.250   1.0722   0.01715   0.00961  -0.0358   0.2875   1.0000
   8.500   1.0809   0.01771   0.01009  -0.0326   0.2649   1.0000
   8.750   1.0866   0.01831   0.01061  -0.0288   0.2409   1.0000
   9.000   1.0889   0.01905   0.01122  -0.0247   0.2135   1.0000
   9.250   1.0872   0.02011   0.01207  -0.0202   0.1783   1.0000
   9.500   1.0793   0.02166   0.01330  -0.0154   0.1276   1.0000
  10.000   1.0603   0.02564   0.01673  -0.0070   0.0501   1.0000
  10.250   1.0636   0.02710   0.01820  -0.0047   0.0438   1.0000
  10.500   1.0705   0.02839   0.01958  -0.0029   0.0399   1.0000
  10.750   1.0750   0.02992   0.02117  -0.0011   0.0370   1.0000
  11.000   1.0786   0.03161   0.02293   0.0005   0.0348   1.0000
  11.250   1.0845   0.03319   0.02463   0.0018   0.0328   1.0000
  11.500   1.0885   0.03500   0.02653   0.0030   0.0310   1.0000
  11.750   1.0894   0.03715   0.02874   0.0041   0.0295   1.0000
  12.000   1.0888   0.03953   0.03121   0.0051   0.0282   1.0000
  12.250   1.0916   0.04168   0.03350   0.0059   0.0271   1.0000
  12.500   1.0924   0.04410   0.03601   0.0065   0.0261   1.0000
  12.750   1.0922   0.04668   0.03869   0.0070   0.0252   1.0000
  13.000   1.0911   0.04944   0.04154   0.0073   0.0244   1.0000
  13.250   1.0889   0.05240   0.04457   0.0076   0.0238   1.0000
  13.500   1.0846   0.05567   0.04790   0.0077   0.0232   1.0000
  13.750   1.0832   0.05869   0.05100   0.0077   0.0226   1.0000
  14.000   1.0840   0.06151   0.05394   0.0077   0.0220   1.0000
  14.250   1.0848   0.06440   0.05692   0.0075   0.0213   1.0000
  14.500   1.0856   0.06732   0.05992   0.0073   0.0206   1.0000
  14.750   1.0865   0.07027   0.06296   0.0070   0.0199   1.0000
  15.000   1.0873   0.07327   0.06601   0.0067   0.0194   1.0000
  15.250   1.0878   0.07630   0.06909   0.0063   0.0189   1.0000
  15.500   1.0882   0.07930   0.07212   0.0060   0.0185   1.0000
  15.750   1.0905   0.08204   0.07492   0.0059   0.0182   1.0000
  16.000   1.0936   0.08473   0.07773   0.0057   0.0178   1.0000
  16.250   1.0969   0.08740   0.08050   0.0055   0.0174   1.0000
  16.500   1.1003   0.09008   0.08327   0.0053   0.0170   1.0000
  16.750   1.1034   0.09282   0.08611   0.0049   0.0166   1.0000
  17.000   1.1063   0.09563   0.08902   0.0045   0.0163   1.0000
  17.250   1.1086   0.09859   0.09208   0.0039   0.0160   1.0000
  17.500   1.1102   0.10167   0.09524   0.0032   0.0157   1.0000
  17.750   1.1114   0.10487   0.09852   0.0023   0.0154   1.0000
  18.000   1.1126   0.10808   0.10180   0.0013   0.0151   1.0000
  18.250   1.1139   0.11127   0.10504   0.0003   0.0148   1.0000
  18.500   1.1156   0.11429   0.10810  -0.0006   0.0146   1.0000
  18.750   1.1123   0.11851   0.11251  -0.0022   0.0143   1.0000
  19.000   1.1083   0.12289   0.11707  -0.0040   0.0141   1.0000
  19.250   1.1034   0.12749   0.12185  -0.0060   0.0139   1.0000
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