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S8035 for RC aerobatic 14% thick (s8035-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: S8035 for RC aerobatic 14% thick (s8035-il)
Reynolds number: 100,000
Max Cl/Cd: 39.33 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8035-il-100000-n5.txt
Download as CSV file: xf-s8035-il-100000-n5.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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8211   0.11730   0.11149  -0.0154   1.0000   0.0477
 -16.000  -0.8922   0.09840   0.09230  -0.0267   1.0000   0.0473
 -15.750  -0.9226   0.08904   0.08272  -0.0321   1.0000   0.0474
 -15.500  -0.9456   0.08158   0.07503  -0.0362   1.0000   0.0479
 -15.250  -0.9634   0.07537   0.06861  -0.0394   1.0000   0.0486
 -15.000  -0.9779   0.06998   0.06298  -0.0419   1.0000   0.0493
 -14.750  -0.9875   0.06554   0.05838  -0.0435   1.0000   0.0502
 -14.500  -0.9903   0.06233   0.05515  -0.0444   1.0000   0.0515
 -14.250  -0.9942   0.05904   0.05179  -0.0454   1.0000   0.0527
 -14.000  -0.9985   0.05580   0.04845  -0.0462   1.0000   0.0542
 -13.750  -1.0022   0.05271   0.04522  -0.0466   1.0000   0.0559
 -13.500  -1.0054   0.04976   0.04208  -0.0469   1.0000   0.0578
 -13.250  -1.0068   0.04709   0.03921  -0.0467   1.0000   0.0598
 -13.000  -1.0062   0.04486   0.03698  -0.0463   1.0000   0.0615
 -12.750  -1.0056   0.04276   0.03482  -0.0457   1.0000   0.0636
 -12.500  -1.0041   0.04080   0.03275  -0.0448   1.0000   0.0663
 -12.250  -1.0010   0.03897   0.03072  -0.0437   1.0000   0.0693
 -12.000  -0.9982   0.03726   0.02898  -0.0423   1.0000   0.0719
 -11.750  -0.9952   0.03578   0.02745  -0.0408   1.0000   0.0748
 -11.500  -0.9904   0.03442   0.02599  -0.0390   1.0000   0.0786
 -11.250  -0.9842   0.03315   0.02458  -0.0371   1.0000   0.0825
 -11.000  -0.9804   0.03196   0.02341  -0.0348   1.0000   0.0860
 -10.750  -0.9742   0.03095   0.02231  -0.0323   1.0000   0.0906
 -10.500  -0.9670   0.02997   0.02122  -0.0298   1.0000   0.0954
 -10.250  -0.9621   0.02905   0.02032  -0.0269   1.0000   0.0998
 -10.000  -0.9526   0.02821   0.01938  -0.0244   1.0000   0.1058
  -9.750  -0.9435   0.02733   0.01851  -0.0219   1.0000   0.1115
  -9.500  -0.9323   0.02656   0.01768  -0.0196   1.0000   0.1182
  -9.250  -0.9211   0.02577   0.01689  -0.0173   1.0000   0.1250
  -9.000  -0.9084   0.02507   0.01612  -0.0150   1.0000   0.1328
  -8.750  -0.8959   0.02435   0.01541  -0.0128   1.0000   0.1402
  -8.500  -0.8815   0.02373   0.01470  -0.0107   1.0000   0.1494
  -8.250  -0.8686   0.02305   0.01409  -0.0084   1.0000   0.1578
  -8.000  -0.8538   0.02245   0.01346  -0.0063   1.0000   0.1673
  -7.750  -0.8389   0.02189   0.01286  -0.0043   1.0000   0.1777
  -7.500  -0.8245   0.02132   0.01234  -0.0021   1.0000   0.1882
  -7.250  -0.8093   0.02080   0.01183  -0.0001   1.0000   0.1994
  -7.000  -0.7938   0.02032   0.01135   0.0020   1.0000   0.2118
  -6.750  -0.7783   0.01987   0.01091   0.0040   1.0000   0.2252
