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UA(2)-180 smoothed (ua2-180sm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: UA(2)-180 smoothed (ua2-180sm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 146.44 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ua2-180sm-il-1000000.txt
Download as CSV file: xf-ua2-180sm-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000   0.0580   0.09818   0.09417  -0.0987   0.5178   0.0146
 -10.750   0.0613   0.09478   0.09079  -0.1001   0.5173   0.0146
 -10.500   0.0611   0.09070   0.08673  -0.1014   0.5168   0.0147
 -10.250   0.0658   0.08780   0.08384  -0.1023   0.5163   0.0148
 -10.000   0.0750   0.08599   0.08205  -0.1026   0.5157   0.0150
  -9.750   0.0843   0.08416   0.08022  -0.1030   0.5150   0.0151
  -9.500   0.0877   0.08129   0.07737  -0.1040   0.5145   0.0152
  -9.250   0.0940   0.07908   0.07517  -0.1047   0.5139   0.0154
  -9.000   0.0971   0.07633   0.07244  -0.1056   0.5133   0.0155
  -8.750   0.1006   0.07379   0.06991  -0.1065   0.5128   0.0160
  -8.500   0.1017   0.07089   0.06704  -0.1076   0.5122   0.0165
  -8.250   0.1005   0.06774   0.06391  -0.1088   0.5117   0.0165
  -7.000   0.0017   0.03854   0.03435  -0.1143   0.5098   0.0181
  -6.750   0.0117   0.03682   0.03255  -0.1133   0.5091   0.0182
  -6.500   0.0274   0.03601   0.03171  -0.1126   0.5083   0.0184
  -6.250   0.0399   0.03429   0.02989  -0.1115   0.5076   0.0186
  -6.000   0.0538   0.03265   0.02812  -0.1104   0.5066   0.0189
  -5.750   0.0686   0.03099   0.02632  -0.1093   0.5056   0.0194
  -5.500   0.0765   0.02825   0.02289  -0.1054   0.5045   0.0213
  -5.250   0.0855   0.02444   0.01888  -0.1036   0.5035   0.0218
  -5.000   0.1073   0.02333   0.01773  -0.1030   0.5032   0.0220
  -4.750   0.1297   0.02245   0.01681  -0.1024   0.5028   0.0224
  -4.500   0.1521   0.02153   0.01579  -0.1017   0.5024   0.0228
  -4.250   0.1749   0.02063   0.01477  -0.1009   0.5019   0.0237
  -4.000   0.1948   0.01925   0.01297  -0.0991   0.5015   0.0259
  -3.750   0.2199   0.01840   0.01215  -0.0988   0.5009   0.0265
  -3.500   0.2451   0.01775   0.01145  -0.0984   0.5003   0.0272
  -3.250   0.2707   0.01729   0.01085  -0.0979   0.4997   0.0288
  -3.000   0.2963   0.01553   0.00882  -0.0968   0.4991   0.0244
  -2.750   0.3224   0.01453   0.00774  -0.0963   0.4985   0.0234
  -2.500   0.3488   0.01382   0.00695  -0.0958   0.4978   0.0228
  -2.250   0.3755   0.01349   0.00659  -0.0956   0.4971   0.0233
  -2.000   0.4020   0.01314   0.00621  -0.0953   0.4963   0.0237
  -1.750   0.4284   0.01280   0.00585  -0.0949   0.4955   0.0241
  -1.500   0.4546   0.01252   0.00555  -0.0946   0.4947   0.0243
  -1.250   0.4809   0.01229   0.00530  -0.0943   0.4940   0.0246
  -1.000   0.5074   0.01211   0.00511  -0.0940   0.4933   0.0249
  -0.750   0.5342   0.01198   0.00496  -0.0938   0.4927   0.0252
  -0.500   0.5600   0.01176   0.00473  -0.0934   0.4920   0.0256
  -0.250   0.5855   0.01153   0.00449  -0.0930   0.4913   0.0265
   0.000   0.6124   0.01146   0.00442  -0.0929   0.4904   0.0275
   0.250   0.6395   0.01144   0.00438  -0.0928   0.4893   0.0284
   0.500   0.6668   0.01154   0.00446  -0.0928   0.4879   0.0292
   0.750   0.6938   0.01153   0.00445  -0.0927   0.4870   0.0301
   1.000   0.7204   0.01139   0.00433  -0.0925   0.4863   0.0319
   1.250   0.7472   0.01130   0.00425  -0.0923   0.4855   0.0343
   1.500   0.7738   0.01122   0.00422  -0.0922   0.4846   0.0445
   1.750   0.7852   0.00999   0.00428  -0.0896   0.4838   0.5372
   2.000   0.8435   0.00911   0.00455  -0.0961   0.4826   0.9605
   2.250   0.8902   0.00925   0.00466  -0.1000   0.4813   0.9816
   2.500   0.9479   0.00935   0.00471  -0.1064   0.4800   0.9887
   2.750   0.9959   0.00941   0.00472  -0.1108   0.4785   0.9940
   3.000   1.0477   0.00940   0.00466  -0.1161   0.4770   0.9975
   3.250   1.0921   0.00941   0.00462  -0.1199   0.4754   1.0000
   3.500   1.1147   0.00949   0.00467  -0.1191   0.4738   1.0000
   3.750   1.1378   0.00968   0.00483  -0.1184   0.4718   1.0000
