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SARATOV AIRFOIL (saratov-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SARATOV AIRFOIL (saratov-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.85 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-saratov-il-1000000-n5.txt
Download as CSV file: xf-saratov-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SARATOV AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.3009   0.06103   0.05713  -0.1149   0.5128   0.0257
 -10.500  -0.3111   0.05506   0.05107  -0.1214   0.5120   0.0261
 -10.250  -0.3062   0.05058   0.04651  -0.1271   0.5106   0.0264
  -9.750  -0.2755   0.04377   0.03954  -0.1371   0.5080   0.0274
  -9.500  -0.2539   0.04131   0.03704  -0.1410   0.5070   0.0281
  -9.250  -0.2306   0.03922   0.03492  -0.1442   0.5059   0.0287
  -9.000  -0.2061   0.03676   0.03238  -0.1482   0.5048   0.0293
  -8.750  -0.1802   0.03455   0.03009  -0.1518   0.5035   0.0298
  -8.500  -0.1533   0.03260   0.02804  -0.1551   0.5023   0.0304
  -8.250  -0.1255   0.03065   0.02599  -0.1583   0.5009   0.0308
  -8.000  -0.0971   0.02869   0.02391  -0.1615   0.4995   0.0313
  -7.750  -0.0686   0.02715   0.02225  -0.1640   0.4981   0.0317
  -7.500  -0.0400   0.02573   0.02072  -0.1662   0.4968   0.0320
  -7.250  -0.0113   0.02435   0.01922  -0.1683   0.4955   0.0323
  -7.000   0.0174   0.02311   0.01788  -0.1701   0.4943   0.0325
  -6.750   0.0463   0.02202   0.01669  -0.1717   0.4930   0.0332
  -6.500   0.0753   0.02086   0.01543  -0.1733   0.4917   0.0342
  -6.250   0.1043   0.01963   0.01412  -0.1749   0.4913   0.0348
  -6.000   0.1332   0.01856   0.01297  -0.1762   0.4907   0.0355
  -5.750   0.1619   0.01753   0.01184  -0.1774   0.4902   0.0362
  -5.500   0.1905   0.01661   0.01082  -0.1783   0.4896   0.0368
  -5.250   0.2190   0.01577   0.00989  -0.1792   0.4889   0.0376
  -5.000   0.2475   0.01502   0.00905  -0.1799   0.4883   0.0383
  -4.750   0.2759   0.01436   0.00829  -0.1804   0.4876   0.0389
  -4.500   0.3042   0.01379   0.00763  -0.1809   0.4869   0.0395
  -4.250   0.3324   0.01332   0.00709  -0.1812   0.4862   0.0399
  -4.000   0.3608   0.01271   0.00638  -0.1817   0.4855   0.0410
  -3.750   0.3891   0.01211   0.00568  -0.1822   0.4848   0.0428
  -3.500   0.4172   0.01169   0.00520  -0.1824   0.4841   0.0445
  -3.250   0.4452   0.01137   0.00482  -0.1825   0.4835   0.0459
  -3.000   0.4732   0.01112   0.00452  -0.1826   0.4828   0.0473
  -2.750   0.5012   0.01093   0.00427  -0.1826   0.4821   0.0484
  -2.500   0.5290   0.01076   0.00405  -0.1826   0.4815   0.0494
  -2.250   0.5569   0.01061   0.00387  -0.1825   0.4809   0.0501
  -2.000   0.5848   0.01042   0.00362  -0.1825   0.4803   0.0532
  -1.750   0.6125   0.01025   0.00342  -0.1825   0.4796   0.0569
  -1.500   0.6403   0.01009   0.00325  -0.1824   0.4790   0.0611
  -1.250   0.6679   0.00991   0.00307  -0.1823   0.4784   0.0739
  -1.000   0.6952   0.00960   0.00288  -0.1824   0.4777   0.1183
  -0.750   0.7228   0.00960   0.00287  -0.1822   0.4771   0.1249
  -0.500   0.7503   0.00961   0.00288  -0.1820   0.4764   0.1280
  -0.250   0.7776   0.00962   0.00290  -0.1818   0.4751   0.1325
   0.000   0.8055   0.00959   0.00289  -0.1817   0.4744   0.1362
   0.250   0.8333   0.00957   0.00288  -0.1816   0.4733   0.1378
   0.500   0.8609   0.00957   0.00288  -0.1814   0.4726   0.1390
   0.750   0.8885   0.00958   0.00290  -0.1813   0.4721   0.1398
   1.000   0.9161   0.00958   0.00291  -0.1811   0.4711   0.1412
   1.250   0.9436   0.00957   0.00292  -0.1809   0.4700   0.1440
   1.500   0.9710   0.00958   0.00295  -0.1808   0.4691   0.1455
   1.750   0.9984   0.00959   0.00299  -0.1806   0.4682   0.1470
   2.000   1.0257   0.00960   0.00302  -0.1804   0.4668   0.1489
   2.250   1.0529   0.00962   0.00306  -0.1802   0.4657   0.1511
   2.500   1.0800   0.00965   0.00310  -0.1800   0.4640   0.1523
   2.750   1.1070   0.00969   0.00314  -0.1797   0.4622   0.1533
   3.000   1.1338   0.00974   0.00320  -0.1795   0.4608   0.1541
   3.250   1.1604   0.00981   0.00328  -0.1792   0.4592   0.1548
   3.500   1.1876   0.00983   0.00334  -0.1790   0.4584   0.1554
