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UA(2)-180 smoothed (ua2-180sm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: UA(2)-180 smoothed (ua2-180sm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 145.34 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ua2-180sm-il-1000000-n5.txt
Download as CSV file: xf-ua2-180sm-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: UA(2)-180 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250   0.0480   0.09856   0.09443  -0.0966   0.4979   0.0083
 -11.000   0.0494   0.09488   0.09076  -0.0979   0.4975   0.0085
 -10.750   0.0354   0.08809   0.08400  -0.1002   0.4972   0.0091
 -10.500   0.0431   0.08605   0.08197  -0.1011   0.4966   0.0092
 -10.250   0.0504   0.08391   0.07984  -0.1020   0.4960   0.0093
 -10.000   0.0503   0.08046   0.07640  -0.1032   0.4956   0.0093
  -9.750   0.0517   0.07737   0.07334  -0.1044   0.4952   0.0094
  -9.500   0.0572   0.07511   0.07109  -0.1053   0.4945   0.0096
  -9.250   0.0581   0.07213   0.06813  -0.1064   0.4940   0.0097
  -9.000   0.0562   0.06880   0.06482  -0.1077   0.4936   0.0099
  -8.500  -0.1893   0.02940   0.02475  -0.1120   0.4946   0.0115
  -8.250  -0.1799   0.02763   0.02280  -0.1103   0.4939   0.0116
  -8.000  -0.1631   0.02670   0.02176  -0.1092   0.4932   0.0117
  -7.750  -0.1464   0.02564   0.02057  -0.1080   0.4924   0.0118
  -7.500  -0.1289   0.02460   0.01940  -0.1068   0.4916   0.0119
  -7.250  -0.1107   0.02356   0.01822  -0.1057   0.4908   0.0120
  -7.000  -0.0905   0.02278   0.01732  -0.1048   0.4899   0.0122
  -6.750  -0.0710   0.02180   0.01619  -0.1037   0.4890   0.0124
  -6.500  -0.0504   0.02085   0.01510  -0.1027   0.4886   0.0127
  -6.250  -0.0322   0.01926   0.01327  -0.1013   0.4883   0.0131
  -6.000  -0.0123   0.01786   0.01163  -0.1000   0.4879   0.0134
  -5.750   0.0097   0.01673   0.01029  -0.0990   0.4875   0.0137
  -5.500   0.0333   0.01593   0.00935  -0.0982   0.4870   0.0139
  -5.250   0.0581   0.01536   0.00866  -0.0977   0.4865   0.0140
  -5.000   0.0824   0.01467   0.00788  -0.0971   0.4859   0.0142
  -4.750   0.1079   0.01427   0.00744  -0.0967   0.4853   0.0144
  -4.500   0.1340   0.01399   0.00713  -0.0964   0.4846   0.0146
  -4.250   0.1602   0.01371   0.00682  -0.0960   0.4839   0.0148
  -4.000   0.1868   0.01350   0.00659  -0.0958   0.4833   0.0150
  -3.750   0.2131   0.01324   0.00629  -0.0955   0.4827   0.0153
  -3.500   0.2392   0.01292   0.00594  -0.0951   0.4821   0.0156
  -3.250   0.2654   0.01264   0.00562  -0.0948   0.4814   0.0159
  -3.000   0.2915   0.01237   0.00531  -0.0945   0.4808   0.0162
  -2.750   0.3176   0.01211   0.00502  -0.0941   0.4802   0.0164
  -2.500   0.3439   0.01191   0.00479  -0.0938   0.4795   0.0167
  -2.250   0.3703   0.01173   0.00458  -0.0935   0.4789   0.0169
  -2.000   0.3968   0.01157   0.00440  -0.0932   0.4783   0.0171
  -1.750   0.4222   0.01130   0.00412  -0.0927   0.4776   0.0174
  -1.500   0.4483   0.01114   0.00396  -0.0924   0.4770   0.0177
  -1.250   0.4747   0.01102   0.00383  -0.0922   0.4763   0.0181
  -1.000   0.5013   0.01094   0.00374  -0.0920   0.4755   0.0185
  -0.750   0.5279   0.01086   0.00365  -0.0918   0.4745   0.0191
  -0.500   0.5545   0.01081   0.00358  -0.0915   0.4735   0.0196
  -0.250   0.5813   0.01074   0.00351  -0.0914   0.4729   0.0201
   0.000   0.6084   0.01067   0.00344  -0.0913   0.4725   0.0204
   0.250   0.6351   0.01058   0.00336  -0.0911   0.4721   0.0208
   0.500   0.6619   0.01050   0.00329  -0.0910   0.4717   0.0214
   0.750   0.6889   0.01045   0.00325  -0.0909   0.4711   0.0221
   1.000   0.7160   0.01041   0.00322  -0.0908   0.4702   0.0231
   1.250   0.7430   0.01036   0.00319  -0.0907   0.4689   0.0240
   1.500   0.7699   0.01032   0.00315  -0.0906   0.4676   0.0252
   1.750   0.7969   0.01028   0.00312  -0.0905   0.4662   0.0267
   2.250   0.8429   0.00961   0.00316  -0.0891   0.4639   0.3241
   2.500   0.8590   0.00896   0.00323  -0.0872   0.4627   0.5989
   2.750   0.8673   0.00831   0.00333  -0.0831   0.4615   0.8529
   3.250   1.0000   0.00855   0.00370  -0.0999   0.4575   0.9836
   3.500   1.0437   0.00863   0.00377  -0.1035   0.4560   0.9892
