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SG6050 (sg6050-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SG6050 (sg6050-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.96 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sg6050-il-1000000-n5.txt
Download as CSV file: xf-sg6050-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6050                                          
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8755   0.10885   0.10603  -0.0341   1.0000   0.0048
 -17.250  -0.9292   0.09520   0.09217  -0.0410   1.0000   0.0047
 -17.000  -0.9740   0.08361   0.08040  -0.0471   1.0000   0.0046
 -16.750  -1.0128   0.07383   0.07045  -0.0524   1.0000   0.0046
 -16.500  -1.0445   0.06560   0.06207  -0.0569   1.0000   0.0046
 -16.250  -1.0710   0.05829   0.05462  -0.0611   1.0000   0.0046
 -16.000  -1.0916   0.05169   0.04788  -0.0651   1.0000   0.0046
 -15.750  -1.1056   0.04572   0.04178  -0.0691   1.0000   0.0046
 -15.500  -1.1134   0.04043   0.03635  -0.0732   1.0000   0.0046
 -15.250  -1.1170   0.03595   0.03173  -0.0768   1.0000   0.0046
 -15.000  -1.1179   0.03245   0.02810  -0.0793   1.0000   0.0047
 -14.750  -1.1170   0.02986   0.02540  -0.0801   1.0000   0.0047
 -14.500  -1.1150   0.02790   0.02334  -0.0798   1.0000   0.0047
 -14.250  -1.1087   0.02633   0.02167  -0.0792   0.9915   0.0048
 -14.000  -1.1009   0.02507   0.02031  -0.0780   0.9664   0.0049
 -13.750  -1.0932   0.02413   0.01923  -0.0757   0.9327   0.0049
 -13.500  -1.0819   0.02328   0.01822  -0.0739   0.9088   0.0050
 -13.250  -1.0667   0.02247   0.01728  -0.0727   0.8912   0.0050
 -12.750  -1.0301   0.02102   0.01558  -0.0711   0.8648   0.0051
 -12.500  -1.0100   0.02032   0.01478  -0.0705   0.8551   0.0052
 -12.250  -0.9899   0.01955   0.01390  -0.0699   0.8455   0.0054
 -12.000  -0.9684   0.01886   0.01311  -0.0695   0.8371   0.0055
 -11.750  -0.9459   0.01824   0.01240  -0.0691   0.8287   0.0057
 -11.500  -0.9224   0.01767   0.01176  -0.0689   0.8218   0.0059
 -11.250  -0.8983   0.01714   0.01116  -0.0687   0.8151   0.0061
 -11.000  -0.8737   0.01666   0.01060  -0.0685   0.8091   0.0064
 -10.750  -0.8484   0.01620   0.01006  -0.0685   0.8033   0.0066
 -10.500  -0.8227   0.01578   0.00957  -0.0685   0.7972   0.0069
 -10.250  -0.7971   0.01531   0.00905  -0.0684   0.7918   0.0074
 -10.000  -0.7710   0.01486   0.00856  -0.0685   0.7868   0.0079
  -9.750  -0.7446   0.01446   0.00810  -0.0686   0.7816   0.0086
  -9.250  -0.6913   0.01363   0.00719  -0.0688   0.7720   0.0119
  -9.000  -0.6646   0.01317   0.00672  -0.0689   0.7670   0.0160
  -8.750  -0.6377   0.01273   0.00627  -0.0691   0.7621   0.0217
  -8.500  -0.6104   0.01234   0.00589  -0.0693   0.7578   0.0283
  -8.250  -0.5824   0.01201   0.00559  -0.0696   0.7534   0.0345
  -8.000  -0.5540   0.01177   0.00534  -0.0699   0.7489   0.0392
  -7.750  -0.5256   0.01155   0.00510  -0.0702   0.7447   0.0426
  -7.500  -0.4967   0.01136   0.00489  -0.0706   0.7408   0.0458
  -7.250  -0.4679   0.01114   0.00468  -0.0709   0.7367   0.0494
  -7.000  -0.4389   0.01096   0.00449  -0.0713   0.7324   0.0528
  -6.750  -0.4097   0.01083   0.00431  -0.0717   0.7283   0.0547
  -6.500  -0.3806   0.01063   0.00411  -0.0721   0.7247   0.0578
  -6.250  -0.3514   0.01045   0.00392  -0.0725   0.7208   0.0609
