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SD5060 (9.5%) (sd5060-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SD5060 (9.5%) (sd5060-il)
Reynolds number: 500,000
Max Cl/Cd: 79.78 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd5060-il-500000-n5.txt
Download as CSV file: xf-sd5060-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD5060 (9.5%)                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.7289   0.07684   0.07440  -0.0204   1.0000   0.0084
 -11.750  -0.7758   0.06336   0.06083  -0.0294   1.0000   0.0083
 -11.500  -0.8154   0.05057   0.04791  -0.0397   1.0000   0.0081
 -11.250  -0.8442   0.04058   0.03770  -0.0509   1.0000   0.0079
 -11.000  -0.8558   0.03614   0.03297  -0.0530   1.0000   0.0080
 -10.750  -0.8525   0.03299   0.02953  -0.0537   1.0000   0.0082
 -10.500  -0.8433   0.03035   0.02661  -0.0540   1.0000   0.0084
 -10.250  -0.8297   0.02814   0.02410  -0.0540   1.0000   0.0086
 -10.000  -0.8124   0.02643   0.02216  -0.0539   1.0000   0.0088
  -9.750  -0.7971   0.02415   0.01965  -0.0538   1.0000   0.0091
  -9.500  -0.7761   0.02297   0.01836  -0.0536   1.0000   0.0094
  -9.250  -0.7538   0.02204   0.01733  -0.0535   1.0000   0.0097
  -9.000  -0.7314   0.02105   0.01623  -0.0532   1.0000   0.0100
  -8.750  -0.7088   0.02010   0.01515  -0.0529   1.0000   0.0104
  -8.500  -0.6811   0.01923   0.01414  -0.0536   0.9915   0.0109
  -8.250  -0.6495   0.01837   0.01312  -0.0549   0.9802   0.0116
  -8.000  -0.6182   0.01758   0.01219  -0.0560   0.9701   0.0120
  -7.750  -0.5890   0.01688   0.01134  -0.0566   0.9589   0.0123
  -7.500  -0.5635   0.01568   0.01000  -0.0566   0.9470   0.0128
  -7.250  -0.5388   0.01485   0.00908  -0.0563   0.9355   0.0133
  -7.000  -0.5141   0.01428   0.00841  -0.0558   0.9248   0.0139
  -6.750  -0.4891   0.01382   0.00786  -0.0553   0.9143   0.0146
  -6.500  -0.4639   0.01334   0.00730  -0.0548   0.9042   0.0153
  -6.250  -0.4384   0.01287   0.00672  -0.0543   0.8948   0.0158
  -6.000  -0.4127   0.01243   0.00617  -0.0538   0.8853   0.0163
  -5.750  -0.3864   0.01203   0.00567  -0.0534   0.8761   0.0167
  -5.500  -0.3602   0.01161   0.00516  -0.0530   0.8673   0.0171
  -5.250  -0.3337   0.01114   0.00461  -0.0527   0.8581   0.0182
  -5.000  -0.3068   0.01080   0.00420  -0.0525   0.8494   0.0195
  -4.750  -0.2798   0.01052   0.00384  -0.0522   0.8406   0.0207
  -4.500  -0.2524   0.01027   0.00351  -0.0520   0.8317   0.0219
  -4.250  -0.2250   0.01002   0.00320  -0.0517   0.8231   0.0243
  -4.000  -0.1975   0.00974   0.00292  -0.0516   0.8140   0.0306
  -3.750  -0.1703   0.00941   0.00264  -0.0514   0.8053   0.0517
  -3.500  -0.1429   0.00915   0.00242  -0.0513   0.7963   0.0739
  -3.250  -0.1153   0.00889   0.00224  -0.0512   0.7870   0.1002
  -3.000  -0.0877   0.00867   0.00208  -0.0511   0.7780   0.1260
  -2.750  -0.0599   0.00853   0.00195  -0.0510   0.7683   0.1433
  -2.500  -0.0320   0.00838   0.00184  -0.0509   0.7588   0.1638
  -2.250  -0.0041   0.00825   0.00173  -0.0508   0.7492   0.1864
  -2.000   0.0238   0.00812   0.00163  -0.0507   0.7388   0.2093
  -1.750   0.0517   0.00797   0.00155  -0.0506   0.7283   0.2385
  -1.500   0.0795   0.00784   0.00148  -0.0506   0.7176   0.2720
