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SA7036 (sa7036-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SA7036 (sa7036-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.5 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sa7036-il-1000000-n5.txt
Download as CSV file: xf-sa7036-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.4067   0.10136   0.09969  -0.0250   1.0000   0.0036
  -9.750  -0.4079   0.09668   0.09504  -0.0267   1.0000   0.0034
  -8.750  -0.5787   0.02232   0.01924  -0.0759   0.9648   0.0027
  -8.500  -0.5610   0.01980   0.01634  -0.0756   0.9573   0.0027
  -8.250  -0.5469   0.01642   0.01239  -0.0746   0.9489   0.0029
  -8.000  -0.5241   0.01542   0.01122  -0.0741   0.9431   0.0031
  -7.750  -0.4998   0.01471   0.01038  -0.0737   0.9372   0.0032
  -7.500  -0.4749   0.01418   0.00974  -0.0733   0.9315   0.0034
  -7.250  -0.4497   0.01364   0.00910  -0.0729   0.9262   0.0036
  -7.000  -0.4244   0.01304   0.00839  -0.0726   0.9200   0.0038
  -6.500  -0.3732   0.01191   0.00703  -0.0719   0.9076   0.0042
  -6.250  -0.3476   0.01137   0.00638  -0.0715   0.9009   0.0044
  -6.000  -0.3212   0.01091   0.00580  -0.0712   0.8939   0.0046
  -5.750  -0.2948   0.01052   0.00532  -0.0709   0.8868   0.0048
  -5.500  -0.2684   0.00996   0.00467  -0.0707   0.8794   0.0052
  -5.000  -0.2142   0.00952   0.00416  -0.0704   0.8632   0.0062
  -4.750  -0.1871   0.00931   0.00389  -0.0702   0.8531   0.0070
  -4.500  -0.1599   0.00911   0.00360  -0.0700   0.8420   0.0075
  -4.250  -0.1329   0.00880   0.00320  -0.0698   0.8307   0.0080
  -4.000  -0.1058   0.00846   0.00280  -0.0696   0.8194   0.0090
  -3.750  -0.0783   0.00826   0.00254  -0.0694   0.8076   0.0098
  -3.500  -0.0508   0.00811   0.00232  -0.0693   0.7947   0.0108
  -3.250  -0.0233   0.00799   0.00212  -0.0692   0.7802   0.0115
  -3.000   0.0041   0.00786   0.00189  -0.0690   0.7645   0.0119
  -2.750   0.0315   0.00772   0.00165  -0.0688   0.7474   0.0130
  -2.500   0.0590   0.00762   0.00147  -0.0687   0.7297   0.0150
  -2.250   0.0865   0.00755   0.00133  -0.0685   0.7115   0.0181
  -2.000   0.1138   0.00740   0.00120  -0.0684   0.6937   0.0414
  -1.500   0.1685   0.00714   0.00102  -0.0683   0.6596   0.1075
  -1.250   0.1959   0.00702   0.00095  -0.0682   0.6422   0.1460
  -1.000   0.2232   0.00689   0.00090  -0.0682   0.6244   0.1976
  -0.750   0.2501   0.00663   0.00087  -0.0682   0.6065   0.2947
  -0.500   0.2769   0.00639   0.00086  -0.0682   0.5884   0.3968
  -0.250   0.3040   0.00626   0.00086  -0.0682   0.5695   0.4678
   0.000   0.3311   0.00617   0.00088  -0.0681   0.5514   0.5322
   0.250   0.3582   0.00613   0.00091  -0.0680   0.5336   0.5874
   0.500   0.3855   0.00610   0.00094  -0.0679   0.5169   0.6339
   0.750   0.4126   0.00608   0.00098  -0.0678   0.5001   0.6812
   1.000   0.4392   0.00607   0.00104  -0.0675   0.4816   0.7320
   1.250   0.4655   0.00608   0.00111  -0.0672   0.4617   0.7792
   1.500   0.4911   0.00608   0.00118  -0.0666   0.4407   0.8302
   1.750   0.5148   0.00607   0.00126  -0.0656   0.4231   0.8872
   2.000   0.5378   0.00610   0.00133  -0.0643   0.4074   0.9432
   2.250   0.5712   0.00620   0.00139  -0.0655   0.3891   0.9829
   2.500   0.6034   0.00634   0.00146  -0.0666   0.3732   1.0000
   2.750   0.6302   0.00651   0.00154  -0.0664   0.3567   1.0000
   3.000   0.6569   0.00668   0.00165  -0.0662   0.3397   1.0000
   3.500   0.7100   0.00708   0.00188  -0.0659   0.3021   1.0000
   3.750   0.7365   0.00730   0.00201  -0.0657   0.2837   1.0000
