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S8035 for RC aerobatic 14% thick (s8035-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S8035 for RC aerobatic 14% thick (s8035-il)
Reynolds number: 1,000,000
Max Cl/Cd: 78.68 at α=9.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8035-il-1000000-n5.txt
Download as CSV file: xf-s8035-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1843   0.10291   0.09937  -0.0203   1.0000   0.0104
 -19.500  -1.2068   0.09577   0.09211  -0.0238   1.0000   0.0104
 -19.250  -1.2296   0.08871   0.08493  -0.0271   1.0000   0.0105
 -19.000  -1.2503   0.08212   0.07821  -0.0302   1.0000   0.0105
 -18.750  -1.2691   0.07596   0.07194  -0.0330   1.0000   0.0106
 -18.500  -1.2852   0.07028   0.06615  -0.0355   1.0000   0.0107
 -18.250  -1.3008   0.06481   0.06056  -0.0379   1.0000   0.0108
 -18.000  -1.3124   0.06004   0.05569  -0.0399   1.0000   0.0110
 -17.750  -1.3221   0.05563   0.05118  -0.0416   1.0000   0.0112
 -17.500  -1.3296   0.05165   0.04710  -0.0430   1.0000   0.0114
 -17.250  -1.3353   0.04801   0.04337  -0.0442   1.0000   0.0115
 -17.000  -1.3394   0.04468   0.03993  -0.0451   1.0000   0.0117
 -16.750  -1.3415   0.04170   0.03686  -0.0458   1.0000   0.0118
 -16.500  -1.3412   0.03906   0.03414  -0.0462   1.0000   0.0120
 -16.250  -1.3403   0.03660   0.03159  -0.0464   1.0000   0.0123
 -16.000  -1.3402   0.03418   0.02908  -0.0464   1.0000   0.0125
 -15.750  -1.3373   0.03212   0.02696  -0.0461   1.0000   0.0128
 -15.500  -1.3342   0.03020   0.02498  -0.0457   1.0000   0.0133
 -15.250  -1.3292   0.02855   0.02327  -0.0450   1.0000   0.0137
 -15.000  -1.3231   0.02708   0.02174  -0.0441   1.0000   0.0141
 -14.750  -1.3161   0.02577   0.02036  -0.0430   1.0000   0.0144
 -14.500  -1.3083   0.02459   0.01913  -0.0418   1.0000   0.0148
 -14.250  -1.2991   0.02360   0.01807  -0.0404   1.0000   0.0153
 -14.000  -1.2919   0.02253   0.01695  -0.0387   1.0000   0.0159
 -13.750  -1.2838   0.02160   0.01598  -0.0368   1.0000   0.0165
 -13.500  -1.2749   0.02078   0.01512  -0.0348   1.0000   0.0171
 -13.250  -1.2653   0.02006   0.01437  -0.0327   1.0000   0.0178
 -13.000  -1.2549   0.01945   0.01370  -0.0304   1.0000   0.0183
 -12.750  -1.2440   0.01890   0.01311  -0.0281   1.0000   0.0187
 -12.500  -1.2343   0.01836   0.01253  -0.0254   1.0000   0.0195
 -12.250  -1.2265   0.01782   0.01197  -0.0223   1.0000   0.0207
 -12.000  -1.2184   0.01738   0.01151  -0.0189   1.0000   0.0215
 -11.750  -1.2090   0.01697   0.01107  -0.0158   1.0000   0.0226
 -11.500  -1.1957   0.01652   0.01060  -0.0134   1.0000   0.0239
 -11.250  -1.1822   0.01606   0.01014  -0.0110   1.0000   0.0256
 -11.000  -1.1674   0.01565   0.00971  -0.0088   1.0000   0.0274
 -10.750  -1.1517   0.01527   0.00931  -0.0067   1.0000   0.0291
 -10.500  -1.1362   0.01485   0.00890  -0.0045   1.0000   0.0316
 -10.250  -1.1193   0.01450   0.00854  -0.0026   1.0000   0.0337
 -10.000  -1.1025   0.01414   0.00817  -0.0006   1.0000   0.0361
  -9.750  -1.0833   0.01377   0.00782   0.0008   0.9998   0.0390
  -9.500  -1.0518   0.01341   0.00745  -0.0003   0.9982   0.0422
  -9.250  -1.0204   0.01300   0.00706  -0.0014   0.9962   0.0463
  -9.000  -0.9871   0.01267   0.00673  -0.0028   0.9942   0.0495
  -8.750  -0.9565   0.01230   0.00638  -0.0037   0.9916   0.0536
  -8.500  -0.9272   0.01196   0.00605  -0.0042   0.9879   0.0577
  -8.250  -0.8964   0.01164   0.00574  -0.0050   0.9844   0.0623
  -8.000  -0.8687   0.01131   0.00544  -0.0052   0.9790   0.0681
