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SARATOV AIRFOIL (saratov-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: SARATOV AIRFOIL (saratov-il)
Reynolds number: 200,000
Max Cl/Cd: 77.9 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-saratov-il-200000-n5.txt
Download as CSV file: xf-saratov-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.0292   0.09726   0.09159  -0.0935   0.5972   0.0371
  -9.500  -0.0232   0.09459   0.08886  -0.0945   0.5921   0.0374
  -9.250  -0.0172   0.09189   0.08614  -0.0955   0.5878   0.0376
  -9.000  -0.0142   0.08887   0.08309  -0.0969   0.5841   0.0387
  -8.750  -0.0194   0.08490   0.07914  -0.0996   0.5815   0.0401
  -8.500  -0.0117   0.08253   0.07673  -0.0999   0.5781   0.0406
  -8.250  -0.0012   0.08075   0.07491  -0.1001   0.5750   0.0410
  -8.000   0.0068   0.07867   0.07283  -0.1005   0.5723   0.0413
  -7.750   0.0166   0.07700   0.07114  -0.1007   0.5696   0.0420
  -7.500   0.0258   0.07546   0.06957  -0.1008   0.5669   0.0429
  -7.250   0.0322   0.07378   0.06787  -0.1009   0.5648   0.0440
  -7.000   0.0392   0.07150   0.06557  -0.1022   0.5629   0.0446
  -6.750   0.0473   0.06886   0.06290  -0.1040   0.5611   0.0449
  -6.500   0.0570   0.06602   0.06002  -0.1064   0.5595   0.0452
  -6.250   0.0688   0.06295   0.05693  -0.1094   0.5580   0.0456
  -6.000   0.0826   0.05960   0.05355  -0.1131   0.5564   0.0461
  -5.500   0.1429   0.03140   0.02451  -0.1570   0.5540   0.0511
  -5.250   0.1756   0.02881   0.02169  -0.1614   0.5520   0.0527
  -5.000   0.2058   0.02746   0.02021  -0.1637   0.5501   0.0544
  -4.750   0.2369   0.02588   0.01841  -0.1663   0.5482   0.0564
  -4.500   0.2679   0.02447   0.01677  -0.1686   0.5466   0.0582
  -4.250   0.2980   0.02343   0.01552  -0.1701   0.5450   0.0598
  -4.000   0.3279   0.02260   0.01448  -0.1714   0.5437   0.0614
  -3.750   0.3575   0.02189   0.01357  -0.1724   0.5425   0.0629
  -3.500   0.3859   0.02170   0.01336  -0.1727   0.5414   0.0656
  -3.250   0.4159   0.02095   0.01255  -0.1738   0.5402   0.0702
  -3.000   0.4464   0.01993   0.01137  -0.1753   0.5390   0.0754
  -2.750   0.4770   0.01886   0.01019  -0.1768   0.5379   0.0839
  -2.500   0.5047   0.01910   0.01065  -0.1766   0.5368   0.0998
  -2.250   0.5360   0.01759   0.00872  -0.1785   0.5358   0.1268
  -2.000   0.5637   0.01787   0.00901  -0.1783   0.5347   0.1355
  -1.750   0.5921   0.01773   0.00873  -0.1786   0.5338   0.1429
  -1.500   0.6191   0.01818   0.00924  -0.1781   0.5328   0.1475
  -1.250   0.6478   0.01778   0.00862  -0.1786   0.5320   0.1527
  -1.000   0.6760   0.01758   0.00827  -0.1788   0.5311   0.1567
  -0.750   0.7028   0.01800   0.00880  -0.1783   0.5303   0.1599
  -0.500   0.7300   0.01827   0.00910  -0.1781   0.5296   0.1638
  -0.250   0.7582   0.01803   0.00873  -0.1783   0.5289   0.1672
   0.000   0.7864   0.01782   0.00835  -0.1785   0.5282   0.1705
   0.250   0.8141   0.01781   0.00829  -0.1785   0.5276   0.1736
   0.500   0.8414   0.01798   0.00851  -0.1784   0.5270   0.1763
   0.750   0.8690   0.01802   0.00854  -0.1784   0.5264   0.1784
   1.000   0.8969   0.01799   0.00845  -0.1784   0.5258   0.1798
   1.250   0.9243   0.01793   0.00837  -0.1784   0.5253   0.1813
   1.500   0.9515   0.01789   0.00833  -0.1783   0.5246   0.1828
   1.750   0.9786   0.01788   0.00833  -0.1782   0.5239   0.1844
   2.000   1.0053   0.01788   0.00834  -0.1780   0.5226   0.1859
   2.250   1.0317   0.01788   0.00835  -0.1777   0.5207   0.1874