   4.250   0.7895   0.00771   0.00230  -0.0653   0.2534   1.0000
   4.500   0.8159   0.00793   0.00245  -0.0651   0.2382   1.0000
   4.750   0.8422   0.00816   0.00262  -0.0649   0.2223   1.0000
   5.000   0.8684   0.00839   0.00281  -0.0647   0.2079   1.0000
   5.250   0.8942   0.00866   0.00301  -0.0645   0.1906   1.0000
   5.500   0.9197   0.00897   0.00323  -0.0642   0.1721   1.0000
   5.750   0.9453   0.00926   0.00346  -0.0639   0.1569   1.0000
   6.000   0.9707   0.00957   0.00370  -0.0636   0.1418   1.0000
   6.250   0.9961   0.00986   0.00396  -0.0633   0.1295   1.0000
   6.500   1.0210   0.01022   0.00425  -0.0629   0.1126   1.0000
   6.750   1.0456   0.01058   0.00455  -0.0625   0.0975   1.0000
   7.000   1.0701   0.01097   0.00487  -0.0621   0.0840   1.0000
   7.250   1.0938   0.01142   0.00525  -0.0615   0.0685   1.0000
   7.500   1.1171   0.01190   0.00565  -0.0610   0.0538   1.0000
   7.750   1.1407   0.01233   0.00604  -0.0604   0.0436   1.0000
   8.000   1.1642   0.01278   0.00645  -0.0599   0.0350   1.0000
   8.250   1.1871   0.01325   0.00689  -0.0593   0.0272   1.0000
   8.500   1.2098   0.01373   0.00735  -0.0586   0.0208   1.0000
   8.750   1.2320   0.01425   0.00785  -0.0579   0.0153   1.0000
   9.000   1.2536   0.01480   0.00839  -0.0571   0.0109   1.0000
   9.250   1.2755   0.01530   0.00890  -0.0563   0.0081   1.0000
   9.500   1.2958   0.01593   0.00952  -0.0554   0.0046   1.0000
   9.750   1.3159   0.01656   0.01017  -0.0543   0.0027   1.0000
  10.000   1.3360   0.01714   0.01080  -0.0533   0.0021   1.0000
  10.250   1.3554   0.01775   0.01147  -0.0522   0.0018   1.0000
  10.500   1.3741   0.01838   0.01218  -0.0510   0.0016   1.0000
  10.750   1.3926   0.01899   0.01285  -0.0498   0.0015   1.0000
  11.000   1.4100   0.01964   0.01357  -0.0484   0.0014   1.0000
  11.250   1.4264   0.02030   0.01431  -0.0470   0.0013   1.0000
  11.500   1.4393   0.02101   0.01510  -0.0449   0.0012   1.0000
  11.750   1.4506   0.02174   0.01590  -0.0426   0.0012   1.0000
  12.000   1.4597   0.02263   0.01688  -0.0401   0.0010   1.0000
  12.250   1.4694   0.02350   0.01784  -0.0379   0.0011   1.0000
  12.500   1.4765   0.02458   0.01901  -0.0355   0.0010   1.0000
  12.750   1.4836   0.02571   0.02023  -0.0334   0.0009   1.0000
  13.000   1.4874   0.02712   0.02177  -0.0311   0.0008   1.0000
  13.250   1.4910   0.02862   0.02338  -0.0290   0.0008   1.0000
  13.500   1.4889   0.03067   0.02558  -0.0268   0.0008   1.0000
  13.750   1.4908   0.03252   0.02753  -0.0253   0.0008   1.0000
  14.000   1.4817   0.03552   0.03070  -0.0236   0.0007   1.0000
  14.250   1.4790   0.03814   0.03346  -0.0227   0.0007   1.0000
  14.500   1.4766   0.04092   0.03636  -0.0223   0.0007   1.0000
  14.750   1.4727   0.04409   0.03965  -0.0222   0.0007   1.0000
  15.000   1.4661   0.04780   0.04349  -0.0227   0.0007   1.0000
  15.250   1.4594   0.05181   0.04764  -0.0236   0.0007   1.0000
  15.500   1.4492   0.05655   0.05252  -0.0251   0.0007   1.0000
  15.750   1.4386   0.06167   0.05778  -0.0270   0.0007   1.0000
  16.000   1.4274   0.06719   0.06344  -0.0294   0.0007   1.0000
  16.250   1.4111   0.07388   0.07028  -0.0326   0.0007   1.0000
  16.500   1.3919   0.08146   0.07802  -0.0364   0.0007   1.0000
  16.750   1.3740   0.08906   0.08576  -0.0403   0.0007   1.0000
  17.000   1.3548   0.09724   0.09408  -0.0447   0.0007   1.0000
  17.250   1.3330   0.10618   0.10317  -0.0495   0.0007   1.0000
  17.500   1.3098   0.11571   0.11284  -0.0548   0.0007   1.0000
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