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SD2083 (9.0%) (sd2083-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SD2083 (9.0%) (sd2083-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.3 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sd2083-il-1000000.txt
Download as CSV file: xf-sd2083-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD2083 (9.0%)                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.3991   0.08557   0.08401  -0.0359   1.0000   0.0110
  -8.750  -0.3996   0.08193   0.08039  -0.0375   1.0000   0.0110
  -8.500  -0.4023   0.07837   0.07687  -0.0389   1.0000   0.0116
  -8.250  -0.3940   0.07309   0.07161  -0.0450   0.9870   0.0119
  -8.000  -0.3742   0.06488   0.06338  -0.0592   0.9729   0.0127
  -6.750  -0.3720   0.02844   0.02547  -0.0733   0.9039   0.0141
  -6.500  -0.3541   0.02676   0.02366  -0.0730   0.8983   0.0146
  -6.250  -0.3336   0.02540   0.02217  -0.0726   0.8926   0.0151
  -6.000  -0.3133   0.02374   0.02031  -0.0720   0.8875   0.0157
  -5.750  -0.2920   0.02181   0.01814  -0.0714   0.8822   0.0166
  -5.500  -0.2693   0.02008   0.01616  -0.0707   0.8770   0.0176
  -5.250  -0.2508   0.01497   0.01020  -0.0683   0.8720   0.0140
  -5.000  -0.2246   0.01415   0.00924  -0.0679   0.8671   0.0137
  -4.750  -0.1999   0.01264   0.00753  -0.0673   0.8623   0.0138
  -4.500  -0.1753   0.01134   0.00606  -0.0667   0.8579   0.0141
  -4.250  -0.1498   0.01044   0.00509  -0.0662   0.8530   0.0144
  -4.000  -0.1238   0.00982   0.00439  -0.0658   0.8481   0.0146
  -3.750  -0.0978   0.00932   0.00380  -0.0654   0.8436   0.0149
  -3.500  -0.0711   0.00888   0.00332  -0.0652   0.8385   0.0153
  -3.250  -0.0443   0.00855   0.00293  -0.0649   0.8335   0.0160
  -3.000  -0.0174   0.00824   0.00254  -0.0647   0.8288   0.0165
  -2.750   0.0099   0.00795   0.00221  -0.0645   0.8233   0.0172
  -2.500   0.0372   0.00773   0.00192  -0.0643   0.8180   0.0184
  -2.250   0.0648   0.00757   0.00172  -0.0641   0.8125   0.0192
  -2.000   0.0924   0.00737   0.00148  -0.0640   0.8063   0.0227
  -1.750   0.1192   0.00709   0.00131  -0.0637   0.8004   0.0597
  -1.500   0.1456   0.00669   0.00120  -0.0636   0.7936   0.1418
  -1.250   0.1714   0.00629   0.00110  -0.0634   0.7872   0.2511
  -1.000   0.1976   0.00591   0.00104  -0.0632   0.7799   0.3568
  -0.750   0.2232   0.00557   0.00099  -0.0629   0.7728   0.4717
  -0.500   0.2486   0.00520   0.00097  -0.0625   0.7646   0.5910
  -0.250   0.2704   0.00469   0.00099  -0.0612   0.7570   0.7643
   0.000   0.2917   0.00432   0.00104  -0.0594   0.7483   0.9052
   0.250   0.3324   0.00430   0.00106  -0.0619   0.7391   0.9681
   0.500   0.3810   0.00436   0.00104  -0.0665   0.7299   0.9873
   0.750   0.4219   0.00440   0.00104  -0.0693   0.7200   0.9949
   1.000   0.4643   0.00443   0.00102  -0.0726   0.7100   0.9999
   1.250   0.4900   0.00448   0.00101  -0.0722   0.6989   1.0000
   1.500   0.5151   0.00454   0.00102  -0.0716   0.6872   1.0000
   1.750   0.5402   0.00461   0.00104  -0.0710   0.6739   1.0000
   2.000   0.5654   0.00469   0.00107  -0.0704   0.6592   1.0000
   2.250   0.5905   0.00479   0.00111  -0.0699   0.6423   1.0000
   2.500   0.6154   0.00490   0.00117  -0.0693   0.6231   1.0000
   2.750   0.6400   0.00505   0.00123  -0.0686   0.6019   1.0000
