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S8035 for RC aerobatic 14% thick (s8035-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: S8035 for RC aerobatic 14% thick (s8035-il)
Reynolds number: 100,000
Max Cl/Cd: 38.68 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8035-il-100000.txt
Download as CSV file: xf-s8035-il-100000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9187   0.07859   0.07269  -0.0444   1.0000   0.0818
 -14.000  -0.9527   0.07159   0.06551  -0.0475   1.0000   0.0814
 -13.750  -0.9847   0.06582   0.05952  -0.0492   1.0000   0.0813
 -13.500  -1.0143   0.06111   0.05458  -0.0493   1.0000   0.0813
 -13.250  -1.0418   0.05729   0.05048  -0.0480   1.0000   0.0816
 -13.000  -1.0656   0.05423   0.04714  -0.0454   1.0000   0.0819
 -12.750  -1.0492   0.05127   0.04430  -0.0453   1.0000   0.0849
 -12.500  -1.0483   0.04956   0.04254  -0.0433   1.0000   0.0876
 -12.250  -1.0572   0.04743   0.04022  -0.0402   1.0000   0.0897
 -12.000  -1.0696   0.04535   0.03784  -0.0361   1.0000   0.0919
 -11.750  -1.0804   0.04328   0.03536  -0.0320   1.0000   0.0940
 -11.500  -1.0635   0.04097   0.03314  -0.0313   1.0000   0.0982
 -11.250  -1.0562   0.03955   0.03162  -0.0290   1.0000   0.1026
 -11.000  -1.0567   0.03792   0.02961  -0.0255   1.0000   0.1069
 -10.750  -1.0384   0.03619   0.02800  -0.0246   1.0000   0.1125
 -10.500  -1.0301   0.03495   0.02657  -0.0221   1.0000   0.1185
 -10.250  -1.0168   0.03339   0.02494  -0.0203   1.0000   0.1247
 -10.000  -1.0038   0.03236   0.02383  -0.0182   1.0000   0.1318
  -9.750  -0.9898   0.03105   0.02248  -0.0163   1.0000   0.1392
  -9.500  -0.9768   0.03010   0.02141  -0.0141   1.0000   0.1473
  -9.250  -0.9601   0.02899   0.02037  -0.0125   1.0000   0.1559
  -9.000  -0.9482   0.02799   0.01914  -0.0100   1.0000   0.1652
  -8.750  -0.9303   0.02708   0.01836  -0.0085   1.0000   0.1753
  -8.500  -0.9139   0.02612   0.01743  -0.0067   1.0000   0.1858
  -8.250  -0.8986   0.02522   0.01647  -0.0047   1.0000   0.1972
  -8.000  -0.8840   0.02449   0.01565  -0.0025   1.0000   0.2097
  -7.750  -0.8668   0.02373   0.01499  -0.0007   1.0000   0.2224
  -7.500  -0.8501   0.02299   0.01432   0.0012   1.0000   0.2357
  -7.250  -0.8340   0.02232   0.01369   0.0032   1.0000   0.2498
  -7.000  -0.8181   0.02168   0.01310   0.0052   1.0000   0.2648
  -6.750  -0.8024   0.02110   0.01256   0.0073   1.0000   0.2807
  -6.500  -0.7871   0.02056   0.01206   0.0095   1.0000   0.2973
  -6.250  -0.7721   0.02008   0.01161   0.0117   1.0000   0.3150
  -6.000  -0.7577   0.01963   0.01118   0.0141   1.0000   0.3335
  -5.750  -0.7422   0.01919   0.01086   0.0162   1.0000   0.3515
  -5.500  -0.7271   0.01882   0.01058   0.0184   1.0000   0.3702
  -5.250  -0.7120   0.01848   0.01031   0.0206   1.0000   0.3896
  -5.000  -0.6973   0.01818   0.01005   0.0228   1.0000   0.4100
  -4.750  -0.6821   0.01791   0.00985   0.0249   1.0000   0.4302
  -4.500  -0.6663   0.01769   0.00974   0.0270   1.0000   0.4502
  -4.250  -0.6509   0.01751   0.00962   0.0290   1.0000   0.4713
  -4.000  -0.6357   0.01736   0.00952   0.0310   1.0000   0.4931
  -3.750  -0.6199   0.01724   0.00952   0.0329   1.0000   0.5137
  -3.500  -0.6047   0.01716   0.00949   0.0349   1.0000   0.5359
  -3.250  -0.5895   0.01710   0.00951   0.0368   1.0000   0.5582
  -3.000  -0.5597   0.01722   0.00974   0.0360   0.9951   0.5847
  -2.750  -0.5145   0.01744   0.01007   0.0324   0.9844   0.6138
  -2.500  -0.4710   0.01759   0.01031   0.0293   0.9730   0.6417
  -2.250  -0.4288   0.01768   0.01045   0.0265   0.9613   0.6694
  -2.000  -0.3860   0.01776   0.01064   0.0239   0.9498   0.6951
  -1.750  -0.3397   0.01781   0.01077   0.0208   0.9393   0.7209
  -1.500  -0.2965   0.01782   0.01084   0.0184   0.9275   0.7461
  -1.250  -0.2553   0.01785   0.01094   0.0166   0.9153   0.7686
  -1.000  -0.2071   0.01787   0.01101   0.0136   0.9053   0.7905
  -0.750  -0.1551   0.01782   0.01099   0.0099   0.8961   0.8119
