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S8035 for RC aerobatic 14% thick (s8035-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: S8035 for RC aerobatic 14% thick (s8035-il)
Reynolds number: 500,000
Max Cl/Cd: 70.55 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8035-il-500000.txt
Download as CSV file: xf-s8035-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8035 for RC aerobatic  14% thick               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -1.0863   0.10248   0.09856  -0.0223   1.0000   0.0210
 -18.500  -1.0943   0.09748   0.09347  -0.0248   1.0000   0.0213
 -18.250  -1.1039   0.09232   0.08821  -0.0272   1.0000   0.0217
 -18.000  -1.1123   0.08750   0.08329  -0.0294   1.0000   0.0219
 -17.750  -1.1205   0.08268   0.07837  -0.0317   1.0000   0.0223
 -17.500  -1.1285   0.07798   0.07355  -0.0338   1.0000   0.0227
 -17.250  -1.1356   0.07355   0.06900  -0.0358   1.0000   0.0229
 -17.000  -1.1398   0.06947   0.06480  -0.0376   1.0000   0.0232
 -16.750  -1.1517   0.06486   0.06011  -0.0392   1.0000   0.0236
 -16.500  -1.1626   0.06036   0.05556  -0.0408   1.0000   0.0242
 -16.250  -1.1701   0.05632   0.05144  -0.0423   1.0000   0.0246
 -16.000  -1.1767   0.05251   0.04755  -0.0435   1.0000   0.0251
 -15.750  -1.1795   0.04925   0.04420  -0.0445   1.0000   0.0255
 -15.500  -1.1826   0.04605   0.04091  -0.0453   1.0000   0.0260
 -15.250  -1.1828   0.04328   0.03804  -0.0459   1.0000   0.0267
 -15.000  -1.1823   0.04066   0.03533  -0.0462   1.0000   0.0273
 -14.750  -1.1799   0.03834   0.03290  -0.0463   1.0000   0.0279
 -14.500  -1.1778   0.03610   0.03056  -0.0462   1.0000   0.0286
 -14.250  -1.1842   0.03322   0.02760  -0.0458   1.0000   0.0293
 -14.000  -1.1843   0.03108   0.02541  -0.0451   1.0000   0.0302
 -13.750  -1.1802   0.02940   0.02368  -0.0442   1.0000   0.0312
 -13.500  -1.1742   0.02799   0.02220  -0.0431   1.0000   0.0323
 -13.250  -1.1667   0.02675   0.02087  -0.0419   1.0000   0.0335
 -13.000  -1.1578   0.02569   0.01972  -0.0405   1.0000   0.0346
 -12.750  -1.1597   0.02406   0.01805  -0.0381   1.0000   0.0360
 -12.500  -1.1544   0.02299   0.01695  -0.0358   1.0000   0.0377
 -12.250  -1.1455   0.02219   0.01610  -0.0337   1.0000   0.0394
 -12.000  -1.1343   0.02155   0.01539  -0.0316   1.0000   0.0412
 -11.750  -1.1323   0.02057   0.01438  -0.0282   1.0000   0.0434
 -11.500  -1.1264   0.01986   0.01367  -0.0250   1.0000   0.0459
 -11.250  -1.1175   0.01935   0.01311  -0.0220   1.0000   0.0484
 -11.000  -1.1104   0.01882   0.01252  -0.0185   1.0000   0.0509
 -10.750  -1.1029   0.01813   0.01185  -0.0153   1.0000   0.0545
 -10.500  -1.0888   0.01768   0.01137  -0.0130   1.0000   0.0579
 -10.250  -1.0761   0.01715   0.01080  -0.0105   1.0000   0.0617
 -10.000  -1.0628   0.01663   0.01030  -0.0081   1.0000   0.0659
  -9.750  -1.0461   0.01627   0.00990  -0.0061   1.0000   0.0697
  -9.500  -1.0325   0.01573   0.00937  -0.0037   1.0000   0.0746
  -9.250  -1.0163   0.01533   0.00898  -0.0017   1.0000   0.0796
  -9.000  -1.0002   0.01492   0.00856   0.0004   1.0000   0.0847
  -8.750  -0.9842   0.01452   0.00819   0.0025   1.0000   0.0911
  -8.500  -0.9677   0.01416   0.00782   0.0046   1.0000   0.0975
  -8.250  -0.9517   0.01380   0.00748   0.0067   1.0000   0.1046
  -8.000  -0.9359   0.01345   0.00715   0.0089   1.0000   0.1120
  -7.750  -0.9202   0.01316   0.00688   0.0110   1.0000   0.1199
