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SARATOV AIRFOIL (saratov-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SARATOV AIRFOIL (saratov-il)
Reynolds number: 500,000
Max Cl/Cd: 113.76 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-saratov-il-500000-n5.txt
Download as CSV file: xf-saratov-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.0529   0.09127   0.08652  -0.0975   0.5289   0.0233
  -9.750  -0.0462   0.08874   0.08398  -0.0985   0.5274   0.0243
  -9.250  -0.0522   0.08009   0.07535  -0.1019   0.5254   0.0270
  -9.000  -0.0410   0.07865   0.07392  -0.1025   0.5242   0.0274
  -8.750  -0.0304   0.07711   0.07237  -0.1030   0.5230   0.0278
  -8.500  -0.0214   0.07534   0.07061  -0.1035   0.5218   0.0284
  -8.250  -0.0142   0.07339   0.06866  -0.1040   0.5206   0.0291
  -8.000  -0.1088   0.04800   0.04328  -0.1272   0.5223   0.0338
  -7.750  -0.0911   0.04077   0.03586  -0.1389   0.5212   0.0346
  -7.500  -0.0642   0.03618   0.03110  -0.1469   0.5198   0.0353
  -7.250  -0.0341   0.03238   0.02710  -0.1537   0.5184   0.0361
  -7.000  -0.0034   0.02947   0.02399  -0.1589   0.5168   0.0368
  -6.750   0.0274   0.02703   0.02136  -0.1631   0.5153   0.0376
  -6.500   0.0579   0.02501   0.01914  -0.1664   0.5139   0.0385
  -6.250   0.0878   0.02339   0.01734  -0.1689   0.5124   0.0391
  -6.000   0.1173   0.02204   0.01581  -0.1708   0.5111   0.0396
  -5.750   0.1463   0.02094   0.01455  -0.1723   0.5099   0.0399
  -5.500   0.1751   0.02012   0.01360  -0.1734   0.5087   0.0408
  -5.250   0.2041   0.01932   0.01272  -0.1744   0.5079   0.0419
  -5.000   0.2331   0.01851   0.01183  -0.1754   0.5072   0.0429
  -4.750   0.2620   0.01775   0.01097  -0.1762   0.5064   0.0439
  -4.500   0.2907   0.01709   0.01021  -0.1770   0.5055   0.0450
  -4.250   0.3193   0.01645   0.00948  -0.1776   0.5047   0.0464
  -4.000   0.3479   0.01588   0.00880  -0.1782   0.5039   0.0477
  -3.750   0.3764   0.01539   0.00821  -0.1786   0.5031   0.0488
  -3.500   0.4047   0.01495   0.00767  -0.1790   0.5023   0.0496
  -3.250   0.4332   0.01450   0.00713  -0.1793   0.5014   0.0511
  -3.000   0.4618   0.01391   0.00643  -0.1798   0.5007   0.0538
  -2.750   0.4901   0.01342   0.00583  -0.1802   0.4999   0.0563
  -2.500   0.5182   0.01305   0.00538  -0.1804   0.4991   0.0590
  -2.250   0.5462   0.01277   0.00502  -0.1805   0.4984   0.0621
  -2.000   0.5742   0.01246   0.00464  -0.1806   0.4977   0.0700
  -1.750   0.6019   0.01193   0.00421  -0.1809   0.4971   0.1134
  -1.500   0.6296   0.01190   0.00415  -0.1808   0.4964   0.1249
  -1.250   0.6572   0.01190   0.00413  -0.1807   0.4958   0.1301
  -1.000   0.6848   0.01193   0.00415  -0.1805   0.4951   0.1352
  -0.750   0.7124   0.01196   0.00414  -0.1804   0.4945   0.1388
  -0.500   0.7400   0.01200   0.00414  -0.1802   0.4939   0.1412
  -0.250   0.7675   0.01205   0.00421  -0.1801   0.4933   0.1445
   0.000   0.7951   0.01212   0.00427  -0.1799   0.4927   0.1468
   0.250   0.8227   0.01219   0.00433  -0.1798   0.4921   0.1489
   0.500   0.8502   0.01225   0.00438  -0.1796   0.4915   0.1513
   0.750   0.8776   0.01224   0.00438  -0.1795   0.4906   0.1530
   1.000   0.9048   0.01221   0.00436  -0.1792   0.4892   0.1540
   1.250   0.9320   0.01222   0.00438  -0.1790   0.4878   0.1552
   1.500   0.9593   0.01221   0.00440  -0.1788   0.4870   0.1577
   1.750   0.9865   0.01222   0.00446  -0.1787   0.4861   0.1601
   2.000   1.0136   0.01223   0.00449  -0.1784   0.4848   0.1613
