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S8035 for RC aerobatic 14% thick (s8035-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S8035 for RC aerobatic 14% thick (s8035-il)
Reynolds number: 500,000
Max Cl/Cd: 66.88 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8035-il-500000-n5.txt
Download as CSV file: xf-s8035-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -1.0837   0.10471   0.10062  -0.0193   1.0000   0.0157
 -18.500  -1.0997   0.09836   0.09418  -0.0224   1.0000   0.0159
 -18.250  -1.1177   0.09181   0.08752  -0.0256   1.0000   0.0160
 -18.000  -1.1331   0.08583   0.08143  -0.0284   1.0000   0.0161
 -17.750  -1.1487   0.07990   0.07540  -0.0312   1.0000   0.0163
 -17.500  -1.1634   0.07427   0.06965  -0.0338   1.0000   0.0165
 -17.250  -1.1770   0.06891   0.06418  -0.0361   1.0000   0.0166
 -17.000  -1.1873   0.06415   0.05932  -0.0382   1.0000   0.0170
 -16.750  -1.1985   0.05940   0.05445  -0.0401   1.0000   0.0171
 -16.500  -1.2050   0.05541   0.05036  -0.0417   1.0000   0.0175
 -16.250  -1.2114   0.05157   0.04641  -0.0430   1.0000   0.0178
 -16.000  -1.2173   0.04790   0.04262  -0.0441   1.0000   0.0181
 -15.750  -1.2197   0.04479   0.03940  -0.0449   1.0000   0.0184
 -15.500  -1.2211   0.04190   0.03640  -0.0455   1.0000   0.0187
 -15.250  -1.2225   0.03911   0.03353  -0.0459   1.0000   0.0192
 -15.000  -1.2243   0.03644   0.03077  -0.0460   1.0000   0.0196
 -14.750  -1.2236   0.03414   0.02839  -0.0458   1.0000   0.0202
 -14.500  -1.2210   0.03215   0.02633  -0.0453   1.0000   0.0210
 -14.250  -1.2176   0.03035   0.02444  -0.0446   1.0000   0.0214
 -14.000  -1.2118   0.02885   0.02286  -0.0437   1.0000   0.0222
 -13.750  -1.2055   0.02748   0.02141  -0.0426   1.0000   0.0229
 -13.500  -1.2001   0.02615   0.02001  -0.0412   1.0000   0.0237
 -13.250  -1.1947   0.02490   0.01872  -0.0395   1.0000   0.0247
 -13.000  -1.1876   0.02385   0.01763  -0.0377   1.0000   0.0259
 -12.750  -1.1793   0.02295   0.01666  -0.0358   1.0000   0.0270
 -12.500  -1.1701   0.02216   0.01580  -0.0337   1.0000   0.0281
 -12.250  -1.1622   0.02137   0.01497  -0.0313   1.0000   0.0295
 -12.000  -1.1539   0.02066   0.01424  -0.0287   1.0000   0.0311
 -11.750  -1.1447   0.02006   0.01361  -0.0260   1.0000   0.0328
 -11.500  -1.1352   0.01956   0.01305  -0.0232   1.0000   0.0343
 -11.250  -1.1281   0.01901   0.01249  -0.0198   1.0000   0.0363
 -11.000  -1.1187   0.01851   0.01196  -0.0168   1.0000   0.0385
 -10.750  -1.1050   0.01805   0.01147  -0.0145   1.0000   0.0409
 -10.500  -1.0917   0.01756   0.01096  -0.0121   1.0000   0.0435
 -10.250  -1.0775   0.01709   0.01049  -0.0099   1.0000   0.0465
 -10.000  -1.0617   0.01670   0.01006  -0.0078   1.0000   0.0492
  -9.750  -1.0462   0.01627   0.00962  -0.0057   1.0000   0.0520
  -9.500  -1.0305   0.01585   0.00920  -0.0036   1.0000   0.0554
  -9.250  -1.0136   0.01550   0.00882  -0.0017   1.0000   0.0587
  -9.000  -0.9973   0.01511   0.00843   0.0003   1.0000   0.0625
  -8.750  -0.9807   0.01474   0.00808   0.0023   1.0000   0.0672
  -8.500  -0.9637   0.01441   0.00774   0.0043   1.0000   0.0718
  -8.250  -0.9310   0.01399   0.00734   0.0029   0.9974   0.0790
  -8.000  -0.8973   0.01358   0.00697   0.0013   0.9942   0.0867
  -7.500  -0.8343   0.01283   0.00626  -0.0008   0.9857   0.1045
  -7.250  -0.8025   0.01245   0.00593  -0.0019   0.9812   0.1146