  -7.750  -0.8424   0.01098   0.00515  -0.0050   0.9698   0.0748
  -7.500  -0.8133   0.01068   0.00486  -0.0054   0.9601   0.0810
  -7.250  -0.7761   0.01032   0.00455  -0.0076   0.9528   0.0907
  -7.000  -0.7349   0.00995   0.00423  -0.0107   0.9431   0.1019
  -6.500  -0.6637   0.00942   0.00367  -0.0141   0.9025   0.1214
  -6.250  -0.6384   0.00923   0.00346  -0.0136   0.8817   0.1307
  -6.000  -0.6136   0.00909   0.00328  -0.0129   0.8643   0.1388
  -5.750  -0.5891   0.00895   0.00312  -0.0122   0.8481   0.1488
  -5.500  -0.5647   0.00878   0.00295  -0.0115   0.8325   0.1595
  -5.250  -0.5397   0.00866   0.00280  -0.0108   0.8172   0.1682
  -5.000  -0.5148   0.00854   0.00265  -0.0102   0.8008   0.1780
  -4.750  -0.4903   0.00840   0.00251  -0.0094   0.7831   0.1902
  -4.500  -0.4655   0.00828   0.00237  -0.0087   0.7660   0.2029
  -4.250  -0.4406   0.00814   0.00224  -0.0081   0.7506   0.2180
  -4.000  -0.4154   0.00800   0.00212  -0.0075   0.7364   0.2341
  -3.750  -0.3899   0.00788   0.00201  -0.0070   0.7224   0.2489
  -3.500  -0.3642   0.00778   0.00191  -0.0064   0.7082   0.2620
  -3.250  -0.3382   0.00770   0.00182  -0.0060   0.6934   0.2732
  -3.000  -0.3124   0.00763   0.00173  -0.0055   0.6774   0.2862
  -2.750  -0.2868   0.00756   0.00165  -0.0049   0.6585   0.3019
  -2.500  -0.2611   0.00750   0.00158  -0.0044   0.6401   0.3165
  -2.250  -0.2351   0.00744   0.00152  -0.0040   0.6243   0.3295
  -2.000  -0.2090   0.00737   0.00146  -0.0035   0.6092   0.3456
  -1.750  -0.1830   0.00731   0.00141  -0.0031   0.5938   0.3619
  -1.500  -0.1570   0.00725   0.00136  -0.0026   0.5780   0.3804
  -1.250  -0.1310   0.00719   0.00132  -0.0021   0.5637   0.3992
  -1.000  -0.1048   0.00715   0.00129  -0.0017   0.5479   0.4157
  -0.750  -0.0784   0.00715   0.00127  -0.0013   0.5306   0.4296
  -0.500  -0.0522   0.00715   0.00125  -0.0009   0.5117   0.4429
  -0.250  -0.0260   0.00716   0.00124  -0.0005   0.4935   0.4576
   0.000   0.0000   0.00716   0.00124   0.0000   0.4751   0.4749
   0.250   0.0260   0.00716   0.00124   0.0005   0.4578   0.4937
   0.500   0.0521   0.00715   0.00125   0.0009   0.4429   0.5124
   0.750   0.0784   0.00715   0.00127   0.0013   0.4296   0.5306
   1.000   0.1048   0.00715   0.00129   0.0017   0.4155   0.5480
   1.250   0.1310   0.00719   0.00132   0.0021   0.3994   0.5638
   1.500   0.1570   0.00725   0.00136   0.0026   0.3807   0.5778
   1.750   0.1830   0.00731   0.00141   0.0031   0.3614   0.5932
   2.000   0.2090   0.00737   0.00146   0.0035   0.3449   0.6091
   2.250   0.2351   0.00743   0.00152   0.0040   0.3299   0.6245
   2.500   0.2611   0.00750   0.00158   0.0044   0.3165   0.6402
   2.750   0.2869   0.00755   0.00165   0.0049   0.3026   0.6585
   3.000   0.3124   0.00763   0.00173   0.0055   0.2863   0.6770
   3.250   0.3382   0.00770   0.00182   0.0060   0.2733   0.6936
   3.500   0.3642   0.00778   0.00191   0.0064   0.2619   0.7083
   3.750   0.3898   0.00788   0.00201   0.0070   0.2481   0.7225
   4.000   0.4154   0.00800   0.00212   0.0075   0.2345   0.7368
   4.250   0.4405   0.00814   0.00224   0.0081   0.2176   0.7508
   4.500   0.4655   0.00828   0.00237   0.0087   0.2027   0.7661
   4.750   0.4903   0.00841   0.00251   0.0094   0.1899   0.7830
   5.000   0.5148   0.00854   0.00265   0.0101   0.1779   0.8006
   5.250   0.5397   0.00866   0.00280   0.0108   0.1683   0.8173
   5.500   0.5647   0.00879   0.00295   0.0115   0.1594   0.8324
