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S3010-103-84 (s3010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S3010-103-84 (s3010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.17 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s3010-il-1000000-n5.txt
Download as CSV file: xf-s3010-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S3010-103-84                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.7513   0.04135   0.03938  -0.0523   1.0000   0.0062
 -10.500  -0.7740   0.03419   0.03183  -0.0560   1.0000   0.0063
 -10.250  -0.7735   0.03001   0.02730  -0.0569   1.0000   0.0063
 -10.000  -0.7585   0.02684   0.02381  -0.0582   0.9815   0.0064
  -9.750  -0.7364   0.02413   0.02077  -0.0599   0.9569   0.0065
  -9.500  -0.7186   0.02245   0.01882  -0.0594   0.9355   0.0066
  -9.250  -0.7001   0.02107   0.01722  -0.0585   0.9184   0.0067
  -9.000  -0.6800   0.01980   0.01572  -0.0578   0.9038   0.0068
  -8.750  -0.6581   0.01875   0.01447  -0.0572   0.8907   0.0070
  -8.500  -0.6352   0.01778   0.01330  -0.0567   0.8787   0.0071
  -8.250  -0.6115   0.01694   0.01229  -0.0563   0.8671   0.0072
  -8.000  -0.5869   0.01617   0.01137  -0.0559   0.8557   0.0073
  -7.750  -0.5616   0.01554   0.01060  -0.0556   0.8449   0.0074
  -7.500  -0.5362   0.01490   0.00983  -0.0553   0.8342   0.0075
  -7.250  -0.5101   0.01437   0.00916  -0.0550   0.8232   0.0075
  -7.000  -0.4844   0.01368   0.00835  -0.0548   0.8127   0.0076
  -6.750  -0.4590   0.01282   0.00735  -0.0545   0.8021   0.0078
  -6.500  -0.4327   0.01225   0.00667  -0.0543   0.7910   0.0080
  -6.250  -0.4059   0.01179   0.00612  -0.0541   0.7802   0.0081
  -6.000  -0.3788   0.01139   0.00565  -0.0540   0.7696   0.0083
  -5.750  -0.3515   0.01105   0.00522  -0.0538   0.7585   0.0085
  -5.500  -0.3241   0.01070   0.00480  -0.0537   0.7476   0.0087
  -5.250  -0.2965   0.01039   0.00442  -0.0536   0.7371   0.0089
  -5.000  -0.2688   0.01012   0.00407  -0.0534   0.7262   0.0092
  -4.750  -0.2409   0.00988   0.00377  -0.0534   0.7152   0.0096
  -4.500  -0.2130   0.00964   0.00347  -0.0533   0.7043   0.0099
  -4.250  -0.1850   0.00942   0.00318  -0.0532   0.6934   0.0102
  -4.000  -0.1570   0.00924   0.00292  -0.0531   0.6822   0.0104
  -3.750  -0.1289   0.00895   0.00258  -0.0530   0.6711   0.0109
  -3.500  -0.1008   0.00877   0.00233  -0.0530   0.6598   0.0115
  -3.250  -0.0726   0.00862   0.00213  -0.0529   0.6484   0.0121
  -3.000  -0.0443   0.00851   0.00196  -0.0529   0.6363   0.0127
  -2.750  -0.0160   0.00840   0.00179  -0.0528   0.6243   0.0135
  -2.500   0.0124   0.00829   0.00164  -0.0528   0.6119   0.0155
  -2.250   0.0406   0.00814   0.00149  -0.0528   0.5993   0.0248
  -2.000   0.0686   0.00795   0.00136  -0.0528   0.5863   0.0518
  -1.750   0.0967   0.00778   0.00126  -0.0528   0.5732   0.0816
  -1.500   0.1249   0.00764   0.00118  -0.0528   0.5603   0.1135
  -1.250   0.1531   0.00752   0.00112  -0.0528   0.5475   0.1474
  -1.000   0.1813   0.00737   0.00107  -0.0529   0.5351   0.1904
  -0.750   0.2093   0.00723   0.00103  -0.0529   0.5226   0.2400
  -0.500   0.2373   0.00707   0.00101  -0.0530   0.5100   0.3011
  -0.250   0.2652   0.00691   0.00100  -0.0531   0.4968   0.3709
   0.000   0.2933   0.00682   0.00100  -0.0531   0.4833   0.4209
   0.250   0.3214   0.00678   0.00101  -0.0531   0.4697   0.4621
   0.500   0.3494   0.00671   0.00104  -0.0531   0.4569   0.5122
   0.750   0.3774   0.00665   0.00107  -0.0531   0.4446   0.5639
   1.000   0.4053   0.00661   0.00111  -0.0531   0.4326   0.6122
   1.250   0.4331   0.00658   0.00116  -0.0530   0.4206   0.6581
   1.500   0.4607   0.00656   0.00122  -0.0529   0.4084   0.7039
   1.750   0.4881   0.00653   0.00129  -0.0527   0.3964   0.7524
   2.000   0.5149   0.00651   0.00137  -0.0524   0.3847   0.8032
   2.250   0.5407   0.00648   0.00145  -0.0518   0.3722   0.8549
   2.500   0.5647   0.00647   0.00153  -0.0507   0.3598   0.9103
   2.750   0.5952   0.00651   0.00159  -0.0511   0.3454   0.9734
   3.000   0.6280   0.00665   0.00167  -0.0521   0.3310   1.0000
   3.250   0.6557   0.00681   0.00176  -0.0521   0.3179   1.0000
