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SA7036 (sa7036-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SA7036 (sa7036-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.99 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sa7036-il-1000000.txt
Download as CSV file: xf-sa7036-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SA7036                                          
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.3924   0.08194   0.08039  -0.0328   1.0000   0.0084
  -8.250  -0.3950   0.07836   0.07683  -0.0339   1.0000   0.0084
  -8.000  -0.4019   0.07499   0.07352  -0.0345   1.0000   0.0086
  -7.750  -0.4184   0.07268   0.07125  -0.0328   0.9996   0.0085
  -7.500  -0.3981   0.06459   0.06316  -0.0466   0.9938   0.0087
  -7.250  -0.3758   0.05406   0.05253  -0.0625   0.9875   0.0090
  -7.000  -0.3808   0.02376   0.02071  -0.0799   0.9736   0.0073
  -6.250  -0.3169   0.01851   0.01483  -0.0789   0.9548   0.0082
  -6.000  -0.2971   0.01606   0.01199  -0.0776   0.9473   0.0082
  -5.750  -0.2744   0.01470   0.01038  -0.0766   0.9416   0.0083
  -5.500  -0.2505   0.01344   0.00893  -0.0759   0.9350   0.0084
  -5.250  -0.2259   0.01274   0.00810  -0.0751   0.9293   0.0089
  -5.000  -0.2005   0.01203   0.00729  -0.0746   0.9226   0.0093
  -4.750  -0.1756   0.01113   0.00624  -0.0738   0.9158   0.0096
  -4.500  -0.1498   0.01040   0.00540  -0.0733   0.9086   0.0099
  -4.250  -0.1234   0.01005   0.00496  -0.0728   0.9016   0.0103
  -4.000  -0.0985   0.00889   0.00367  -0.0722   0.8940   0.0116
  -3.750  -0.0720   0.00852   0.00324  -0.0718   0.8867   0.0125
  -3.500  -0.0447   0.00819   0.00286  -0.0716   0.8783   0.0135
  -3.250  -0.0176   0.00798   0.00258  -0.0713   0.8700   0.0147
  -3.000   0.0097   0.00758   0.00209  -0.0710   0.8602   0.0171
  -2.750   0.0372   0.00737   0.00182  -0.0708   0.8499   0.0197
  -2.500   0.0646   0.00713   0.00157  -0.0706   0.8389   0.0312
  -2.250   0.0913   0.00671   0.00137  -0.0704   0.8268   0.0987
  -2.000   0.1183   0.00642   0.00123  -0.0703   0.8141   0.1621
  -1.750   0.1454   0.00615   0.00113  -0.0702   0.8004   0.2299
  -1.500   0.1723   0.00587   0.00105  -0.0701   0.7856   0.3137
  -1.250   0.1992   0.00560   0.00099  -0.0701   0.7701   0.4064
  -1.000   0.2260   0.00535   0.00095  -0.0699   0.7537   0.4978
  -0.750   0.2525   0.00512   0.00095  -0.0697   0.7364   0.5976
  -0.500   0.2790   0.00497   0.00095  -0.0693   0.7186   0.6762
  -0.250   0.3053   0.00488   0.00096  -0.0689   0.7008   0.7391
   0.000   0.3312   0.00480   0.00098  -0.0684   0.6829   0.7987
   0.250   0.3559   0.00473   0.00101  -0.0675   0.6647   0.8568
   0.500   0.3789   0.00470   0.00105  -0.0661   0.6470   0.9130
   0.750   0.4053   0.00472   0.00106  -0.0655   0.6288   0.9623
   1.000   0.4439   0.00480   0.00105  -0.0678   0.6081   0.9912
   1.250   0.4762   0.00493   0.00107  -0.0688   0.5861   1.0000
   1.500   0.5025   0.00506   0.00111  -0.0685   0.5655   1.0000
   1.750   0.5289   0.00521   0.00115  -0.0682   0.5459   1.0000
   2.000   0.5556   0.00535   0.00121  -0.0680   0.5266   1.0000
   2.250   0.5823   0.00549   0.00127  -0.0678   0.5073   1.0000
   2.500   0.6090   0.00566   0.00134  -0.0675   0.4876   1.0000
   2.750   0.6359   0.00581   0.00142  -0.0674   0.4692   1.0000
   3.000   0.6626   0.00598   0.00152  -0.0672   0.4495   1.0000
   3.250   0.6892   0.00617   0.00162  -0.0670   0.4287   1.0000
   3.500   0.7158   0.00637   0.00172  -0.0668   0.4061   1.0000