   3.750   1.0838   0.00872   0.00385  -0.1064   0.4541   0.9940
   4.000   1.1221   0.00877   0.00389  -0.1089   0.4522   0.9963
   4.250   1.1580   0.00883   0.00394  -0.1109   0.4504   0.9981
   4.500   1.1929   0.00890   0.00400  -0.1127   0.4486   0.9996
   4.750   1.2197   0.00897   0.00405  -0.1128   0.4468   1.0000
   5.000   1.2410   0.00906   0.00412  -0.1118   0.4448   1.0000
   5.250   1.2629   0.00915   0.00421  -0.1108   0.4434   1.0000
   5.500   1.2857   0.00922   0.00430  -0.1101   0.4418   1.0000
   5.750   1.3082   0.00929   0.00439  -0.1093   0.4399   1.0000
   6.000   1.3304   0.00937   0.00448  -0.1084   0.4376   1.0000
   6.250   1.3520   0.00946   0.00457  -0.1075   0.4348   1.0000
   6.500   1.3724   0.00956   0.00466  -0.1063   0.4316   1.0000
   6.750   1.3932   0.00967   0.00477  -0.1052   0.4290   1.0000
   7.000   1.4151   0.00977   0.00489  -0.1044   0.4262   1.0000
   7.250   1.4360   0.00988   0.00501  -0.1034   0.4225   1.0000
   7.500   1.4551   0.01002   0.00515  -0.1020   0.4182   1.0000
   7.750   1.4742   0.01017   0.00530  -0.1006   0.4139   1.0000
   8.000   1.4921   0.01033   0.00546  -0.0991   0.4077   1.0000
   8.250   1.5039   0.01053   0.00565  -0.0963   0.4003   1.0000
   8.500   1.5152   0.01080   0.00589  -0.0935   0.3906   1.0000
   8.750   1.5268   0.01112   0.00618  -0.0910   0.3813   1.0000
   9.000   1.5370   0.01154   0.00656  -0.0883   0.3717   1.0000
   9.250   1.5463   0.01204   0.00703  -0.0856   0.3617   1.0000
   9.500   1.5578   0.01253   0.00752  -0.0834   0.3534   1.0000
   9.750   1.5661   0.01319   0.00815  -0.0809   0.3450   1.0000
  10.000   1.5769   0.01381   0.00877  -0.0789   0.3370   1.0000
  10.250   1.5837   0.01466   0.00960  -0.0766   0.3284   1.0000
  10.500   1.5938   0.01544   0.01040  -0.0748   0.3217   1.0000
  10.750   1.5994   0.01653   0.01148  -0.0728   0.3143   1.0000
  11.000   1.6082   0.01754   0.01251  -0.0713   0.3080   1.0000
  11.250   1.6108   0.01901   0.01398  -0.0694   0.3017   1.0000
  11.500   1.6186   0.02025   0.01527  -0.0682   0.2960   1.0000
  11.750   1.6203   0.02200   0.01704  -0.0666   0.2901   1.0000
  12.000   1.6209   0.02393   0.01900  -0.0652   0.2853   1.0000
  12.250   1.6210   0.02601   0.02112  -0.0639   0.2795   1.0000
  12.500   1.6098   0.02915   0.02429  -0.0623   0.2733   1.0000
  12.750   1.6082   0.03161   0.02682  -0.0613   0.2692   1.0000
  13.000   1.6022   0.03449   0.02974  -0.0602   0.2642   1.0000
  13.250   1.5895   0.03801   0.03330  -0.0588   0.2594   1.0000
  13.500   1.5839   0.04088   0.03622  -0.0578   0.2556   1.0000
  13.750   1.5814   0.04344   0.03883  -0.0570   0.2520   1.0000
  14.000   1.5743   0.04645   0.04186  -0.0560   0.2473   1.0000
  14.250   1.5651   0.04969   0.04512  -0.0550   0.2428   1.0000
  14.500   1.5673   0.05187   0.04735  -0.0544   0.2389   1.0000
  14.750   1.5636   0.05465   0.05015  -0.0538   0.2340   1.0000
  15.000   1.5614   0.05731   0.05281  -0.0532   0.2299   1.0000
  15.250   1.5635   0.05957   0.05512  -0.0527   0.2266   1.0000
  15.500   1.5672   0.06168   0.05726  -0.0524   0.2225   1.0000
  15.750   1.5694   0.06395   0.05955  -0.0520   0.2186   1.0000
  16.000   1.5668   0.06676   0.06237  -0.0516   0.2140   1.0000
  16.250   1.5712   0.06884   0.06447  -0.0514   0.2090   1.0000
  16.500   1.5745   0.07101   0.06666  -0.0511   0.2050   1.0000
  16.750   1.5734   0.07370   0.06936  -0.0508   0.2005   1.0000
  17.000   1.5791   0.07569   0.07139  -0.0508   0.1972   1.0000
  17.250   1.5827   0.07789   0.07362  -0.0506   0.1927   1.0000
  17.500   1.5808   0.08070   0.07641  -0.0504   0.1866   1.0000
  17.750   1.5809   0.08332   0.07905  -0.0503   0.1800   1.0000
  18.000   1.5746   0.08665   0.08234  -0.0502   0.1703   1.0000
  18.250   1.5673   0.09018   0.08584  -0.0501   0.1611   1.0000
  18.500   1.5613   0.09357   0.08921  -0.0501   0.1508   1.0000
  18.750   1.5571   0.09675   0.09237  -0.0501   0.1417   1.0000
  19.000   1.5468   0.10072   0.09631  -0.0502   0.1317   1.0000
  19.250   1.5372   0.10463   0.10018  -0.0504   0.1205   1.0000
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