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SD2030-086-88 (sd2030-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SD2030-086-88 (sd2030-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.43 at α=2.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sd2030-il-1000000.txt
Download as CSV file: xf-sd2030-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD2030-086-88                                   
  
 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  -0.4603   0.08496   0.08337  -0.0325   1.0000   0.0118
  -8.750  -0.4692   0.08186   0.08031  -0.0322   1.0000   0.0122
  -8.500  -0.4821   0.07892   0.07741  -0.0313   1.0000   0.0123
  -8.250  -0.4875   0.07389   0.07241  -0.0357   0.9985   0.0124
  -8.000  -0.4715   0.06426   0.06272  -0.0516   0.9944   0.0129
  -7.250  -0.4417   0.02995   0.02713  -0.0751   0.9810   0.0146
  -7.000  -0.4202   0.02727   0.02426  -0.0761   0.9777   0.0151
  -6.750  -0.3919   0.02596   0.02286  -0.0776   0.9760   0.0156
  -6.500  -0.3687   0.01940   0.01552  -0.0781   0.9737   0.0133
  -6.250  -0.3405   0.01665   0.01239  -0.0789   0.9722   0.0130
  -6.000  -0.3099   0.01532   0.01085  -0.0798   0.9708   0.0133
  -5.750  -0.2882   0.01455   0.00994  -0.0786   0.9656   0.0137
  -5.500  -0.2606   0.01365   0.00889  -0.0786   0.9625   0.0139
  -5.250  -0.2333   0.01225   0.00730  -0.0786   0.9597   0.0143
  -5.000  -0.2072   0.01090   0.00583  -0.0784   0.9570   0.0147
  -4.750  -0.1853   0.01018   0.00505  -0.0772   0.9514   0.0151
  -4.500  -0.1595   0.00961   0.00442  -0.0767   0.9473   0.0156
  -4.250  -0.1330   0.00914   0.00390  -0.0764   0.9438   0.0160
  -4.000  -0.1081   0.00877   0.00349  -0.0757   0.9386   0.0165
  -3.750  -0.0820   0.00844   0.00313  -0.0753   0.9336   0.0174
  -3.500  -0.0552   0.00811   0.00274  -0.0750   0.9294   0.0183
  -3.250  -0.0293   0.00785   0.00243  -0.0745   0.9232   0.0191
  -3.000  -0.0027   0.00758   0.00211  -0.0741   0.9177   0.0202
  -2.750   0.0242   0.00733   0.00182  -0.0738   0.9119   0.0234
  -2.500   0.0505   0.00706   0.00161  -0.0734   0.9048   0.0395
  -2.250   0.0767   0.00673   0.00144  -0.0731   0.8977   0.0897
  -2.000   0.1027   0.00640   0.00131  -0.0727   0.8896   0.1525
  -1.750   0.1285   0.00603   0.00120  -0.0725   0.8814   0.2397
  -1.500   0.1541   0.00564   0.00110  -0.0722   0.8732   0.3474
  -1.250   0.1792   0.00520   0.00103  -0.0718   0.8641   0.4733
  -1.000   0.2032   0.00468   0.00098  -0.0712   0.8555   0.6376
  -0.750   0.2264   0.00431   0.00102  -0.0701   0.8462   0.7762
  -0.500   0.2519   0.00423   0.00104  -0.0694   0.8368   0.8241
  -0.250   0.2779   0.00421   0.00105  -0.0688   0.8276   0.8525
   0.000   0.3035   0.00421   0.00106  -0.0680   0.8175   0.8767
   0.250   0.3290   0.00423   0.00108  -0.0673   0.8066   0.8967
   0.500   0.3543   0.00425   0.00110  -0.0665   0.7954   0.9126
   0.750   0.3791   0.00429   0.00112  -0.0656   0.7835   0.9266
   1.000   0.4034   0.00433   0.00114  -0.0646   0.7703   0.9395
   1.250   0.4275   0.00438   0.00116  -0.0636   0.7555   0.9514
   1.500   0.4525   0.00443   0.00118  -0.0627   0.7380   0.9627
   1.750   0.4794   0.00452   0.00120  -0.0624   0.7170   0.9733
   2.000   0.5097   0.00466   0.00123  -0.0628   0.6884   0.9815
   2.250   0.5437   0.00485   0.00128  -0.0642   0.6499   0.9864
   2.500   0.5779   0.00514   0.00136  -0.0658   0.5976   0.9904