   3.000   0.6645   0.00522   0.00131  -0.0680   0.5771   1.0000
   3.250   0.6886   0.00542   0.00140  -0.0672   0.5484   1.0000
   3.500   0.7124   0.00566   0.00153  -0.0665   0.5152   1.0000
   3.750   0.7355   0.00597   0.00168  -0.0657   0.4764   1.0000
   4.000   0.7586   0.00629   0.00184  -0.0648   0.4365   1.0000
   4.250   0.7814   0.00663   0.00203  -0.0640   0.3972   1.0000
   4.500   0.8042   0.00700   0.00223  -0.0631   0.3584   1.0000
   4.750   0.8262   0.00744   0.00248  -0.0622   0.3124   1.0000
   5.000   0.8484   0.00788   0.00273  -0.0613   0.2701   1.0000
   5.250   0.8707   0.00832   0.00298  -0.0604   0.2323   1.0000
   5.500   0.8938   0.00869   0.00323  -0.0597   0.2047   1.0000
   5.750   0.9168   0.00907   0.00350  -0.0590   0.1778   1.0000
   6.000   0.9392   0.00951   0.00380  -0.0582   0.1472   1.0000
   6.250   0.9603   0.01006   0.00415  -0.0572   0.1122   1.0000
   6.500   0.9818   0.01057   0.00452  -0.0563   0.0841   1.0000
   6.750   1.0028   0.01114   0.00494  -0.0553   0.0574   1.0000
   7.000   1.0207   0.01199   0.00556  -0.0538   0.0225   1.0000
   7.250   1.0406   0.01267   0.00616  -0.0525   0.0097   1.0000
   7.500   1.0623   0.01316   0.00668  -0.0515   0.0082   1.0000
   7.750   1.0825   0.01380   0.00741  -0.0503   0.0072   1.0000
   8.000   1.1040   0.01427   0.00793  -0.0493   0.0069   1.0000
   8.250   1.1250   0.01477   0.00849  -0.0483   0.0065   1.0000
   8.500   1.1450   0.01536   0.00914  -0.0471   0.0062   1.0000
   8.750   1.1641   0.01598   0.00983  -0.0458   0.0060   1.0000
   9.000   1.1822   0.01666   0.01057  -0.0443   0.0058   1.0000
   9.250   1.1990   0.01740   0.01139  -0.0427   0.0056   1.0000
   9.500   1.2145   0.01819   0.01225  -0.0409   0.0054   1.0000
   9.750   1.2273   0.01910   0.01324  -0.0387   0.0052   1.0000
  10.000   1.2362   0.02004   0.01427  -0.0358   0.0052   1.0000
  10.250   1.2427   0.02113   0.01546  -0.0327   0.0051   1.0000
  10.500   1.2378   0.02323   0.01771  -0.0283   0.0048   1.0000
  10.750   1.2424   0.02480   0.01940  -0.0255   0.0048   1.0000
  11.000   1.2538   0.02572   0.02041  -0.0236   0.0047   1.0000
  11.250   1.2609   0.02711   0.02190  -0.0214   0.0046   1.0000
  11.500   1.2693   0.02837   0.02328  -0.0195   0.0046   1.0000
  11.750   1.2772   0.02968   0.02471  -0.0176   0.0043   1.0000
  12.000   1.2810   0.03148   0.02664  -0.0156   0.0043   1.0000
  12.250   1.2825   0.03359   0.02892  -0.0135   0.0043   1.0000
  12.500   1.2842   0.03565   0.03112  -0.0118   0.0042   1.0000
  12.750   1.2814   0.03836   0.03401  -0.0099   0.0043   1.0000
  13.000   1.2777   0.04115   0.03697  -0.0085   0.0043   1.0000
  13.250   1.2705   0.04448   0.04049  -0.0072   0.0043   1.0000
  13.500   1.2612   0.04814   0.04435  -0.0064   0.0043   1.0000
  13.750   1.2517   0.05196   0.04834  -0.0061   0.0044   1.0000
  14.000   1.2384   0.05653   0.05309  -0.0064   0.0044   1.0000
  14.250   1.2230   0.06164   0.05839  -0.0074   0.0044   1.0000
  14.500   1.2072   0.06724   0.06415  -0.0091   0.0045   1.0000
  14.750   1.1876   0.07393   0.07103  -0.0118   0.0045   1.0000
  15.000   1.1693   0.08098   0.07825  -0.0153   0.0046   1.0000
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