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RUTAN WING AIRFOIL (amsoil2-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: RUTAN WING AIRFOIL (amsoil2-il)
Reynolds number: 500,000
Max Cl/Cd: 56.86 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-amsoil2-il-500000.txt
Download as CSV file: xf-amsoil2-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RUTAN WING AIRFOIL                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.4508   0.15542   0.15303  -0.0004   1.0000   0.0333
 -15.000  -0.4484   0.15309   0.15070  -0.0015   1.0000   0.0342
 -14.500  -1.0544   0.06083   0.05728  -0.0441   1.0000   0.0274
 -14.000  -1.1080   0.04831   0.04427  -0.0495   1.0000   0.0276
 -13.750  -1.1196   0.04458   0.04039  -0.0497   1.0000   0.0278
 -13.500  -1.1203   0.04225   0.03799  -0.0492   1.0000   0.0281
 -13.250  -1.1185   0.04040   0.03605  -0.0484   1.0000   0.0283
 -13.000  -1.1155   0.03879   0.03436  -0.0472   1.0000   0.0286
 -12.750  -1.1130   0.03726   0.03272  -0.0454   1.0000   0.0289
 -12.500  -1.1071   0.03578   0.03113  -0.0438   1.0000   0.0292
 -12.250  -1.0983   0.03417   0.02937  -0.0425   1.0000   0.0296
 -12.000  -1.0883   0.03247   0.02748  -0.0412   1.0000   0.0301
 -11.750  -1.0767   0.03077   0.02555  -0.0400   1.0000   0.0306
 -11.500  -1.0628   0.02925   0.02379  -0.0389   1.0000   0.0312
 -11.250  -1.0462   0.02811   0.02241  -0.0379   1.0000   0.0316
 -11.000  -1.0297   0.02608   0.02031  -0.0372   1.0000   0.0323
 -10.750  -1.0083   0.02531   0.01953  -0.0368   1.0000   0.0329
 -10.500  -0.9864   0.02464   0.01881  -0.0364   1.0000   0.0335
 -10.250  -0.9644   0.02388   0.01798  -0.0359   1.0000   0.0343
 -10.000  -0.9426   0.02302   0.01698  -0.0354   1.0000   0.0351
  -9.750  -0.9206   0.02221   0.01602  -0.0348   1.0000   0.0358
  -9.500  -0.9007   0.02107   0.01477  -0.0340   1.0000   0.0365
  -9.250  -0.8855   0.02028   0.01399  -0.0322   1.0000   0.0372
  -9.000  -0.8589   0.01969   0.01339  -0.0325   0.9975   0.0381
  -8.750  -0.8247   0.01909   0.01274  -0.0343   0.9946   0.0392
  -8.500  -0.7913   0.01849   0.01205  -0.0358   0.9905   0.0405
  -8.250  -0.7584   0.01778   0.01123  -0.0373   0.9860   0.0415
  -8.000  -0.7266   0.01685   0.01032  -0.0386   0.9816   0.0427
  -7.750  -0.6962   0.01636   0.00983  -0.0395   0.9750   0.0439
  -7.500  -0.6660   0.01594   0.00936  -0.0401   0.9690   0.0453
  -7.250  -0.6393   0.01560   0.00894  -0.0399   0.9607   0.0466
  -7.000  -0.6152   0.01491   0.00824  -0.0394   0.9533   0.0480
  -6.750  -0.5913   0.01452   0.00785  -0.0386   0.9455   0.0493
  -6.500  -0.5668   0.01421   0.00752  -0.0380   0.9386   0.0509
  -6.250  -0.5418   0.01393   0.00719  -0.0373   0.9313   0.0526
  -6.000  -0.5182   0.01348   0.00670  -0.0365   0.9252   0.0543
  -5.750  -0.4926   0.01310   0.00634  -0.0361   0.9186   0.0563
  -5.500  -0.4670   0.01282   0.00605  -0.0356   0.9128   0.0585
  -5.250  -0.4408   0.01262   0.00578  -0.0352   0.9076   0.0607