   4.000   1.1599   0.00969   0.00485  -0.1175   0.4711   1.0000
   4.250   1.1820   0.00972   0.00489  -0.1166   0.4702   1.0000
   4.500   1.2043   0.00975   0.00494  -0.1157   0.4690   1.0000
   4.750   1.2267   0.00979   0.00499  -0.1149   0.4678   1.0000
   5.000   1.2491   0.00982   0.00503  -0.1140   0.4663   1.0000
   5.250   1.2717   0.00986   0.00508  -0.1132   0.4649   1.0000
   5.500   1.2943   0.00990   0.00511  -0.1124   0.4635   1.0000
   5.750   1.3169   0.00994   0.00515  -0.1116   0.4621   1.0000
   6.000   1.3393   0.00999   0.00520  -0.1108   0.4607   1.0000
   6.250   1.3617   0.01008   0.00527  -0.1100   0.4588   1.0000
   6.500   1.3843   0.01021   0.00539  -0.1093   0.4567   1.0000
   6.750   1.4057   0.01024   0.00548  -0.1083   0.4554   1.0000
   7.000   1.4274   0.01029   0.00556  -0.1074   0.4537   1.0000
   7.250   1.4490   0.01034   0.00563  -0.1065   0.4518   1.0000
   7.500   1.4705   0.01038   0.00571  -0.1055   0.4497   1.0000
   7.750   1.4916   0.01043   0.00576  -0.1045   0.4475   1.0000
   8.000   1.5117   0.01050   0.00583  -0.1033   0.4450   1.0000
   8.250   1.5315   0.01061   0.00594  -0.1021   0.4422   1.0000
   8.500   1.5519   0.01068   0.00607  -0.1011   0.4396   1.0000
   8.750   1.5722   0.01076   0.00619  -0.1000   0.4365   1.0000
   9.000   1.5889   0.01085   0.00630  -0.0982   0.4331   1.0000
   9.250   1.6022   0.01098   0.00642  -0.0957   0.4296   1.0000
   9.500   1.6199   0.01110   0.00659  -0.0942   0.4259   1.0000
   9.750   1.6372   0.01124   0.00677  -0.0927   0.4207   1.0000
  10.000   1.6509   0.01147   0.00699  -0.0906   0.4154   1.0000
  10.250   1.6685   0.01169   0.00724  -0.0892   0.4088   1.0000
  10.500   1.6799   0.01207   0.00760  -0.0870   0.4006   1.0000
  10.750   1.6939   0.01246   0.00799  -0.0853   0.3914   1.0000
  11.000   1.7036   0.01303   0.00855  -0.0830   0.3818   1.0000
  11.250   1.7095   0.01382   0.00931  -0.0804   0.3714   1.0000
  11.500   1.7149   0.01473   0.01021  -0.0780   0.3611   1.0000
  11.750   1.7204   0.01574   0.01122  -0.0758   0.3519   1.0000
  12.000   1.7207   0.01714   0.01260  -0.0733   0.3425   1.0000
  12.250   1.7231   0.01856   0.01403  -0.0713   0.3338   1.0000
  12.500   1.7235   0.02024   0.01573  -0.0695   0.3263   1.0000
  12.750   1.7210   0.02223   0.01774  -0.0676   0.3187   1.0000
  13.000   1.7168   0.02447   0.02001  -0.0658   0.3113   1.0000
  13.250   1.7092   0.02712   0.02270  -0.0641   0.3044   1.0000
  13.500   1.6985   0.03020   0.02582  -0.0625   0.2978   1.0000
  13.750   1.6839   0.03376   0.02941  -0.0609   0.2902   1.0000
  14.000   1.6693   0.03739   0.03308  -0.0594   0.2850   1.0000
  14.250   1.6626   0.04032   0.03606  -0.0584   0.2790   1.0000
  14.500   1.6490   0.04387   0.03962  -0.0571   0.2739   1.0000
  14.750   1.6412   0.04695   0.04273  -0.0561   0.2684   1.0000
  15.000   1.6310   0.05025   0.04605  -0.0551   0.2617   1.0000
  15.500   1.6254   0.05557   0.05143  -0.0538   0.2528   1.0000
  15.750   1.6250   0.05802   0.05390  -0.0533   0.2481   1.0000
  16.000   1.6163   0.06129   0.05714  -0.0525   0.2423   1.0000
  16.250   1.6232   0.06310   0.05902  -0.0523   0.2391   1.0000
  16.500   1.6251   0.06539   0.06133  -0.0520   0.2342   1.0000
  16.750   1.6210   0.06831   0.06423  -0.0516   0.2292   1.0000
  17.000   1.6260   0.07030   0.06629  -0.0514   0.2259   1.0000
  17.250   1.6287   0.07256   0.06856  -0.0512   0.2206   1.0000
  17.500   1.6261   0.07537   0.07136  -0.0509   0.2155   1.0000
  17.750   1.6278   0.07781   0.07384  -0.0508   0.2100   1.0000
  18.000   1.6306   0.08008   0.07614  -0.0507   0.2057   1.0000
  18.250   1.6275   0.08298   0.07901  -0.0505   0.2001   1.0000
  18.500   1.6300   0.08534   0.08143  -0.0505   0.1946   1.0000
  18.750   1.6283   0.08815   0.08425  -0.0505   0.1892   1.0000
  19.000   1.6303   0.09057   0.08668  -0.0505   0.1841   1.0000
  19.250   1.6296   0.09333   0.08947  -0.0506   0.1788   1.0000
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