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SARATOV AIRFOIL (saratov-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SARATOV AIRFOIL (saratov-il)
Reynolds number: 1,000,000
Max Cl/Cd: 145.9 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-saratov-il-1000000.txt
Download as CSV file: xf-saratov-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.0209   0.09268   0.08876  -0.1020   0.5313   0.0260
  -9.750  -0.0254   0.08762   0.08372  -0.1042   0.5307   0.0266
  -9.500  -0.0030   0.08842   0.08450  -0.1036   0.5289   0.0279
  -9.250   0.0086   0.08684   0.08292  -0.1042   0.5274   0.0287
  -9.000   0.0077   0.08320   0.07930  -0.1064   0.5264   0.0319
  -8.750   0.0126   0.08032   0.07642  -0.1074   0.5254   0.0319
  -8.250  -0.1264   0.03163   0.02729  -0.1568   0.5280   0.0333
  -8.000  -0.0985   0.02980   0.02539  -0.1599   0.5263   0.0340
  -7.750  -0.0701   0.02800   0.02351  -0.1629   0.5246   0.0347
  -7.500  -0.0408   0.02591   0.02129  -0.1664   0.5229   0.0354
  -7.250  -0.0113   0.02395   0.01917  -0.1694   0.5211   0.0361
  -7.000   0.0179   0.02228   0.01735  -0.1719   0.5193   0.0368
  -6.750   0.0468   0.02090   0.01581  -0.1739   0.5173   0.0374
  -6.500   0.0756   0.01974   0.01453  -0.1754   0.5161   0.0380
  -6.250   0.1047   0.01871   0.01339  -0.1767   0.5153   0.0384
  -6.000   0.1334   0.01768   0.01223  -0.1778   0.5144   0.0395
  -5.750   0.1620   0.01697   0.01145  -0.1786   0.5135   0.0406
  -5.500   0.1906   0.01625   0.01066  -0.1793   0.5124   0.0415
  -5.250   0.2191   0.01561   0.00995  -0.1799   0.5114   0.0424
  -5.000   0.2475   0.01500   0.00925  -0.1805   0.5104   0.0434
  -4.750   0.2759   0.01446   0.00863  -0.1810   0.5095   0.0444
  -4.500   0.3042   0.01397   0.00805  -0.1813   0.5085   0.0454
  -4.250   0.3325   0.01358   0.00758  -0.1816   0.5076   0.0461
  -4.000   0.3609   0.01308   0.00698  -0.1820   0.5067   0.0475
  -3.750   0.3893   0.01249   0.00630  -0.1824   0.5058   0.0497
  -3.500   0.4174   0.01207   0.00580  -0.1826   0.5049   0.0514
  -3.250   0.4454   0.01173   0.00538  -0.1828   0.5040   0.0531
  -3.000   0.4734   0.01147   0.00504  -0.1829   0.5030   0.0547
  -2.750   0.5012   0.01128   0.00479  -0.1829   0.5019   0.0562
  -2.500   0.5291   0.01091   0.00433  -0.1830   0.5008   0.0609
  -2.250   0.5569   0.01069   0.00406  -0.1831   0.4998   0.0649
  -2.000   0.5849   0.01034   0.00370  -0.1831   0.4995   0.0770
  -1.750   0.6125   0.00995   0.00345  -0.1833   0.4992   0.1259
  -1.500   0.6404   0.00993   0.00346  -0.1832   0.4988   0.1335
  -1.250   0.6683   0.00998   0.00351  -0.1830   0.4984   0.1382
  -1.000   0.6963   0.01005   0.00357  -0.1829   0.4980   0.1401
  -0.750   0.7241   0.01002   0.00354  -0.1828   0.4976   0.1434
  -0.500   0.7519   0.01006   0.00360  -0.1827   0.4972   0.1462
  -0.250   0.7797   0.01013   0.00368  -0.1825   0.4967   0.1487
   0.000   0.8074   0.01015   0.00370  -0.1824   0.4957   0.1507
   0.250   0.8351   0.01014   0.00369  -0.1822   0.4943   0.1522
   0.500   0.8627   0.01014   0.00368  -0.1820   0.4931   0.1534
   0.750   0.8904   0.01019   0.00373  -0.1819   0.4924   0.1544
   1.000   0.9179   0.01016   0.00370  -0.1817   0.4915   0.1567
   1.250   0.9453   0.01013   0.00368  -0.1816   0.4905   0.1592
   1.500   0.9728   0.01014   0.00370  -0.1814   0.4895   0.1606
   1.750   1.0002   0.01018   0.00375  -0.1812   0.4888   0.1625
   2.000   1.0275   0.01021   0.00380  -0.1811   0.4877   0.1642
   2.250   1.0548   0.01027   0.00386  -0.1809   0.4863   0.1653
   2.500   1.0820   0.01039   0.00397  -0.1807   0.4846   0.1666
   2.750   1.1093   0.01046   0.00406  -0.1806   0.4833   0.1677
   3.000   1.1365   0.01045   0.00408  -0.1804   0.4827   0.1689