  -6.500  -0.7632   0.01944   0.01049   0.0061   1.0000   0.2387
  -6.250  -0.7484   0.01903   0.01012   0.0083   1.0000   0.2531
  -6.000  -0.7335   0.01865   0.00979   0.0105   1.0000   0.2678
  -5.750  -0.7188   0.01831   0.00949   0.0126   1.0000   0.2830
  -5.500  -0.7041   0.01800   0.00920   0.0148   1.0000   0.2985
  -5.250  -0.6893   0.01772   0.00896   0.0169   1.0000   0.3143
  -5.000  -0.6538   0.01744   0.00872   0.0149   0.9932   0.3358
  -4.750  -0.6181   0.01714   0.00847   0.0130   0.9847   0.3576
  -4.500  -0.5832   0.01687   0.00823   0.0113   0.9754   0.3801
  -4.250  -0.5484   0.01660   0.00803   0.0097   0.9662   0.4021
  -4.000  -0.5127   0.01634   0.00782   0.0080   0.9570   0.4257
  -3.750  -0.4793   0.01609   0.00763   0.0068   0.9466   0.4484
  -3.500  -0.4431   0.01585   0.00746   0.0052   0.9379   0.4724
  -3.250  -0.4074   0.01562   0.00728   0.0037   0.9285   0.4951
  -3.000  -0.3733   0.01541   0.00713   0.0026   0.9182   0.5169
  -2.500  -0.3038   0.01502   0.00685   0.0003   0.8974   0.5608
  -2.250  -0.2709   0.01486   0.00674  -0.0004   0.8854   0.5823
  -2.000  -0.2372   0.01472   0.00662  -0.0012   0.8736   0.6041
  -1.750  -0.2032   0.01458   0.00653  -0.0019   0.8614   0.6246
  -1.500  -0.1728   0.01448   0.00646  -0.0020   0.8468   0.6441
  -1.250  -0.1432   0.01439   0.00640  -0.0018   0.8319   0.6631
  -1.000  -0.1142   0.01433   0.00635  -0.0016   0.8168   0.6816
  -0.750  -0.0856   0.01428   0.00631  -0.0012   0.8013   0.6999
  -0.500  -0.0570   0.01424   0.00629  -0.0009   0.7857   0.7175
  -0.250  -0.0285   0.01422   0.00628  -0.0004   0.7693   0.7350
   0.000   0.0000   0.01421   0.00628   0.0000   0.7524   0.7523
   0.250   0.0285   0.01422   0.00628   0.0004   0.7350   0.7693
   0.500   0.0570   0.01424   0.00629   0.0009   0.7176   0.7857
   0.750   0.0857   0.01428   0.00631   0.0012   0.7000   0.8014
   1.000   0.1142   0.01433   0.00635   0.0016   0.6816   0.8167
   1.250   0.1432   0.01439   0.00640   0.0018   0.6631   0.8319
   1.500   0.1728   0.01447   0.00646   0.0020   0.6441   0.8468
   1.750   0.2031   0.01458   0.00653   0.0019   0.6246   0.8614
   2.000   0.2372   0.01472   0.00662   0.0011   0.6042   0.8736
   2.250   0.2709   0.01487   0.00674   0.0003   0.5823   0.8855
   2.500   0.3038   0.01502   0.00685  -0.0003   0.5607   0.8974
   3.000   0.3733   0.01541   0.00713  -0.0026   0.5169   0.9182
   3.250   0.4074   0.01562   0.00728  -0.0037   0.4951   0.9285
   3.500   0.4431   0.01585   0.00745  -0.0052   0.4724   0.9378
   3.750   0.4793   0.01609   0.00763  -0.0068   0.4485   0.9466
   4.000   0.5126   0.01634   0.00782  -0.0080   0.4258   0.9570
   4.250   0.5484   0.01660   0.00803  -0.0097   0.4022   0.9662
   4.500   0.5833   0.01687   0.00823  -0.0113   0.3800   0.9754
   4.750   0.6181   0.01714   0.00847  -0.0130   0.3576   0.9847
   5.000   0.6538   0.01744   0.00872  -0.0149   0.3358   0.9932