  -6.000  -0.3220   0.01031   0.00376  -0.0730   0.7165   0.0634
  -5.750  -0.2926   0.01017   0.00359  -0.0734   0.7124   0.0664
  -5.500  -0.2633   0.01000   0.00342  -0.0738   0.7087   0.0703
  -5.250  -0.2337   0.00985   0.00326  -0.0743   0.7044   0.0734
  -5.000  -0.2041   0.00973   0.00312  -0.0747   0.6993   0.0760
  -4.750  -0.1747   0.00958   0.00296  -0.0752   0.6945   0.0822
  -4.500  -0.1450   0.00945   0.00284  -0.0756   0.6899   0.0877
  -4.250  -0.1154   0.00929   0.00270  -0.0761   0.6850   0.0970
  -4.000  -0.0858   0.00914   0.00257  -0.0766   0.6801   0.1085
  -3.750  -0.0562   0.00897   0.00244  -0.0771   0.6758   0.1242
  -3.250   0.0029   0.00855   0.00218  -0.0782   0.6655   0.1767
  -3.000   0.0321   0.00824   0.00204  -0.0787   0.6608   0.2258
  -2.750   0.0617   0.00802   0.00195  -0.0793   0.6555   0.2655
  -2.500   0.0914   0.00790   0.00190  -0.0798   0.6499   0.2925
  -2.250   0.1212   0.00784   0.00186  -0.0803   0.6446   0.3117
  -2.000   0.1512   0.00779   0.00184  -0.0809   0.6387   0.3259
  -1.750   0.1810   0.00777   0.00182  -0.0813   0.6323   0.3380
  -1.500   0.2110   0.00776   0.00181  -0.0818   0.6262   0.3473
  -1.250   0.2409   0.00775   0.00180  -0.0823   0.6194   0.3567
  -1.000   0.2706   0.00775   0.00181  -0.0828   0.6131   0.3731
  -0.750   0.3006   0.00774   0.00182  -0.0833   0.6071   0.3844
  -0.500   0.3304   0.00775   0.00182  -0.0838   0.6005   0.3907
  -0.250   0.3603   0.00777   0.00182  -0.0843   0.5942   0.3945
   0.000   0.3901   0.00780   0.00183  -0.0848   0.5871   0.3974
   0.250   0.4198   0.00783   0.00184  -0.0853   0.5803   0.4009
   0.500   0.4496   0.00784   0.00185  -0.0858   0.5723   0.4051
   0.750   0.4791   0.00789   0.00188  -0.0862   0.5639   0.4091
   1.000   0.5086   0.00794   0.00190  -0.0866   0.5544   0.4132
   1.250   0.5381   0.00799   0.00194  -0.0871   0.5457   0.4174
   1.500   0.5674   0.00804   0.00198  -0.0875   0.5366   0.4225
   1.750   0.5968   0.00809   0.00203  -0.0880   0.5282   0.4281
   2.250   0.6553   0.00821   0.00214  -0.0888   0.5106   0.4404
   2.500   0.6842   0.00830   0.00221  -0.0892   0.5014   0.4483
   2.750   0.7134   0.00834   0.00229  -0.0896   0.4924   0.4599
   3.000   0.7423   0.00840   0.00238  -0.0900   0.4832   0.4751
   3.250   0.7710   0.00846   0.00247  -0.0904   0.4728   0.4975
   3.500   0.7998   0.00849   0.00258  -0.0908   0.4626   0.5328
   3.750   0.8280   0.00851   0.00271  -0.0911   0.4498   0.5840
   4.000   0.8561   0.00853   0.00285  -0.0915   0.4369   0.6487
   4.250   0.8841   0.00852   0.00301  -0.0918   0.4250   0.7164
   4.500   0.9113   0.00846   0.00318  -0.0918   0.4140   0.7991
   4.750   0.9370   0.00853   0.00338  -0.0914   0.4030   0.8600
   5.000   0.9626   0.00869   0.00355  -0.0911   0.3903   0.8861
   5.250   0.9878   0.00887   0.00373  -0.0907   0.3762   0.9051
   5.500   1.0120   0.00904   0.00390  -0.0900   0.3633   0.9244
   5.750   1.0339   0.00920   0.00407  -0.0888   0.3511   0.9455
   6.000   1.0557   0.00937   0.00422  -0.0876   0.3386   0.9741
   6.250   1.0833   0.00959   0.00439  -0.0878   0.3247   1.0000
   6.500   1.1088   0.00991   0.00464  -0.0877   0.3079   1.0000
   6.750   1.1338   0.01024   0.00490  -0.0875   0.2906   1.0000