   2.500   1.0580   0.01788   0.00839  -0.1774   0.5185   0.1889
   2.750   1.0844   0.01793   0.00851  -0.1771   0.5167   0.1907
   3.000   1.1110   0.01803   0.00867  -0.1769   0.5155   0.1927
   3.250   1.1375   0.01812   0.00883  -0.1767   0.5139   0.1953
   3.500   1.1641   0.01819   0.00892  -0.1764   0.5118   0.1986
   3.750   1.1910   0.01830   0.00901  -0.1762   0.5099   0.2019
   4.000   1.2180   0.01847   0.00921  -0.1760   0.5087   0.2049
   4.250   1.2433   0.01861   0.00952  -0.1756   0.5075   0.2079
   4.500   1.2683   0.01875   0.00981  -0.1751   0.5058   0.2116
   4.750   1.2932   0.01888   0.01006  -0.1746   0.5035   0.2161
   5.000   1.3182   0.01900   0.01031  -0.1740   0.5012   0.2210
   5.250   1.3434   0.01918   0.01064  -0.1736   0.4993   0.2264
   5.500   1.3688   0.01931   0.01088  -0.1731   0.4970   0.2341
   5.750   1.3945   0.01946   0.01113  -0.1726   0.4940   0.2413
   6.000   1.4201   0.01964   0.01139  -0.1721   0.4912   0.2508
   6.250   1.4417   0.01988   0.01187  -0.1710   0.4877   0.2570
   6.500   1.4647   0.02006   0.01222  -0.1701   0.4842   0.2667
   6.750   1.4881   0.02021   0.01250  -0.1692   0.4805   0.2750
   7.000   1.5122   0.02015   0.01246  -0.1683   0.4752   0.2846
   7.250   1.5292   0.02014   0.01267  -0.1662   0.4650   0.2950
   7.500   1.5473   0.02008   0.01275  -0.1643   0.4522   0.3019
   7.750   1.5643   0.02008   0.01289  -0.1623   0.4328   0.3100
   8.000   1.5534   0.02047   0.01270  -0.1553   0.3237   0.3129
   8.250   1.5194   0.02280   0.01459  -0.1455   0.2470   0.3135
   8.500   1.4924   0.02540   0.01694  -0.1382   0.1974   0.3148
   8.750   1.4796   0.02758   0.01906  -0.1334   0.1789   0.3189
   9.000   1.4714   0.02974   0.02124  -0.1296   0.1677   0.3215
   9.250   1.4633   0.03215   0.02370  -0.1265   0.1590   0.3235
   9.500   1.4591   0.03454   0.02616  -0.1240   0.1510   0.3265
   9.750   1.4528   0.03737   0.02904  -0.1219   0.1436   0.3299
  10.000   1.4505   0.04006   0.03179  -0.1203   0.1359   0.3330
  10.250   1.4477   0.04292   0.03472  -0.1190   0.1283   0.3349
  10.500   1.4477   0.04562   0.03750  -0.1179   0.1215   0.3376
  10.750   1.4471   0.04844   0.04035  -0.1169   0.1130   0.3413
  11.000   1.4484   0.05109   0.04306  -0.1160   0.1033   0.3447
  11.250   1.4487   0.05390   0.04591  -0.1152   0.0922   0.3471
  11.500   1.4466   0.05699   0.04894  -0.1143   0.0752   0.3500
  11.750   1.4418   0.06041   0.05222  -0.1135   0.0560   0.3529
  12.000   1.4373   0.06379   0.05545  -0.1125   0.0401   0.3557
  12.250   1.4373   0.06670   0.05832  -0.1118   0.0320   0.3587
  12.500   1.4405   0.06929   0.06093  -0.1110   0.0275   0.3631
  12.750   1.4443   0.07186   0.06352  -0.1104   0.0250   0.3671
  13.000   1.4497   0.07429   0.06603  -0.1099   0.0234   0.3709
  13.250   1.4556   0.07668   0.06851  -0.1094   0.0219   0.3746
  13.500   1.4607   0.07921   0.07112  -0.1089   0.0207   0.3765
  13.750   1.4645   0.08194   0.07392  -0.1085   0.0195   0.3774
  14.000   1.4686   0.08468   0.07674  -0.1082   0.0186   0.3782
  14.250   1.4745   0.08717   0.07934  -0.1079   0.0178   0.3793
  14.500   1.4792   0.08985   0.08211  -0.1077   0.0172   0.3806
  14.750   1.4837   0.09256   0.08492  -0.1074   0.0166   0.3821
  15.000   1.4880   0.09531   0.08776  -0.1073   0.0161   0.3833
  15.250   1.4920   0.09811   0.09065  -0.1071   0.0156   0.3842
  15.500   1.4953   0.10100   0.09361  -0.1070   0.0152   0.3848
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