   5.750   0.5891   0.00895   0.00312   0.0122   0.1485   0.8477
   6.000   0.6136   0.00910   0.00328   0.0129   0.1387   0.8643
   6.250   0.6384   0.00923   0.00346   0.0136   0.1307   0.8819
   6.500   0.6637   0.00942   0.00367   0.0141   0.1215   0.9025
   7.000   0.7348   0.00995   0.00423   0.0107   0.1018   0.9431
   7.250   0.7762   0.01032   0.00455   0.0076   0.0903   0.9528
   7.500   0.8133   0.01068   0.00486   0.0054   0.0810   0.9599
   8.000   0.8688   0.01130   0.00544   0.0052   0.0683   0.9790
   8.250   0.8965   0.01164   0.00574   0.0050   0.0624   0.9844
   8.500   0.9273   0.01196   0.00605   0.0042   0.0578   0.9880
   8.750   0.9566   0.01230   0.00638   0.0036   0.0537   0.9916
   9.000   0.9871   0.01267   0.00673   0.0028   0.0495   0.9941
   9.250   1.0204   0.01299   0.00705   0.0014   0.0464   0.9962
   9.500   1.0519   0.01341   0.00745   0.0002   0.0422   0.9982
   9.750   1.0834   0.01377   0.00782  -0.0009   0.0390   0.9998
  10.000   1.1025   0.01414   0.00817   0.0006   0.0361   1.0000
  10.250   1.1194   0.01450   0.00854   0.0026   0.0338   1.0000
  10.500   1.1363   0.01485   0.00890   0.0045   0.0317   1.0000
  10.750   1.1519   0.01526   0.00930   0.0066   0.0293   1.0000
  11.000   1.1674   0.01565   0.00971   0.0087   0.0274   1.0000
  11.250   1.1823   0.01606   0.01013   0.0110   0.0256   1.0000
  11.500   1.1956   0.01653   0.01060   0.0134   0.0238   1.0000
  11.750   1.2092   0.01696   0.01106   0.0157   0.0226   1.0000
  12.000   1.2188   0.01737   0.01150   0.0189   0.0216   1.0000
  12.250   1.2267   0.01782   0.01197   0.0222   0.0207   1.0000
  12.500   1.2351   0.01833   0.01251   0.0253   0.0197   1.0000
  12.750   1.2443   0.01890   0.01311   0.0280   0.0189   1.0000
  13.000   1.2552   0.01944   0.01370   0.0304   0.0183   1.0000
  13.250   1.2654   0.02007   0.01437   0.0326   0.0175   1.0000
  13.500   1.2753   0.02078   0.01512   0.0347   0.0171   1.0000
  13.750   1.2839   0.02161   0.01598   0.0368   0.0163   1.0000
  14.000   1.2921   0.02254   0.01695   0.0386   0.0157   1.0000
  14.250   1.2999   0.02357   0.01804   0.0403   0.0152   1.0000
  14.500   1.3088   0.02459   0.01913   0.0417   0.0149   1.0000
  14.750   1.3170   0.02574   0.02034   0.0429   0.0146   1.0000
  15.000   1.3241   0.02704   0.02169   0.0440   0.0138   1.0000
  15.250   1.3303   0.02851   0.02323   0.0448   0.0138   1.0000
  15.500   1.3354   0.03016   0.02494   0.0455   0.0133   1.0000
  15.750   1.3389   0.03204   0.02687   0.0460   0.0129   1.0000
  16.000   1.3410   0.03417   0.02907   0.0462   0.0125   1.0000
  16.250   1.3413   0.03659   0.03157   0.0462   0.0122   1.0000
  16.500   1.3419   0.03908   0.03416   0.0460   0.0120   1.0000
  16.750   1.3430   0.04165   0.03681   0.0456   0.0119   1.0000
  17.000   1.3416   0.04454   0.03979   0.0449   0.0117   1.0000
  17.250   1.3375   0.04788   0.04323   0.0440   0.0115   1.0000
  17.500   1.3325   0.05144   0.04689   0.0429   0.0113   1.0000
  17.750   1.3245   0.05548   0.05102   0.0414   0.0110   1.0000
  18.000   1.3155   0.05981   0.05546   0.0397   0.0109   1.0000
  18.250   1.3031   0.06469   0.06044   0.0377   0.0107   1.0000
  18.500   1.2884   0.07004   0.06590   0.0354   0.0107   1.0000
  18.750   1.2718   0.07580   0.07177   0.0328   0.0106   1.0000
  19.000   1.2523   0.08206   0.07816   0.0299   0.0104   1.0000
  19.250   1.2327   0.08850   0.08472   0.0269   0.0104   1.0000
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