  -5.000  -0.4150   0.01217   0.00538  -0.0349   0.9015   0.0640
  -4.750  -0.3886   0.01194   0.00513  -0.0346   0.8959   0.0672
  -4.500  -0.3627   0.01161   0.00480  -0.0342   0.8908   0.0711
  -4.250  -0.3351   0.01138   0.00460  -0.0341   0.8851   0.0758
  -4.000  -0.3083   0.01110   0.00432  -0.0339   0.8795   0.0813
  -3.750  -0.2814   0.01093   0.00413  -0.0336   0.8746   0.0871
  -3.500  -0.2537   0.01065   0.00391  -0.0336   0.8694   0.0944
  -3.250  -0.2257   0.01045   0.00372  -0.0336   0.8642   0.1024
  -3.000  -0.1982   0.01024   0.00355  -0.0335   0.8595   0.1124
  -2.750  -0.1706   0.01003   0.00339  -0.0334   0.8549   0.1255
  -2.500  -0.1423   0.00979   0.00324  -0.0336   0.8499   0.1440
  -2.250  -0.1145   0.00950   0.00309  -0.0336   0.8450   0.1771
  -2.000  -0.0876   0.00901   0.00291  -0.0337   0.8407   0.2526
  -1.750  -0.0637   0.00775   0.00265  -0.0337   0.8362   0.5143
  -1.500  -0.0372   0.00729   0.00268  -0.0335   0.8311   0.6427
  -1.250  -0.0093   0.00719   0.00271  -0.0333   0.8263   0.6905
  -1.000   0.0188   0.00716   0.00274  -0.0330   0.8222   0.7200
  -0.750   0.0470   0.00717   0.00280  -0.0329   0.8177   0.7432
  -0.500   0.0752   0.00714   0.00281  -0.0326   0.8101   0.7629
  -0.250   0.1025   0.00714   0.00278  -0.0320   0.8019   0.7791
   0.000   0.1305   0.00709   0.00278  -0.0317   0.7922   0.7920
   0.250   0.1581   0.00708   0.00272  -0.0312   0.7814   0.8048
   0.500   0.1857   0.00705   0.00272  -0.0308   0.7705   0.8170
   0.750   0.2133   0.00705   0.00273  -0.0304   0.7616   0.8281
   1.000   0.2410   0.00706   0.00275  -0.0300   0.7512   0.8411
   1.250   0.2674   0.00708   0.00281  -0.0292   0.7405   0.8550
   1.500   0.2944   0.00708   0.00279  -0.0287   0.7265   0.8634
   1.750   0.3221   0.00708   0.00276  -0.0284   0.7080   0.8699
   2.000   0.3502   0.00710   0.00273  -0.0282   0.6853   0.8766
   2.250   0.3766   0.00714   0.00272  -0.0276   0.6578   0.8829
   2.500   0.4032   0.00728   0.00272  -0.0271   0.6147   0.8904
   2.750   0.4265   0.00772   0.00278  -0.0261   0.5201   0.8973
   3.000   0.4426   0.00920   0.00326  -0.0246   0.2871   0.9053
   3.250   0.4643   0.00999   0.00360  -0.0238   0.1879   0.9129
   3.500   0.4879   0.01038   0.00383  -0.0229   0.1506   0.9211
   3.750   0.5119   0.01071   0.00404  -0.0222   0.1280   0.9297
   4.000   0.5355   0.01098   0.00424  -0.0213   0.1136   0.9393
   4.250   0.5594   0.01120   0.00443  -0.0204   0.1034   0.9490
   4.500   0.5844   0.01142   0.00464  -0.0197   0.0955   0.9599
   4.750   0.6113   0.01175   0.00491  -0.0196   0.0883   0.9715
   5.000   0.6435   0.01201   0.00517  -0.0207   0.0827   0.9818
   5.250   0.6774   0.01243   0.00554  -0.0222   0.0770   0.9917
   5.500   0.7096   0.01273   0.00582  -0.0234   0.0727   1.0000
   5.750   0.7335   0.01324   0.00628  -0.0231   0.0688   1.0000
   6.000   0.7604   0.01351   0.00656  -0.0231   0.0659   1.0000