   3.750   1.2148   0.00984   0.00340  -0.1788   0.4571   0.1573
   4.000   1.2419   0.00984   0.00346  -0.1786   0.4550   0.1596
   4.250   1.2688   0.00986   0.00352  -0.1784   0.4522   0.1618
   4.500   1.2954   0.00989   0.00359  -0.1781   0.4495   0.1639
   4.750   1.3217   0.00994   0.00367  -0.1778   0.4465   0.1661
   5.000   1.3479   0.00999   0.00375  -0.1775   0.4419   0.1684
   5.250   1.3740   0.01004   0.00381  -0.1771   0.4311   0.1707
   5.500   1.3820   0.01147   0.00460  -0.1739   0.3128   0.1719
   5.750   1.3772   0.01381   0.00620  -0.1686   0.1693   0.1739
   6.000   1.3967   0.01424   0.00660  -0.1672   0.1541   0.1781
   6.250   1.4172   0.01456   0.00692  -0.1659   0.1459   0.1820
   6.500   1.4378   0.01487   0.00724  -0.1647   0.1388   0.1861
   6.750   1.4579   0.01517   0.00755  -0.1634   0.1322   0.1907
   7.000   1.4763   0.01553   0.00792  -0.1618   0.1244   0.1978
   7.500   1.5063   0.01626   0.00866  -0.1573   0.1060   0.2168
   7.750   1.5175   0.01676   0.00915  -0.1545   0.0940   0.2380
   8.000   1.5259   0.01744   0.00983  -0.1512   0.0787   0.2680
   8.250   1.5291   0.01840   0.01073  -0.1473   0.0603   0.2815
   8.500   1.5294   0.01954   0.01181  -0.1432   0.0432   0.2883
   8.750   1.5274   0.02085   0.01307  -0.1391   0.0288   0.2935
   9.000   1.5287   0.02216   0.01438  -0.1356   0.0206   0.2965
   9.250   1.5337   0.02337   0.01561  -0.1329   0.0172   0.3004
   9.500   1.5386   0.02465   0.01692  -0.1303   0.0153   0.3044
   9.750   1.5448   0.02592   0.01824  -0.1281   0.0141   0.3075
  10.000   1.5510   0.02734   0.01971  -0.1261   0.0135   0.3087
  10.250   1.5559   0.02896   0.02140  -0.1242   0.0128   0.3098
  10.500   1.5592   0.03083   0.02333  -0.1223   0.0120   0.3109
  10.750   1.5622   0.03285   0.02540  -0.1207   0.0114   0.3122
  11.000   1.5649   0.03503   0.02764  -0.1192   0.0108   0.3135
  11.250   1.5700   0.03705   0.02973  -0.1180   0.0105   0.3153
  11.500   1.5743   0.03921   0.03195  -0.1169   0.0101   0.3168
  11.750   1.5785   0.04143   0.03422  -0.1159   0.0097   0.3187
  12.000   1.5822   0.04375   0.03660  -0.1149   0.0093   0.3199
  12.250   1.5857   0.04615   0.03905  -0.1140   0.0090   0.3208
  12.500   1.5886   0.04864   0.04160  -0.1131   0.0086   0.3216
  12.750   1.5918   0.05113   0.04415  -0.1123   0.0083   0.3222
  13.000   1.5945   0.05371   0.04679  -0.1116   0.0080   0.3227
  13.250   1.6001   0.05595   0.04909  -0.1109   0.0078   0.3236
  13.500   1.6052   0.05830   0.05150  -0.1103   0.0077   0.3246
  13.750   1.6109   0.06059   0.05385  -0.1097   0.0075   0.3260
  14.000   1.6165   0.06292   0.05625  -0.1092   0.0073   0.3279
  14.250   1.6228   0.06513   0.05851  -0.1087   0.0070   0.3283
  14.500   1.6285   0.06748   0.06090  -0.1083   0.0068   0.3293
  14.750   1.6347   0.06975   0.06323  -0.1079   0.0066   0.3300
  15.000   1.6412   0.07201   0.06553  -0.1075   0.0064   0.3308
  15.250   1.6463   0.07449   0.06805  -0.1072   0.0061   0.3318
  15.500   1.6509   0.07704   0.07065  -0.1069   0.0059   0.3323
  15.750   1.6564   0.07949   0.07316  -0.1067   0.0057   0.3326
  16.000   1.6630   0.08182   0.07557  -0.1065   0.0057   0.3329
  16.250   1.6684   0.08435   0.07817  -0.1064   0.0056   0.3331
  16.500   1.6744   0.08682   0.08070  -0.1062   0.0055   0.3334
  16.750   1.6806   0.08922   0.08316  -0.1062   0.0053   0.3337
  17.000   1.6859   0.09178   0.08580  -0.1061   0.0052   0.3340
  17.250   1.6905   0.09450   0.08859  -0.1062   0.0051   0.3343
  17.500   1.6955   0.09714   0.09130  -0.1063   0.0050   0.3346
  17.750   1.7009   0.09973   0.09395  -0.1064   0.0049   0.3349
  18.000   1.7053   0.10250   0.09680  -0.1066   0.0048   0.3353
  18.250   1.7088   0.10542   0.09979  -0.1069   0.0047   0.3356
  18.500   1.7126   0.10828   0.10272  -0.1072   0.0046   0.3360
  18.750   1.7162   0.11116   0.10567  -0.1076   0.0045   0.3364
  19.000   1.7179   0.11440   0.10899  -0.1081   0.0044   0.3367
  19.250   1.7195   0.11766   0.11232  -0.1087   0.0043   0.3371
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