   3.250   1.1637   0.01045   0.00412  -0.1802   0.4820   0.1698
   3.500   1.1908   0.01045   0.00415  -0.1799   0.4811   0.1710
   3.750   1.2178   0.01041   0.00416  -0.1797   0.4799   0.1741
   4.000   1.2446   0.01038   0.00419  -0.1795   0.4783   0.1767
   4.250   1.2714   0.01038   0.00423  -0.1792   0.4767   0.1791
   4.500   1.2982   0.01039   0.00428  -0.1789   0.4751   0.1815
   4.750   1.3248   0.01040   0.00433  -0.1786   0.4735   0.1840
   5.000   1.3506   0.01042   0.00435  -0.1782   0.4699   0.1860
   5.250   1.3766   0.01040   0.00439  -0.1778   0.4660   0.1917
   5.500   1.4029   0.01028   0.00436  -0.1775   0.4617   0.1972
   5.750   1.4290   0.01025   0.00436  -0.1771   0.4570   0.2019
   6.000   1.4543   0.01025   0.00442  -0.1766   0.4509   0.2120
   6.250   1.4800   0.01020   0.00443  -0.1761   0.4396   0.2284
   6.500   1.5042   0.01031   0.00460  -0.1755   0.4150   0.2704
   6.750   1.4786   0.01394   0.00694  -0.1667   0.1895   0.2761
   7.000   1.4908   0.01478   0.00765  -0.1641   0.1618   0.2925
   7.250   1.5074   0.01535   0.00820  -0.1621   0.1494   0.2984
   7.500   1.5213   0.01582   0.00863  -0.1597   0.1390   0.3061
   7.750   1.5358   0.01624   0.00907  -0.1573   0.1319   0.3080
   8.000   1.5483   0.01678   0.00960  -0.1546   0.1240   0.3097
   8.250   1.5624   0.01727   0.01010  -0.1523   0.1167   0.3115
   8.500   1.5736   0.01787   0.01068  -0.1496   0.1074   0.3138
   8.750   1.5812   0.01863   0.01139  -0.1464   0.0933   0.3173
   9.000   1.5795   0.01985   0.01246  -0.1421   0.0701   0.3204
   9.250   1.5696   0.02161   0.01410  -0.1370   0.0450   0.3210
   9.500   1.5586   0.02367   0.01609  -0.1322   0.0282   0.3215
   9.750   1.5569   0.02541   0.01784  -0.1290   0.0226   0.3223
  10.000   1.5594   0.02702   0.01951  -0.1265   0.0204   0.3231
  10.250   1.5601   0.02891   0.02144  -0.1241   0.0188   0.3240
  10.500   1.5600   0.03104   0.02364  -0.1219   0.0176   0.3250
  10.750   1.5638   0.03297   0.02565  -0.1203   0.0170   0.3263
  11.000   1.5664   0.03513   0.02788  -0.1188   0.0163   0.3276
  11.250   1.5687   0.03741   0.03023  -0.1175   0.0158   0.3293
  11.500   1.5694   0.03994   0.03282  -0.1162   0.0152   0.3312
  11.750   1.5687   0.04271   0.03564  -0.1150   0.0146   0.3331
  12.000   1.5643   0.04594   0.03896  -0.1137   0.0139   0.3347
  12.250   1.5697   0.04812   0.04121  -0.1129   0.0137   0.3355
  12.500   1.5745   0.05042   0.04358  -0.1121   0.0133   0.3370
  12.750   1.5783   0.05286   0.04609  -0.1114   0.0130   0.3384
  13.000   1.5820   0.05532   0.04861  -0.1107   0.0126   0.3396
  13.250   1.5859   0.05777   0.05111  -0.1100   0.0123   0.3412
  13.500   1.5897   0.06028   0.05367  -0.1094   0.0119   0.3437
  13.750   1.5926   0.06292   0.05636  -0.1087   0.0116   0.3468
  14.000   1.5939   0.06578   0.05929  -0.1082   0.0113   0.3492
  14.250   1.5893   0.06940   0.06300  -0.1076   0.0109   0.3508
  14.500   1.5956   0.07172   0.06539  -0.1072   0.0107   0.3527
  14.750   1.6020   0.07406   0.06779  -0.1069   0.0106   0.3535
  15.000   1.6085   0.07636   0.07015  -0.1065   0.0104   0.3541
  15.250   1.6140   0.07883   0.07270  -0.1063   0.0102   0.3550
  15.500   1.6193   0.08137   0.07529  -0.1061   0.0099   0.3561
  15.750   1.6254   0.08381   0.07779  -0.1059   0.0097   0.3571
  16.000   1.6313   0.08626   0.08030  -0.1057   0.0094   0.3577
  16.250   1.6363   0.08891   0.08300  -0.1057   0.0092   0.3582
  16.500   1.6412   0.09156   0.08571  -0.1057   0.0090   0.3587
  16.750   1.6447   0.09441   0.08860  -0.1057   0.0088   0.3592
  17.000   1.6447   0.09779   0.09204  -0.1058   0.0085   0.3596
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