  -7.500  -0.9059   0.01284   0.00660   0.0134   1.0000   0.1284
  -7.250  -0.8800   0.01254   0.00633   0.0135   0.9986   0.1395
  -7.000  -0.8427   0.01220   0.00605   0.0112   0.9954   0.1540
  -6.750  -0.8055   0.01186   0.00577   0.0090   0.9923   0.1695
  -6.500  -0.7701   0.01150   0.00547   0.0071   0.9878   0.1847
  -6.250  -0.7329   0.01117   0.00521   0.0050   0.9841   0.2009
  -6.000  -0.6972   0.01084   0.00494   0.0032   0.9795   0.2187
  -5.750  -0.6624   0.01051   0.00468   0.0016   0.9735   0.2366
  -5.500  -0.6245   0.01021   0.00443  -0.0006   0.9698   0.2546
  -5.250  -0.5935   0.00989   0.00418  -0.0013   0.9616   0.2726
  -5.000  -0.5569   0.00956   0.00393  -0.0032   0.9570   0.2927
  -4.750  -0.5235   0.00927   0.00371  -0.0044   0.9493   0.3130
  -4.500  -0.4862   0.00898   0.00349  -0.0063   0.9429   0.3352
  -4.250  -0.4519   0.00870   0.00329  -0.0077   0.9329   0.3557
  -4.000  -0.4163   0.00846   0.00309  -0.0092   0.9220   0.3764
  -3.750  -0.3834   0.00827   0.00291  -0.0101   0.9084   0.3955
  -3.500  -0.3546   0.00811   0.00277  -0.0102   0.8930   0.4148
  -3.000  -0.3021   0.00788   0.00256  -0.0092   0.8625   0.4510
  -2.750  -0.2768   0.00778   0.00248  -0.0084   0.8473   0.4701
  -2.500  -0.2516   0.00770   0.00240  -0.0077   0.8322   0.4891
  -2.250  -0.2266   0.00762   0.00233  -0.0069   0.8165   0.5087
  -2.000  -0.2018   0.00754   0.00227  -0.0061   0.8003   0.5282
  -1.750  -0.1768   0.00748   0.00221  -0.0053   0.7841   0.5470
  -1.500  -0.1516   0.00742   0.00216  -0.0045   0.7685   0.5649
  -1.250  -0.1263   0.00738   0.00212  -0.0038   0.7529   0.5820
  -1.000  -0.1009   0.00734   0.00208  -0.0030   0.7373   0.5998
  -0.750  -0.0756   0.00732   0.00206  -0.0023   0.7214   0.6181
  -0.500  -0.0503   0.00730   0.00204  -0.0016   0.7056   0.6363
  -0.250  -0.0251   0.00728   0.00203  -0.0008   0.6891   0.6542
   0.000   0.0000   0.00727   0.00203   0.0000   0.6718   0.6718
   0.250   0.0251   0.00728   0.00203   0.0008   0.6542   0.6891
   0.500   0.0503   0.00730   0.00204   0.0016   0.6363   0.7055
   0.750   0.0756   0.00732   0.00206   0.0023   0.6182   0.7214
   1.000   0.1009   0.00734   0.00208   0.0030   0.5998   0.7373
   1.250   0.1263   0.00738   0.00212   0.0038   0.5820   0.7528
   1.500   0.1516   0.00742   0.00216   0.0045   0.5649   0.7685
   1.750   0.1768   0.00748   0.00221   0.0052   0.5471   0.7841
   2.000   0.2018   0.00754   0.00227   0.0061   0.5282   0.8003
   2.250   0.2266   0.00762   0.00233   0.0069   0.5088   0.8166
   2.500   0.2516   0.00770   0.00240   0.0077   0.4891   0.8322
   2.750   0.2768   0.00779   0.00248   0.0084   0.4698   0.8474
   3.000   0.3021   0.00788   0.00256   0.0092   0.4512   0.8625
   3.500   0.3546   0.00811   0.00277   0.0102   0.4148   0.8930
   3.750   0.3834   0.00827   0.00291   0.0101   0.3957   0.9084
   4.000   0.4163   0.00846   0.00309   0.0092   0.3764   0.9219
   4.250   0.4519   0.00870   0.00329   0.0077   0.3559   0.9329
   4.500   0.4862   0.00898   0.00349   0.0063   0.3352   0.9429
   4.750   0.5235   0.00927   0.00371   0.0043   0.3128   0.9493
   5.000   0.5569   0.00956   0.00393   0.0032   0.2926   0.9570
   5.250   0.5935   0.00989   0.00418   0.0013   0.2722   0.9616
   5.500   0.6245   0.01021   0.00443   0.0006   0.2546   0.9698
   5.750   0.6625   0.01051   0.00468  -0.0016   0.2366   0.9735
