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S8038 (13%) (s8038-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: S8038 (13%) (s8038-il)
Reynolds number: 50,000
Max Cl/Cd: 30.33 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8038-il-50000-n5.txt
Download as CSV file: xf-s8038-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8038 (13%)                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.5917   0.09482   0.08715  -0.0359   1.0000   0.0486
 -11.500  -0.6230   0.08459   0.07689  -0.0426   1.0000   0.0474
 -11.250  -0.6613   0.07561   0.06777  -0.0483   1.0000   0.0464
 -11.000  -0.6939   0.06926   0.06126  -0.0511   1.0000   0.0458
 -10.750  -0.7205   0.06460   0.05638  -0.0515   1.0000   0.0455
 -10.500  -0.7403   0.06107   0.05266  -0.0500   1.0000   0.0454
 -10.250  -0.7550   0.05815   0.04957  -0.0474   1.0000   0.0456
 -10.000  -0.7635   0.05528   0.04648  -0.0449   1.0000   0.0458
  -9.750  -0.7668   0.05252   0.04350  -0.0426   1.0000   0.0463
  -9.500  -0.7662   0.04987   0.04060  -0.0403   1.0000   0.0470
  -9.250  -0.7622   0.04733   0.03780  -0.0381   1.0000   0.0478
  -9.000  -0.7550   0.04491   0.03512  -0.0360   1.0000   0.0490
  -8.750  -0.7456   0.04268   0.03257  -0.0339   1.0000   0.0510
  -8.500  -0.7335   0.04055   0.03008  -0.0319   1.0000   0.0533
  -8.250  -0.7189   0.03882   0.02840  -0.0304   1.0000   0.0559
  -8.000  -0.7028   0.03716   0.02663  -0.0288   1.0000   0.0589
  -7.750  -0.6840   0.03546   0.02469  -0.0271   1.0000   0.0624
  -7.500  -0.6681   0.03397   0.02319  -0.0254   1.0000   0.0666
  -7.250  -0.6535   0.03267   0.02184  -0.0234   1.0000   0.0733
  -7.000  -0.6404   0.03134   0.02053  -0.0212   1.0000   0.0809
  -6.750  -0.6279   0.03010   0.01927  -0.0189   1.0000   0.0912
  -6.500  -0.6175   0.02884   0.01812  -0.0164   1.0000   0.1064
  -6.250  -0.6078   0.02759   0.01697  -0.0139   1.0000   0.1289
  -6.000  -0.5993   0.02631   0.01592  -0.0112   1.0000   0.1597
  -5.750  -0.5915   0.02508   0.01502  -0.0085   1.0000   0.1993
  -5.500  -0.5833   0.02400   0.01423  -0.0057   1.0000   0.2508
  -5.250  -0.5751   0.02305   0.01365  -0.0029   1.0000   0.3088
  -5.000  -0.5660   0.02232   0.01324   0.0001   1.0000   0.3713
  -4.750  -0.5555   0.02183   0.01306   0.0032   1.0000   0.4321
  -4.500  -0.5437   0.02161   0.01304   0.0063   1.0000   0.4879
  -4.250  -0.5312   0.02157   0.01311   0.0094   1.0000   0.5359
  -4.000  -0.5185   0.02160   0.01314   0.0123   1.0000   0.5778
  -3.750  -0.5055   0.02169   0.01320   0.0153   1.0000   0.6126
  -3.500  -0.4808   0.02189   0.01332   0.0160   0.9949   0.6475
  -3.250  -0.4452   0.02214   0.01346   0.0149   0.9846   0.6810
  -3.000  -0.4103   0.02234   0.01353   0.0139   0.9739   0.7094
  -2.750  -0.3766   0.02245   0.01350   0.0130   0.9629   0.7355
  -2.500  -0.3404   0.02262   0.01356   0.0120   0.9528   0.7575
  -2.250  -0.3016   0.02274   0.01353   0.0102   0.9435   0.7793
  -2.000  -0.2680   0.02278   0.01347   0.0093   0.9321   0.7993
  -1.750  -0.2299   0.02286   0.01345   0.0077   0.9221   0.8168
  -1.500  -0.1851   0.02294   0.01340   0.0048   0.9139   0.8334
  -1.250  -0.1467   0.02298   0.01336   0.0029   0.9031   0.8490
  -1.000  -0.1011   0.02301   0.01327  -0.0003   0.8946   0.8633
  -0.750  -0.0540   0.02303   0.01321  -0.0038   0.8853   0.8761
  -0.500  -0.0040   0.02305   0.01316  -0.0080   0.8760   0.8869
  -0.250   0.0473   0.02299   0.01303  -0.0124   0.8673   0.8975
   0.000   0.0892   0.02295   0.01294  -0.0152   0.8553   0.9092