   3.750   0.7423   0.00658   0.00184  -0.0666   0.3861   1.0000
   4.000   0.7689   0.00677   0.00198  -0.0664   0.3667   1.0000
   4.500   0.8218   0.00721   0.00227  -0.0660   0.3284   1.0000
   4.750   0.8481   0.00744   0.00242  -0.0658   0.3092   1.0000
   5.250   0.9002   0.00795   0.00280  -0.0654   0.2698   1.0000
   5.500   0.9258   0.00825   0.00300  -0.0651   0.2484   1.0000
   5.750   0.9516   0.00853   0.00321  -0.0648   0.2300   1.0000
   6.000   0.9772   0.00883   0.00345  -0.0645   0.2107   1.0000
   6.250   1.0023   0.00917   0.00371  -0.0642   0.1913   1.0000
   6.500   1.0274   0.00950   0.00397  -0.0639   0.1723   1.0000
   6.750   1.0521   0.00988   0.00426  -0.0635   0.1533   1.0000
   7.000   1.0767   0.01025   0.00458  -0.0631   0.1371   1.0000
   7.250   1.1013   0.01062   0.00489  -0.0627   0.1216   1.0000
   7.500   1.1254   0.01103   0.00524  -0.0622   0.1047   1.0000
   7.750   1.1485   0.01154   0.00564  -0.0616   0.0864   1.0000
   8.000   1.1717   0.01203   0.00605  -0.0610   0.0707   1.0000
   8.250   1.1946   0.01253   0.00650  -0.0604   0.0571   1.0000
   8.500   1.2171   0.01306   0.00697  -0.0597   0.0449   1.0000
   8.750   1.2395   0.01358   0.00745  -0.0590   0.0362   1.0000
   9.000   1.2614   0.01414   0.00798  -0.0583   0.0287   1.0000
   9.250   1.2838   0.01461   0.00846  -0.0576   0.0245   1.0000
   9.500   1.3053   0.01516   0.00901  -0.0567   0.0199   1.0000
   9.750   1.3261   0.01573   0.00959  -0.0559   0.0160   1.0000
  10.000   1.3464   0.01634   0.01020  -0.0549   0.0119   1.0000
  10.250   1.3646   0.01711   0.01096  -0.0536   0.0078   1.0000
  10.500   1.3818   0.01793   0.01182  -0.0522   0.0054   1.0000
  10.750   1.3962   0.01896   0.01292  -0.0503   0.0042   1.0000
  11.000   1.4136   0.01962   0.01366  -0.0490   0.0040   1.0000
  11.250   1.4290   0.02040   0.01452  -0.0473   0.0037   1.0000
  11.500   1.4416   0.02117   0.01538  -0.0452   0.0035   1.0000
  11.750   1.4514   0.02199   0.01630  -0.0427   0.0033   1.0000
  12.000   1.4595   0.02293   0.01733  -0.0401   0.0032   1.0000
  12.250   1.4662   0.02400   0.01848  -0.0375   0.0030   1.0000
  12.500   1.4704   0.02528   0.01987  -0.0348   0.0029   1.0000
  12.750   1.4700   0.02694   0.02166  -0.0320   0.0028   1.0000
  13.000   1.4630   0.02922   0.02410  -0.0289   0.0026   1.0000
  13.250   1.4631   0.03110   0.02611  -0.0270   0.0026   1.0000
  13.500   1.4607   0.03334   0.02848  -0.0253   0.0026   1.0000
  13.750   1.4637   0.03527   0.03051  -0.0242   0.0025   1.0000
  14.000   1.4587   0.03810   0.03348  -0.0232   0.0025   1.0000
  14.250   1.4605   0.04046   0.03595  -0.0227   0.0024   1.0000
  14.500   1.4558   0.04372   0.03934  -0.0226   0.0023   1.0000
  14.750   1.4496   0.04737   0.04313  -0.0230   0.0023   1.0000
  15.000   1.4420   0.05150   0.04739  -0.0239   0.0023   1.0000
  15.250   1.4321   0.05622   0.05225  -0.0253   0.0022   1.0000
  15.500   1.4210   0.06142   0.05759  -0.0273   0.0022   1.0000
  15.750   1.4075   0.06730   0.06363  -0.0298   0.0022   1.0000
  16.000   1.3947   0.07336   0.06984  -0.0326   0.0022   1.0000
  16.250   1.3783   0.08035   0.07697  -0.0360   0.0022   1.0000
  16.500   1.3600   0.08792   0.08470  -0.0398   0.0023   1.0000
  16.750   1.3456   0.09512   0.09202  -0.0436   0.0022   1.0000
  17.000   1.3288   0.10297   0.10000  -0.0478   0.0021   1.0000
  17.250   1.3098   0.11143   0.10859  -0.0524   0.0021   1.0000
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