   3.500   0.6833   0.00698   0.00186  -0.0520   0.3036   1.0000
   3.750   0.7109   0.00716   0.00198  -0.0520   0.2899   1.0000
   4.000   0.7383   0.00735   0.00210  -0.0519   0.2759   1.0000
   4.250   0.7658   0.00754   0.00223  -0.0519   0.2634   1.0000
   4.500   0.7931   0.00775   0.00238  -0.0518   0.2492   1.0000
   4.750   0.8203   0.00796   0.00254  -0.0517   0.2364   1.0000
   5.000   0.8474   0.00819   0.00270  -0.0516   0.2225   1.0000
   5.250   0.8744   0.00841   0.00287  -0.0515   0.2111   1.0000
   5.500   0.9012   0.00866   0.00306  -0.0514   0.1983   1.0000
   5.750   0.9280   0.00892   0.00326  -0.0513   0.1859   1.0000
   6.000   0.9547   0.00917   0.00346  -0.0511   0.1743   1.0000
   6.250   0.9813   0.00942   0.00368  -0.0510   0.1636   1.0000
   6.500   1.0076   0.00970   0.00392  -0.0508   0.1525   1.0000
   6.750   1.0336   0.01001   0.00417  -0.0506   0.1400   1.0000
   7.000   1.0595   0.01034   0.00444  -0.0504   0.1283   1.0000
   7.250   1.0851   0.01068   0.00473  -0.0502   0.1174   1.0000
   7.500   1.1110   0.01096   0.00500  -0.0500   0.1096   1.0000
   7.750   1.1365   0.01129   0.00530  -0.0497   0.1015   1.0000
   8.000   1.1613   0.01169   0.00564  -0.0494   0.0907   1.0000
   8.250   1.1857   0.01212   0.00602  -0.0490   0.0795   1.0000
   8.500   1.2103   0.01250   0.00637  -0.0487   0.0716   1.0000
   8.750   1.2349   0.01288   0.00673  -0.0483   0.0657   1.0000
   9.000   1.2588   0.01330   0.00713  -0.0479   0.0591   1.0000
   9.250   1.2826   0.01372   0.00753  -0.0475   0.0528   1.0000
   9.500   1.3056   0.01420   0.00799  -0.0469   0.0469   1.0000
   9.750   1.3285   0.01467   0.00844  -0.0464   0.0415   1.0000
  10.000   1.3508   0.01517   0.00893  -0.0458   0.0362   1.0000
  10.250   1.3721   0.01573   0.00948  -0.0451   0.0313   1.0000
  10.500   1.3939   0.01621   0.00997  -0.0444   0.0282   1.0000
  10.750   1.4145   0.01678   0.01054  -0.0436   0.0249   1.0000
  11.000   1.4348   0.01733   0.01110  -0.0427   0.0219   1.0000
  11.250   1.4538   0.01795   0.01173  -0.0417   0.0189   1.0000
  11.500   1.4709   0.01866   0.01245  -0.0405   0.0151   1.0000
  11.750   1.4858   0.01947   0.01325  -0.0390   0.0110   1.0000
  12.000   1.4986   0.02033   0.01413  -0.0372   0.0084   1.0000
  12.250   1.5083   0.02109   0.01493  -0.0349   0.0074   1.0000
  12.500   1.5172   0.02189   0.01579  -0.0326   0.0067   1.0000
  12.750   1.5252   0.02281   0.01677  -0.0304   0.0062   1.0000
  13.000   1.5326   0.02385   0.01787  -0.0285   0.0058   1.0000
  13.250   1.5394   0.02502   0.01911  -0.0267   0.0055   1.0000
  13.500   1.5456   0.02633   0.02048  -0.0251   0.0052   1.0000
  13.750   1.5526   0.02767   0.02190  -0.0238   0.0050   1.0000
  14.000   1.5586   0.02917   0.02348  -0.0227   0.0049   1.0000
  14.250   1.5637   0.03085   0.02525  -0.0218   0.0048   1.0000
  14.500   1.5675   0.03274   0.02722  -0.0210   0.0047   1.0000
  14.750   1.5701   0.03485   0.02943  -0.0204   0.0045   1.0000
  15.000   1.5722   0.03714   0.03181  -0.0201   0.0045   1.0000
  15.250   1.5719   0.03979   0.03456  -0.0200   0.0044   1.0000
  15.500   1.5708   0.04266   0.03753  -0.0202   0.0043   1.0000
  15.750   1.5684   0.04582   0.04078  -0.0206   0.0042   1.0000
  16.000   1.5640   0.04936   0.04444  -0.0213   0.0041   1.0000
  16.250   1.5574   0.05336   0.04854  -0.0223   0.0041   1.0000
  16.500   1.5500   0.05762   0.05292  -0.0236   0.0040   1.0000
  16.750   1.5414   0.06226   0.05768  -0.0253   0.0039   1.0000
  17.000   1.5318   0.06725   0.06278  -0.0272   0.0039   1.0000
  17.250   1.5179   0.07311   0.06878  -0.0297   0.0038   1.0000
  17.500   1.5070   0.07868   0.07446  -0.0322   0.0039   1.0000
  17.750   1.4901   0.08545   0.08137  -0.0354   0.0038   1.0000
  18.000   1.4717   0.09272   0.08878  -0.0390   0.0038   1.0000
  18.250   1.4545   0.10000   0.09619  -0.0427   0.0038   1.0000
  18.500   1.4348   0.10789   0.10423  -0.0468   0.0037   1.0000
  18.750   1.4181   0.11544   0.11190  -0.0509   0.0038   1.0000
  19.000   1.4005   0.12329   0.11988  -0.0552   0.0038   1.0000
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