   2.250   1.0406   0.01224   0.00453  -0.1782   0.4833   0.1625
   2.500   1.0675   0.01226   0.00458  -0.1780   0.4819   0.1639
   2.750   1.0944   0.01229   0.00463  -0.1777   0.4805   0.1653
   3.000   1.1212   0.01234   0.00469  -0.1775   0.4794   0.1668
   3.250   1.1479   0.01239   0.00477  -0.1772   0.4779   0.1684
   3.500   1.1744   0.01247   0.00485  -0.1769   0.4761   0.1699
   3.750   1.2010   0.01254   0.00496  -0.1766   0.4747   0.1712
   4.000   1.2276   0.01257   0.00507  -0.1763   0.4736   0.1729
   4.250   1.2541   0.01260   0.00519  -0.1760   0.4723   0.1756
   4.500   1.2805   0.01264   0.00531  -0.1757   0.4706   0.1788
   4.750   1.3066   0.01266   0.00542  -0.1753   0.4682   0.1821
   5.000   1.3324   0.01268   0.00550  -0.1749   0.4652   0.1853
   5.250   1.3578   0.01272   0.00558  -0.1744   0.4622   0.1881
   5.500   1.3829   0.01281   0.00571  -0.1739   0.4593   0.1925
   5.750   1.4088   0.01281   0.00586  -0.1735   0.4552   0.1979
   6.000   1.4332   0.01280   0.00592  -0.1728   0.4471   0.2037
   6.250   1.4572   0.01281   0.00600  -0.1720   0.4338   0.2122
   6.500   1.4548   0.01425   0.00676  -0.1669   0.3055   0.2186
   6.750   1.4387   0.01685   0.00873  -0.1600   0.1813   0.2226
   7.250   1.4579   0.01824   0.01016  -0.1537   0.1542   0.2530
   7.500   1.4696   0.01891   0.01089  -0.1510   0.1467   0.2666
   7.750   1.4796   0.01963   0.01162  -0.1482   0.1379   0.2774
   8.000   1.4905   0.02031   0.01233  -0.1456   0.1303   0.2845
   8.500   1.5075   0.02196   0.01398  -0.1402   0.1125   0.2971
   8.750   1.5149   0.02292   0.01495  -0.1375   0.1019   0.3006
   9.250   1.5209   0.02554   0.01751  -0.1317   0.0773   0.3082
   9.500   1.5168   0.02756   0.01948  -0.1285   0.0612   0.3092
   9.750   1.5087   0.03009   0.02198  -0.1255   0.0465   0.3102
  10.000   1.5009   0.03292   0.02480  -0.1230   0.0344   0.3113
  10.250   1.4948   0.03589   0.02778  -0.1210   0.0262   0.3126
  10.500   1.4924   0.03869   0.03062  -0.1195   0.0219   0.3143
  10.750   1.4915   0.04144   0.03343  -0.1182   0.0193   0.3169
  11.000   1.4935   0.04394   0.03599  -0.1171   0.0178   0.3203
  11.250   1.4953   0.04653   0.03864  -0.1162   0.0166   0.3211
  11.500   1.4967   0.04919   0.04137  -0.1152   0.0155   0.3221
  11.750   1.4983   0.05185   0.04410  -0.1143   0.0146   0.3234
  12.000   1.5024   0.05427   0.04659  -0.1135   0.0140   0.3250
  12.250   1.5069   0.05664   0.04903  -0.1128   0.0135   0.3267
  12.500   1.5114   0.05902   0.05148  -0.1121   0.0129   0.3283
  12.750   1.5162   0.06141   0.05394  -0.1115   0.0124   0.3306
  13.000   1.5207   0.06385   0.05643  -0.1108   0.0119   0.3330
  13.250   1.5247   0.06636   0.05901  -0.1102   0.0114   0.3347
  13.500   1.5269   0.06914   0.06186  -0.1097   0.0109   0.3365
  13.750   1.5338   0.07136   0.06414  -0.1092   0.0106   0.3385
  14.000   1.5401   0.07367   0.06653  -0.1088   0.0103   0.3401
  14.250   1.5461   0.07604   0.06897  -0.1084   0.0099   0.3413
  14.500   1.5521   0.07844   0.07144  -0.1081   0.0096   0.3421
  14.750   1.5581   0.08084   0.07391  -0.1078   0.0093   0.3428
  15.000   1.5639   0.08331   0.07645  -0.1075   0.0090   0.3435
  15.250   1.5691   0.08589   0.07909  -0.1073   0.0088   0.3440
  15.500   1.5741   0.08849   0.08176  -0.1072   0.0085   0.3444
  15.750   1.5781   0.09126   0.08460  -0.1071   0.0083   0.3448
  16.000   1.5794   0.09446   0.08787  -0.1071   0.0081   0.3451
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