   6.000   0.6972   0.01084   0.00494  -0.0032   0.2185   0.9795
   6.250   0.7328   0.01117   0.00521  -0.0050   0.2010   0.9841
   6.500   0.7702   0.01150   0.00547  -0.0072   0.1848   0.9878
   6.750   0.8055   0.01186   0.00577  -0.0090   0.1693   0.9923
   7.000   0.8428   0.01220   0.00605  -0.0112   0.1541   0.9954
   7.250   0.8801   0.01254   0.00633  -0.0135   0.1394   0.9986
   7.500   0.9059   0.01284   0.00660  -0.0134   0.1284   1.0000
   7.750   0.9202   0.01316   0.00687  -0.0110   0.1199   1.0000
   8.000   0.9359   0.01345   0.00715  -0.0089   0.1119   1.0000
   8.250   0.9517   0.01379   0.00748  -0.0067   0.1046   1.0000
   8.500   0.9677   0.01416   0.00782  -0.0046   0.0975   1.0000
   8.750   0.9842   0.01452   0.00819  -0.0025   0.0912   1.0000
   9.000   1.0002   0.01492   0.00856  -0.0004   0.0849   1.0000
   9.250   1.0163   0.01533   0.00898   0.0016   0.0795   1.0000
   9.500   1.0326   0.01573   0.00937   0.0037   0.0746   1.0000
   9.750   1.0461   0.01627   0.00990   0.0061   0.0697   1.0000
  10.000   1.0628   0.01662   0.01030   0.0081   0.0659   1.0000
  10.250   1.0762   0.01715   0.01080   0.0105   0.0617   1.0000
  10.500   1.0888   0.01769   0.01137   0.0130   0.0580   1.0000
  10.750   1.1029   0.01813   0.01185   0.0152   0.0546   1.0000
  11.000   1.1104   0.01883   0.01252   0.0185   0.0509   1.0000
  11.250   1.1178   0.01935   0.01310   0.0219   0.0484   1.0000
  11.500   1.1267   0.01986   0.01366   0.0249   0.0459   1.0000
  11.750   1.1330   0.02055   0.01436   0.0281   0.0436   1.0000
  12.000   1.1347   0.02155   0.01539   0.0316   0.0412   1.0000
  12.250   1.1457   0.02219   0.01610   0.0337   0.0395   1.0000
  12.500   1.1551   0.02297   0.01693   0.0358   0.0376   1.0000
  12.750   1.1608   0.02401   0.01800   0.0379   0.0360   1.0000
  13.000   1.1583   0.02568   0.01970   0.0404   0.0344   1.0000
  13.250   1.1674   0.02673   0.02086   0.0418   0.0334   1.0000
  13.500   1.1748   0.02796   0.02217   0.0431   0.0323   1.0000
  13.750   1.1813   0.02936   0.02363   0.0441   0.0312   1.0000
  14.000   1.1854   0.03103   0.02535   0.0450   0.0301   1.0000
  14.250   1.1849   0.03322   0.02760   0.0457   0.0294   1.0000
  14.500   1.1772   0.03621   0.03066   0.0461   0.0284   1.0000
  14.750   1.1811   0.03830   0.03285   0.0462   0.0279   1.0000
  15.000   1.1837   0.04060   0.03526   0.0461   0.0272   1.0000
  15.250   1.1853   0.04310   0.03786   0.0457   0.0265   1.0000
  15.500   1.1837   0.04603   0.04090   0.0452   0.0261   1.0000
  15.750   1.1817   0.04912   0.04407   0.0444   0.0255   1.0000
  16.000   1.1774   0.05255   0.04759   0.0433   0.0250   1.0000
  16.250   1.1723   0.05621   0.05132   0.0420   0.0244   1.0000
  16.500   1.1640   0.06033   0.05552   0.0406   0.0241   1.0000
  16.750   1.1542   0.06471   0.05996   0.0390   0.0236   1.0000
  17.000   1.1436   0.06922   0.06456   0.0374   0.0232   1.0000
  17.250   1.1370   0.07351   0.06896   0.0356   0.0229   1.0000
  17.500   1.1307   0.07793   0.07351   0.0335   0.0226   1.0000
  17.750   1.1225   0.08254   0.07823   0.0316   0.0224   1.0000
  18.000   1.1147   0.08734   0.08313   0.0293   0.0220   1.0000
  18.250   1.1056   0.09233   0.08822   0.0269   0.0216   1.0000
  18.500   1.0968   0.09735   0.09334   0.0245   0.0213   1.0000
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