  -0.500  -0.1104   0.01782   0.01102   0.0077   0.8839   0.8305
  -0.250  -0.0569   0.01780   0.01102   0.0041   0.8731   0.8471
   0.000   0.0000   0.01774   0.01095   0.0000   0.8621   0.8621
   0.250   0.0569   0.01780   0.01102  -0.0041   0.8470   0.8730
   0.500   0.1103   0.01782   0.01102  -0.0077   0.8306   0.8839
   0.750   0.1554   0.01782   0.01099  -0.0099   0.8121   0.8961
   1.000   0.2070   0.01787   0.01101  -0.0136   0.7905   0.9053
   1.250   0.2552   0.01785   0.01094  -0.0166   0.7687   0.9153
   1.500   0.2965   0.01782   0.01084  -0.0184   0.7461   0.9275
   1.750   0.3396   0.01781   0.01077  -0.0208   0.7209   0.9393
   2.000   0.3861   0.01776   0.01064  -0.0240   0.6951   0.9498
   2.250   0.4290   0.01767   0.01046  -0.0266   0.6694   0.9614
   2.500   0.4711   0.01758   0.01031  -0.0293   0.6417   0.9731
   2.750   0.5145   0.01744   0.01007  -0.0324   0.6139   0.9844
   3.000   0.5598   0.01721   0.00973  -0.0360   0.5847   0.9951
   3.250   0.5895   0.01709   0.00951  -0.0368   0.5583   1.0000
   3.500   0.6047   0.01716   0.00949  -0.0349   0.5362   1.0000
   3.750   0.6199   0.01724   0.00952  -0.0329   0.5138   1.0000
   4.000   0.6356   0.01736   0.00951  -0.0310   0.4931   1.0000
   4.250   0.6509   0.01751   0.00962  -0.0290   0.4714   1.0000
   4.500   0.6663   0.01769   0.00973  -0.0270   0.4502   1.0000
   4.750   0.6821   0.01791   0.00985  -0.0249   0.4303   1.0000
   5.000   0.6973   0.01818   0.01005  -0.0228   0.4100   1.0000
   5.250   0.7120   0.01848   0.01031  -0.0206   0.3896   1.0000
   5.500   0.7271   0.01882   0.01058  -0.0184   0.3703   1.0000
   5.750   0.7422   0.01919   0.01086  -0.0162   0.3516   1.0000
   6.000   0.7577   0.01963   0.01118  -0.0141   0.3335   1.0000
   6.250   0.7721   0.02007   0.01161  -0.0117   0.3150   1.0000
   6.500   0.7871   0.02056   0.01206  -0.0095   0.2974   1.0000
   6.750   0.8024   0.02109   0.01256  -0.0073   0.2807   1.0000
   7.000   0.8180   0.02167   0.01309  -0.0052   0.2648   1.0000
   7.250   0.8340   0.02231   0.01368  -0.0032   0.2498   1.0000
   7.500   0.8501   0.02299   0.01432  -0.0012   0.2357   1.0000
   7.750   0.8668   0.02373   0.01499   0.0007   0.2224   1.0000
   8.000   0.8840   0.02449   0.01565   0.0025   0.2097   1.0000
   8.250   0.8986   0.02522   0.01647   0.0047   0.1972   1.0000
   8.500   0.9139   0.02612   0.01743   0.0067   0.1858   1.0000
   8.750   0.9303   0.02707   0.01835   0.0085   0.1753   1.0000
   9.000   0.9483   0.02799   0.01914   0.0100   0.1652   1.0000
   9.250   0.9601   0.02898   0.02036   0.0125   0.1558   1.0000
   9.500   0.9768   0.03009   0.02140   0.0141   0.1473   1.0000
   9.750   0.9898   0.03105   0.02247   0.0163   0.1391   1.0000
  10.000   1.0039   0.03236   0.02383   0.0182   0.1318   1.0000
  10.250   1.0169   0.03340   0.02495   0.0202   0.1248   1.0000
  10.500   1.0302   0.03495   0.02658   0.0221   0.1185   1.0000
  10.750   1.0386   0.03622   0.02804   0.0246   0.1126   1.0000
  11.000   1.0571   0.03796   0.02964   0.0254   0.1069   1.0000
  11.250   1.0564   0.03956   0.03162   0.0290   0.1026   1.0000
  11.500   1.0637   0.04098   0.03316   0.0313   0.0982   1.0000
  11.750   1.0807   0.04325   0.03533   0.0319   0.0940   1.0000
  12.000   1.0699   0.04533   0.03782   0.0361   0.0919   1.0000
  12.250   1.0576   0.04743   0.04021   0.0401   0.0897   1.0000
  12.500   1.0492   0.04952   0.04249   0.0433   0.0875   1.0000
  12.750   1.0487   0.05134   0.04438   0.0453   0.0850   1.0000
  13.000   1.0660   0.05422   0.04712   0.0453   0.0819   1.0000
  13.250   1.0410   0.05728   0.05047   0.0480   0.0815   1.0000
  13.500   1.0150   0.06111   0.05457   0.0493   0.0813   1.0000
  13.750   0.9859   0.06579   0.05950   0.0491   0.0813   1.0000
  14.000   0.9533   0.07161   0.06554   0.0474   0.0814   1.0000
  14.250   0.9184   0.07872   0.07283   0.0443   0.0818   1.0000
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