   2.750   0.6102   0.00551   0.00148  -0.0670   0.5362   0.9948
   3.000   0.6435   0.00592   0.00162  -0.0685   0.4739   0.9984
   3.250   0.6679   0.00629   0.00176  -0.0681   0.4194   1.0000
   3.500   0.6851   0.00661   0.00190  -0.0661   0.3764   1.0000
   3.750   0.7036   0.00696   0.00207  -0.0643   0.3321   1.0000
   4.000   0.7244   0.00730   0.00224  -0.0631   0.2919   1.0000
   4.250   0.7465   0.00765   0.00243  -0.0621   0.2549   1.0000
   4.500   0.7698   0.00797   0.00262  -0.0613   0.2252   1.0000
   4.750   0.7932   0.00830   0.00283  -0.0606   0.1952   1.0000
   5.000   0.8168   0.00864   0.00305  -0.0599   0.1683   1.0000
   5.250   0.8406   0.00898   0.00328  -0.0593   0.1454   1.0000
   5.500   0.8648   0.00930   0.00352  -0.0587   0.1253   1.0000
   5.750   0.8885   0.00966   0.00379  -0.0581   0.1057   1.0000
   6.000   0.9123   0.01001   0.00406  -0.0575   0.0877   1.0000
   6.250   0.9359   0.01038   0.00436  -0.0568   0.0725   1.0000
   6.500   0.9598   0.01073   0.00465  -0.0562   0.0614   1.0000
   6.750   0.9837   0.01108   0.00498  -0.0556   0.0524   1.0000
   7.000   1.0071   0.01146   0.00531  -0.0550   0.0442   1.0000
   7.250   1.0314   0.01175   0.00562  -0.0545   0.0399   1.0000
   7.500   1.0545   0.01217   0.00599  -0.0538   0.0334   1.0000
   7.750   1.0787   0.01245   0.00630  -0.0532   0.0306   1.0000
   8.000   1.1015   0.01286   0.00670  -0.0525   0.0257   1.0000
   8.250   1.1248   0.01323   0.00707  -0.0519   0.0212   1.0000
   8.500   1.1451   0.01389   0.00764  -0.0507   0.0125   1.0000
   8.750   1.1656   0.01453   0.00829  -0.0496   0.0093   1.0000
   9.000   1.1868   0.01509   0.00891  -0.0486   0.0081   1.0000
   9.250   1.2077   0.01564   0.00952  -0.0475   0.0075   1.0000
   9.500   1.2273   0.01632   0.01026  -0.0463   0.0069   1.0000
   9.750   1.2433   0.01733   0.01139  -0.0444   0.0061   1.0000
  10.000   1.2618   0.01803   0.01218  -0.0431   0.0059   1.0000
  10.250   1.2801   0.01870   0.01293  -0.0417   0.0055   1.0000
  10.500   1.2972   0.01944   0.01375  -0.0401   0.0054   1.0000
  10.750   1.3120   0.02029   0.01469  -0.0382   0.0052   1.0000
  11.000   1.3248   0.02110   0.01559  -0.0359   0.0051   1.0000
  11.250   1.3351   0.02203   0.01665  -0.0333   0.0050   1.0000
  11.500   1.3458   0.02292   0.01762  -0.0309   0.0048   1.0000
  11.750   1.3543   0.02397   0.01877  -0.0283   0.0047   1.0000
  12.000   1.3626   0.02503   0.01994  -0.0258   0.0046   1.0000
  12.250   1.3680   0.02632   0.02134  -0.0230   0.0045   1.0000
  12.500   1.3724   0.02769   0.02283  -0.0204   0.0045   1.0000
  12.750   1.3747   0.02925   0.02451  -0.0177   0.0044   1.0000
  13.000   1.3747   0.03106   0.02646  -0.0151   0.0044   1.0000
  13.250   1.3718   0.03318   0.02872  -0.0126   0.0043   1.0000
  13.500   1.3659   0.03569   0.03139  -0.0103   0.0042   1.0000
  13.750   1.3596   0.03840   0.03426  -0.0085   0.0042   1.0000
  14.000   1.3520   0.04143   0.03745  -0.0071   0.0042   1.0000
  14.250   1.3295   0.04638   0.04264  -0.0062   0.0040   1.0000
  14.500   1.3243   0.04970   0.04609  -0.0062   0.0041   1.0000
  14.750   1.3069   0.05491   0.05149  -0.0071   0.0040   1.0000
  15.500   1.2506   0.07516   0.07230  -0.0164   0.0039   1.0000
  15.750   1.2375   0.08201   0.07927  -0.0203   0.0040   1.0000
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