   7.000   1.1584   0.01059   0.00518  -0.0872   0.2742   1.0000
   7.250   1.1824   0.01097   0.00548  -0.0868   0.2577   1.0000
   7.500   1.2049   0.01142   0.00583  -0.0861   0.2380   1.0000
   7.750   1.2246   0.01202   0.00628  -0.0850   0.2097   1.0000
   8.000   1.2417   0.01273   0.00681  -0.0835   0.1791   1.0000
   8.250   1.2599   0.01333   0.00730  -0.0822   0.1584   1.0000
   8.500   1.2776   0.01389   0.00777  -0.0808   0.1413   1.0000
   8.750   1.2942   0.01448   0.00828  -0.0791   0.1258   1.0000
   9.000   1.3071   0.01508   0.00883  -0.0768   0.1122   1.0000
   9.250   1.3198   0.01574   0.00944  -0.0745   0.1001   1.0000
   9.500   1.3322   0.01648   0.01012  -0.0723   0.0879   1.0000
   9.750   1.3436   0.01732   0.01090  -0.0702   0.0753   1.0000
  10.000   1.3555   0.01820   0.01172  -0.0682   0.0649   1.0000
  10.250   1.3680   0.01908   0.01258  -0.0665   0.0565   1.0000
  10.500   1.3804   0.02003   0.01351  -0.0649   0.0496   1.0000
  10.750   1.3924   0.02103   0.01450  -0.0633   0.0434   1.0000
  11.000   1.4046   0.02207   0.01552  -0.0619   0.0381   1.0000
  11.250   1.4168   0.02315   0.01661  -0.0606   0.0335   1.0000
  11.500   1.4281   0.02432   0.01778  -0.0593   0.0293   1.0000
  11.750   1.4385   0.02558   0.01904  -0.0580   0.0257   1.0000
  12.000   1.4495   0.02683   0.02031  -0.0568   0.0228   1.0000
  12.250   1.4598   0.02817   0.02167  -0.0556   0.0203   1.0000
  12.500   1.4688   0.02962   0.02314  -0.0544   0.0179   1.0000
  12.750   1.4779   0.03109   0.02465  -0.0533   0.0155   1.0000
  13.000   1.4856   0.03271   0.02629  -0.0522   0.0133   1.0000
  13.250   1.4925   0.03443   0.02804  -0.0511   0.0113   1.0000
  13.500   1.4988   0.03621   0.02985  -0.0500   0.0098   1.0000
  13.750   1.5054   0.03799   0.03168  -0.0491   0.0089   1.0000
  14.000   1.5114   0.03989   0.03362  -0.0482   0.0082   1.0000
  14.250   1.5165   0.04192   0.03571  -0.0473   0.0077   1.0000
  14.500   1.5223   0.04392   0.03777  -0.0466   0.0073   1.0000
  14.750   1.5278   0.04600   0.03990  -0.0459   0.0070   1.0000
  15.000   1.5323   0.04823   0.04220  -0.0453   0.0068   1.0000
  15.250   1.5359   0.05061   0.04464  -0.0448   0.0065   1.0000
  15.500   1.5389   0.05311   0.04720  -0.0443   0.0063   1.0000
  15.750   1.5408   0.05574   0.04991  -0.0439   0.0061   1.0000
  16.000   1.5418   0.05854   0.05277  -0.0436   0.0059   1.0000
  16.250   1.5426   0.06143   0.05573  -0.0434   0.0058   1.0000
  16.500   1.5439   0.06432   0.05871  -0.0433   0.0057   1.0000
  16.750   1.5444   0.06735   0.06182  -0.0432   0.0056   1.0000
  17.000   1.5440   0.07050   0.06505  -0.0433   0.0055   1.0000
  17.250   1.5429   0.07378   0.06841  -0.0434   0.0054   1.0000
  17.500   1.5412   0.07721   0.07192  -0.0437   0.0054   1.0000
  17.750   1.5388   0.08078   0.07557  -0.0441   0.0053   1.0000
  18.000   1.5353   0.08454   0.07942  -0.0446   0.0052   1.0000
  18.250   1.5310   0.08842   0.08339  -0.0451   0.0051   1.0000
  18.500   1.5259   0.09246   0.08751  -0.0458   0.0050   1.0000
  18.750   1.5204   0.09663   0.09178  -0.0467   0.0049   1.0000
  19.000   1.5145   0.10091   0.09615  -0.0476   0.0048   1.0000
  19.250   1.5078   0.10535   0.10067  -0.0488   0.0048   1.0000
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