  -7.000  -0.7750   0.01211   0.00562  -0.0020   0.9725   0.1243
  -6.750  -0.7468   0.01178   0.00531  -0.0022   0.9633   0.1346
  -6.500  -0.7142   0.01144   0.00501  -0.0034   0.9562   0.1454
  -6.250  -0.6809   0.01111   0.00472  -0.0046   0.9478   0.1568
  -6.000  -0.6426   0.01078   0.00443  -0.0070   0.9405   0.1703
  -5.750  -0.6052   0.01048   0.00415  -0.0091   0.9292   0.1827
  -5.500  -0.5687   0.01018   0.00388  -0.0110   0.9166   0.1973
  -5.250  -0.5355   0.00991   0.00363  -0.0122   0.9016   0.2128
  -5.000  -0.5062   0.00971   0.00343  -0.0125   0.8849   0.2278
  -4.750  -0.4797   0.00951   0.00324  -0.0122   0.8685   0.2450
  -4.500  -0.4542   0.00934   0.00307  -0.0117   0.8525   0.2611
  -4.250  -0.4290   0.00920   0.00292  -0.0110   0.8364   0.2759
  -4.000  -0.4040   0.00907   0.00279  -0.0104   0.8196   0.2902
  -3.750  -0.3789   0.00896   0.00265  -0.0097   0.8029   0.3046
  -3.500  -0.3540   0.00884   0.00253  -0.0090   0.7868   0.3209
  -3.250  -0.3288   0.00873   0.00242  -0.0083   0.7719   0.3357
  -3.000  -0.3035   0.00864   0.00232  -0.0077   0.7572   0.3503
  -2.750  -0.2783   0.00854   0.00222  -0.0070   0.7425   0.3672
  -2.500  -0.2532   0.00844   0.00214  -0.0064   0.7275   0.3844
  -2.250  -0.2282   0.00835   0.00205  -0.0057   0.7110   0.4034
  -2.000  -0.2032   0.00828   0.00198  -0.0050   0.6931   0.4225
  -1.750  -0.1781   0.00822   0.00192  -0.0043   0.6753   0.4401
  -1.500  -0.1526   0.00817   0.00186  -0.0037   0.6589   0.4561
  -1.250  -0.1270   0.00813   0.00182  -0.0031   0.6430   0.4710
  -1.000  -0.1014   0.00810   0.00178  -0.0025   0.6274   0.4875
  -0.750  -0.0760   0.00806   0.00175  -0.0019   0.6111   0.5055
  -0.250  -0.0252   0.00801   0.00172  -0.0007   0.5786   0.5423
   0.000   0.0000   0.00801   0.00172   0.0000   0.5605   0.5606
   0.250   0.0252   0.00801   0.00172   0.0007   0.5423   0.5786
   0.500   0.0504   0.00804   0.00173   0.0013   0.5238   0.5953
   0.750   0.0760   0.00806   0.00175   0.0019   0.5057   0.6111
   1.000   0.1014   0.00810   0.00178   0.0025   0.4874   0.6273
   1.250   0.1270   0.00813   0.00182   0.0031   0.4710   0.6429
   1.500   0.1526   0.00817   0.00186   0.0037   0.4561   0.6590
   1.750   0.1780   0.00822   0.00192   0.0043   0.4401   0.6754
   2.000   0.2032   0.00828   0.00198   0.0050   0.4225   0.6932
   2.250   0.2282   0.00835   0.00205   0.0057   0.4036   0.7111
   2.500   0.2532   0.00844   0.00214   0.0064   0.3845   0.7276
   2.750   0.2783   0.00854   0.00222   0.0071   0.3667   0.7427
   3.000   0.3035   0.00864   0.00232   0.0077   0.3506   0.7572
   3.250   0.3288   0.00873   0.00242   0.0083   0.3358   0.7717
   3.500   0.3540   0.00884   0.00253   0.0090   0.3208   0.7868
   3.750   0.3790   0.00895   0.00265   0.0097   0.3050   0.8030
   4.000   0.4040   0.00907   0.00279   0.0103   0.2903   0.8194
   4.250   0.4290   0.00919   0.00292   0.0110   0.2761   0.8364
   4.500   0.4542   0.00934   0.00307   0.0117   0.2613   0.8524
   4.750   0.4796   0.00951   0.00324   0.0122   0.2447   0.8686
   5.000   0.5061   0.00971   0.00343   0.0125   0.2275   0.8850
   5.250   0.5354   0.00992   0.00363   0.0122   0.2124   0.9015
   5.500   0.5686   0.01019   0.00388   0.0110   0.1967   0.9166
   5.750   0.6053   0.01048   0.00415   0.0091   0.1827   0.9292