   5.250   0.6893   0.01772   0.00896  -0.0169   0.3143   1.0000
   5.500   0.7041   0.01800   0.00920  -0.0148   0.2986   1.0000
   5.750   0.7188   0.01831   0.00949  -0.0126   0.2832   1.0000
   6.000   0.7335   0.01865   0.00979  -0.0105   0.2679   1.0000
   6.250   0.7483   0.01903   0.01012  -0.0083   0.2531   1.0000
   6.500   0.7632   0.01944   0.01049  -0.0061   0.2388   1.0000
   6.750   0.7783   0.01987   0.01090  -0.0040   0.2251   1.0000
   7.000   0.7938   0.02032   0.01135  -0.0020   0.2118   1.0000
   7.250   0.8093   0.02079   0.01182   0.0001   0.1994   1.0000
   7.500   0.8245   0.02131   0.01233   0.0021   0.1881   1.0000
   7.750   0.8389   0.02188   0.01286   0.0043   0.1778   1.0000
   8.000   0.8538   0.02245   0.01346   0.0063   0.1673   1.0000
   8.250   0.8686   0.02305   0.01408   0.0084   0.1578   1.0000
   8.500   0.8815   0.02372   0.01470   0.0107   0.1494   1.0000
   8.750   0.8960   0.02435   0.01541   0.0128   0.1402   1.0000
   9.000   0.9084   0.02507   0.01612   0.0150   0.1328   1.0000
   9.250   0.9211   0.02577   0.01689   0.0173   0.1249   1.0000
   9.500   0.9324   0.02656   0.01768   0.0196   0.1182   1.0000
   9.750   0.9437   0.02733   0.01851   0.0219   0.1115   1.0000
  10.000   0.9528   0.02821   0.01938   0.0244   0.1058   1.0000
  10.250   0.9623   0.02905   0.02032   0.0268   0.0999   1.0000
  10.500   0.9672   0.02997   0.02122   0.0298   0.0954   1.0000
  10.750   0.9745   0.03095   0.02231   0.0323   0.0906   1.0000
  11.000   0.9807   0.03196   0.02341   0.0347   0.0860   1.0000
  11.250   0.9846   0.03314   0.02457   0.0370   0.0825   1.0000
  11.500   0.9908   0.03442   0.02598   0.0390   0.0786   1.0000
  11.750   0.9958   0.03577   0.02744   0.0407   0.0749   1.0000
  12.000   0.9989   0.03725   0.02896   0.0423   0.0720   1.0000
  12.250   1.0015   0.03896   0.03070   0.0436   0.0692   1.0000
  12.500   1.0048   0.04078   0.03273   0.0447   0.0663   1.0000
  12.750   1.0064   0.04273   0.03479   0.0456   0.0636   1.0000
  13.000   1.0070   0.04483   0.03695   0.0462   0.0615   1.0000
  13.250   1.0074   0.04706   0.03918   0.0466   0.0597   1.0000
  13.500   1.0064   0.04973   0.04204   0.0468   0.0578   1.0000
  13.750   1.0034   0.05265   0.04516   0.0466   0.0559   1.0000
  14.000   0.9995   0.05576   0.04841   0.0461   0.0542   1.0000
  14.250   0.9953   0.05899   0.05174   0.0453   0.0527   1.0000
  14.500   0.9915   0.06227   0.05508   0.0443   0.0514   1.0000
  14.750   0.9889   0.06548   0.05831   0.0434   0.0502   1.0000
  15.000   0.9789   0.06996   0.06297   0.0417   0.0493   1.0000
  15.250   0.9644   0.07537   0.06860   0.0392   0.0485   1.0000
  15.500   0.9468   0.08156   0.07501   0.0361   0.0479   1.0000
  15.750   0.9241   0.08897   0.08264   0.0320   0.0474   1.0000
  16.000   0.8920   0.09867   0.09258   0.0264   0.0472   1.0000
  16.250   0.8235   0.11705   0.11124   0.0154   0.0478   1.0000
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