   6.250   0.7865   0.01388   0.00689  -0.0230   0.0630   1.0000
   6.500   0.8107   0.01447   0.00746  -0.0227   0.0603   1.0000
   6.750   0.8369   0.01480   0.00781  -0.0225   0.0582   1.0000
   7.000   0.8626   0.01517   0.00816  -0.0223   0.0560   1.0000
   7.250   0.8857   0.01583   0.00877  -0.0218   0.0538   1.0000
   7.500   0.9107   0.01626   0.00924  -0.0214   0.0523   1.0000
   7.750   0.9358   0.01665   0.00966  -0.0211   0.0505   1.0000
   8.000   0.9604   0.01707   0.01006  -0.0207   0.0489   1.0000
   8.250   0.9824   0.01782   0.01077  -0.0200   0.0473   1.0000
   8.500   1.0061   0.01835   0.01136  -0.0195   0.0461   1.0000
   8.750   1.0299   0.01884   0.01190  -0.0190   0.0448   1.0000
   9.000   1.0534   0.01931   0.01239  -0.0184   0.0434   1.0000
   9.250   1.0760   0.01984   0.01290  -0.0178   0.0422   1.0000
   9.500   1.0966   0.02080   0.01386  -0.0170   0.0410   1.0000
   9.750   1.1191   0.02133   0.01449  -0.0163   0.0400   1.0000
  10.000   1.1408   0.02195   0.01517  -0.0156   0.0390   1.0000
  10.250   1.1620   0.02255   0.01581  -0.0148   0.0380   1.0000
  10.500   1.1825   0.02320   0.01646  -0.0139   0.0372   1.0000
  10.750   1.2013   0.02434   0.01759  -0.0130   0.0362   1.0000
  11.000   1.2203   0.02515   0.01851  -0.0119   0.0355   1.0000
  11.250   1.2385   0.02587   0.01935  -0.0108   0.0347   1.0000
  11.500   1.2547   0.02662   0.02018  -0.0093   0.0339   1.0000
  11.750   1.2697   0.02738   0.02100  -0.0077   0.0332   1.0000
  12.000   1.2844   0.02820   0.02185  -0.0062   0.0326   1.0000
  12.250   1.2987   0.02919   0.02286  -0.0048   0.0321   1.0000
  12.500   1.3116   0.03094   0.02467  -0.0035   0.0314   1.0000
  12.750   1.3219   0.03203   0.02593  -0.0017   0.0310   1.0000
  13.000   1.3312   0.03332   0.02738   0.0000   0.0306   1.0000
  13.250   1.3397   0.03473   0.02894   0.0016   0.0301   1.0000
  13.500   1.3472   0.03622   0.03056   0.0032   0.0297   1.0000
  13.750   1.3535   0.03779   0.03226   0.0046   0.0292   1.0000
  14.000   1.3596   0.03937   0.03395   0.0059   0.0289   1.0000
  14.250   1.3656   0.04095   0.03560   0.0071   0.0285   1.0000
  14.500   1.3714   0.04262   0.03733   0.0081   0.0282   1.0000
  14.750   1.3760   0.04449   0.03925   0.0090   0.0278   1.0000
  15.000   1.3760   0.04708   0.04192   0.0100   0.0275   1.0000
  15.250   1.3680   0.05048   0.04551   0.0108   0.0272   1.0000
  15.500   1.3602   0.05379   0.04903   0.0112   0.0271   1.0000
  15.750   1.3493   0.05766   0.05312   0.0111   0.0269   1.0000
  16.000   1.3353   0.06215   0.05783   0.0104   0.0268   1.0000
  16.250   1.3175   0.06745   0.06335   0.0089   0.0267   1.0000
  16.500   1.2955   0.07379   0.06992   0.0065   0.0266   1.0000
  16.750   1.2683   0.08170   0.07808   0.0025   0.0265   1.0000
  17.000   1.2320   0.09217   0.08881  -0.0037   0.0266   1.0000
  17.250   1.1720   0.10929   0.10626  -0.0151   0.0268   1.0000
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