   6.000   0.6426   0.01078   0.00443   0.0070   0.1701   0.9405
   6.250   0.6808   0.01111   0.00472   0.0047   0.1569   0.9477
   6.500   0.7142   0.01144   0.00501   0.0034   0.1454   0.9562
   6.750   0.7469   0.01178   0.00531   0.0022   0.1345   0.9632
   7.000   0.7751   0.01211   0.00562   0.0020   0.1243   0.9725
   7.250   0.8026   0.01245   0.00593   0.0019   0.1148   0.9812
   7.500   0.8344   0.01282   0.00626   0.0008   0.1046   0.9857
   8.000   0.8973   0.01359   0.00697  -0.0013   0.0866   0.9942
   8.250   0.9311   0.01399   0.00734  -0.0029   0.0787   0.9974
   8.500   0.9637   0.01441   0.00774  -0.0043   0.0718   1.0000
   8.750   0.9807   0.01474   0.00807  -0.0023   0.0674   1.0000
   9.000   0.9974   0.01510   0.00843  -0.0003   0.0628   1.0000
   9.250   1.0136   0.01550   0.00882   0.0017   0.0586   1.0000
   9.500   1.0305   0.01585   0.00920   0.0036   0.0555   1.0000
   9.750   1.0463   0.01627   0.00962   0.0057   0.0521   1.0000
  10.000   1.0617   0.01670   0.01006   0.0078   0.0491   1.0000
  10.250   1.0775   0.01709   0.01049   0.0098   0.0466   1.0000
  10.500   1.0918   0.01756   0.01096   0.0121   0.0436   1.0000
  10.750   1.1051   0.01805   0.01147   0.0145   0.0410   1.0000
  11.000   1.1188   0.01851   0.01196   0.0168   0.0386   1.0000
  11.250   1.1284   0.01900   0.01248   0.0198   0.0363   1.0000
  11.500   1.1354   0.01955   0.01304   0.0231   0.0343   1.0000
  11.750   1.1451   0.02006   0.01360   0.0259   0.0329   1.0000
  12.000   1.1543   0.02065   0.01423   0.0286   0.0312   1.0000
  12.250   1.1626   0.02136   0.01497   0.0312   0.0295   1.0000
  12.500   1.1706   0.02215   0.01579   0.0336   0.0281   1.0000
  12.750   1.1799   0.02293   0.01664   0.0357   0.0269   1.0000
  13.000   1.1881   0.02384   0.01760   0.0376   0.0256   1.0000
  13.250   1.1951   0.02490   0.01872   0.0394   0.0246   1.0000
  13.500   1.2006   0.02614   0.02000   0.0411   0.0237   1.0000
  13.750   1.2065   0.02745   0.02138   0.0425   0.0229   1.0000
  14.000   1.2130   0.02880   0.02281   0.0436   0.0221   1.0000
  14.250   1.2180   0.03037   0.02446   0.0445   0.0215   1.0000
  14.500   1.2223   0.03209   0.02626   0.0452   0.0208   1.0000
  14.750   1.2249   0.03408   0.02833   0.0457   0.0203   1.0000
  15.000   1.2253   0.03641   0.03074   0.0459   0.0197   1.0000
  15.250   1.2237   0.03907   0.03348   0.0457   0.0191   1.0000
  15.500   1.2223   0.04186   0.03636   0.0453   0.0188   1.0000
  15.750   1.2217   0.04467   0.03928   0.0448   0.0184   1.0000
  16.000   1.2181   0.04793   0.04265   0.0439   0.0181   1.0000
  16.250   1.2151   0.05124   0.04607   0.0429   0.0176   1.0000
  16.500   1.2070   0.05530   0.05024   0.0415   0.0174   1.0000
  16.750   1.2006   0.05928   0.05433   0.0400   0.0171   1.0000
  17.000   1.1906   0.06386   0.05902   0.0381   0.0168   1.0000
  17.250   1.1780   0.06895   0.06422   0.0359   0.0167   1.0000
  17.500   1.1656   0.07416   0.06954   0.0336   0.0164   1.0000
  17.750   1.1509   0.07979   0.07529   0.0310   0.0164   1.0000
  18.000   1.1357   0.08566   0.08126   0.0283   0.0162   1.0000
  18.250   1.1193   0.09182   0.08753   0.0253   0.0160   1.0000
  18.500   1.1025   0.09817   0.09398   0.0223   0.0159   1.0000
  18.750   1.0862   0.10454   0.10046   0.0192   0.0157   1.0000
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