   0.250   0.1431   0.02287   0.01283  -0.0201   0.8449   0.9167
   0.500   0.1921   0.02272   0.01264  -0.0241   0.8346   0.9260
   0.750   0.2396   0.02263   0.01254  -0.0280   0.8213   0.9339
   1.000   0.2820   0.02254   0.01244  -0.0309   0.8075   0.9434
   1.250   0.3253   0.02242   0.01233  -0.0340   0.7934   0.9525
   1.500   0.3679   0.02230   0.01223  -0.0368   0.7783   0.9614
   1.750   0.4078   0.02219   0.01213  -0.0392   0.7622   0.9713
   2.000   0.4480   0.02206   0.01203  -0.0417   0.7452   0.9811
   2.250   0.4883   0.02191   0.01190  -0.0441   0.7273   0.9909
   2.500   0.5269   0.02176   0.01176  -0.0462   0.7087   1.0000
   2.750   0.5419   0.02177   0.01177  -0.0440   0.6903   1.0000
   3.000   0.5551   0.02181   0.01182  -0.0415   0.6708   1.0000
   3.250   0.5689   0.02185   0.01185  -0.0389   0.6512   1.0000
   3.500   0.5838   0.02186   0.01184  -0.0364   0.6315   1.0000
   3.750   0.5982   0.02191   0.01188  -0.0338   0.6112   1.0000
   4.000   0.6113   0.02203   0.01199  -0.0311   0.5894   1.0000
   4.250   0.6272   0.02210   0.01202  -0.0286   0.5677   1.0000
   4.500   0.6414   0.02227   0.01217  -0.0260   0.5440   1.0000
   4.750   0.6577   0.02241   0.01226  -0.0235   0.5197   1.0000
   5.000   0.6721   0.02264   0.01247  -0.0210   0.4929   1.0000
   5.250   0.6870   0.02290   0.01266  -0.0184   0.4647   1.0000
   5.500   0.7019   0.02322   0.01288  -0.0159   0.4355   1.0000
   5.750   0.7162   0.02361   0.01319  -0.0134   0.4048   1.0000
   6.000   0.7299   0.02411   0.01354  -0.0109   0.3737   1.0000
   6.250   0.7435   0.02470   0.01399  -0.0084   0.3436   1.0000
   6.500   0.7567   0.02540   0.01453  -0.0061   0.3157   1.0000
   6.750   0.7697   0.02618   0.01518  -0.0038   0.2899   1.0000
   7.000   0.7835   0.02703   0.01593  -0.0017   0.2674   1.0000
   7.250   0.7976   0.02793   0.01674   0.0002   0.2476   1.0000
   7.500   0.8122   0.02888   0.01761   0.0020   0.2307   1.0000
   7.750   0.8280   0.02986   0.01856   0.0037   0.2161   1.0000
   8.000   0.8439   0.03087   0.01958   0.0052   0.2028   1.0000
   8.250   0.8601   0.03192   0.02062   0.0067   0.1909   1.0000
   8.500   0.8783   0.03301   0.02164   0.0078   0.1816   1.0000
   8.750   0.8961   0.03417   0.02293   0.0090   0.1720   1.0000
   9.000   0.9137   0.03537   0.02418   0.0102   0.1635   1.0000
   9.250   0.9307   0.03656   0.02543   0.0114   0.1558   1.0000
   9.500   0.9497   0.03797   0.02695   0.0123   0.1494   1.0000
   9.750   0.9657   0.03937   0.02850   0.0135   0.1430   1.0000
  10.000   0.9834   0.04074   0.02988   0.0144   0.1373   1.0000
  10.250   0.9936   0.04245   0.03189   0.0161   0.1317   1.0000
  10.500   1.0086   0.04401   0.03355   0.0172   0.1272   1.0000
  10.750   1.0228   0.04572   0.03533   0.0183   0.1229   1.0000
  11.000   1.0232   0.04782   0.03778   0.0208   0.1190   1.0000
  11.250   1.0267   0.04968   0.03981   0.0229   0.1152   1.0000
  11.500   1.0389   0.05132   0.04149   0.0240   0.1117   1.0000
  11.750   1.0388   0.05375   0.04411   0.0259   0.1092   1.0000
  12.000   1.0243   0.05682   0.04751   0.0282   0.1072   1.0000
  12.250   1.0086   0.06024   0.05121   0.0297   0.1052   1.0000
  12.500   0.9912   0.06405   0.05526   0.0304   0.1035   1.0000
  12.750   0.9710   0.06855   0.05996   0.0301   0.1022   1.0000
  13.000   0.9430   0.07442   0.06602   0.0284   0.1014   1.0000
  13.250   0.8516   0.09114   0.08298   0.0189   0.1042   1.0000
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