  -1.250   0.1073   0.00773   0.00141  -0.0505   0.7062   0.3019
  -1.000   0.1353   0.00763   0.00136  -0.0504   0.6940   0.3303
  -0.750   0.1632   0.00754   0.00132  -0.0503   0.6811   0.3632
  -0.500   0.1910   0.00745   0.00128  -0.0502   0.6674   0.3971
  -0.250   0.2187   0.00736   0.00126  -0.0501   0.6525   0.4374
   0.000   0.2462   0.00728   0.00125  -0.0500   0.6367   0.4804
   0.250   0.2737   0.00720   0.00125  -0.0498   0.6201   0.5281
   0.500   0.3010   0.00712   0.00127  -0.0496   0.6033   0.5781
   0.750   0.3281   0.00704   0.00130  -0.0494   0.5860   0.6332
   1.000   0.3548   0.00696   0.00135  -0.0490   0.5678   0.6912
   1.250   0.3807   0.00689   0.00140  -0.0485   0.5484   0.7531
   1.500   0.4054   0.00682   0.00147  -0.0475   0.5279   0.8195
   1.750   0.4283   0.00677   0.00153  -0.0461   0.5056   0.8929
   2.000   0.4640   0.00682   0.00157  -0.0475   0.4793   0.9742
   2.250   0.4953   0.00700   0.00163  -0.0483   0.4539   1.0000
   2.500   0.5222   0.00722   0.00172  -0.0481   0.4276   1.0000
   2.750   0.5491   0.00745   0.00183  -0.0479   0.4004   1.0000
   3.000   0.5759   0.00771   0.00195  -0.0477   0.3714   1.0000
   3.250   0.6025   0.00798   0.00209  -0.0475   0.3428   1.0000
   3.500   0.6293   0.00824   0.00225  -0.0474   0.3179   1.0000
   3.750   0.6559   0.00852   0.00242  -0.0472   0.2919   1.0000
   4.000   0.6823   0.00883   0.00261  -0.0470   0.2658   1.0000
   4.250   0.7088   0.00913   0.00280  -0.0468   0.2442   1.0000
   4.500   0.7353   0.00941   0.00302  -0.0466   0.2257   1.0000
   4.750   0.7617   0.00971   0.00324  -0.0464   0.2066   1.0000
   5.000   0.7881   0.01001   0.00347  -0.0462   0.1900   1.0000
   5.250   0.8145   0.01029   0.00371  -0.0460   0.1765   1.0000
   5.500   0.8406   0.01060   0.00397  -0.0458   0.1625   1.0000
   5.750   0.8668   0.01090   0.00423  -0.0455   0.1508   1.0000
   6.000   0.8928   0.01122   0.00451  -0.0453   0.1397   1.0000
   6.500   0.9446   0.01184   0.00510  -0.0448   0.1209   1.0000
   6.750   0.9701   0.01218   0.00542  -0.0445   0.1117   1.0000
   7.000   0.9954   0.01256   0.00576  -0.0441   0.1029   1.0000
   7.250   1.0210   0.01286   0.00609  -0.0438   0.0968   1.0000
   7.750   1.0711   0.01360   0.00684  -0.0431   0.0830   1.0000
   8.000   1.0955   0.01402   0.00725  -0.0427   0.0762   1.0000
   8.250   1.1199   0.01442   0.00765  -0.0423   0.0686   1.0000
   8.500   1.1438   0.01487   0.00811  -0.0418   0.0614   1.0000
   8.750   1.1669   0.01540   0.00860  -0.0413   0.0524   1.0000
   9.000   1.1897   0.01594   0.00912  -0.0407   0.0447   1.0000
   9.250   1.2124   0.01647   0.00966  -0.0401   0.0389   1.0000
   9.500   1.2341   0.01709   0.01026  -0.0394   0.0332   1.0000
   9.750   1.2560   0.01766   0.01085  -0.0387   0.0288   1.0000
  10.000   1.2768   0.01832   0.01154  -0.0379   0.0244   1.0000
  10.250   1.2972   0.01897   0.01222  -0.0371   0.0209   1.0000
  10.500   1.3170   0.01966   0.01294  -0.0362   0.0180   1.0000
  10.750   1.3355   0.02041   0.01373  -0.0351   0.0150   1.0000
  11.000   1.3534   0.02119   0.01455  -0.0340   0.0123   1.0000
  11.250   1.3694   0.02207   0.01548  -0.0327   0.0101   1.0000
  11.500   1.3846   0.02295   0.01643  -0.0313   0.0086   1.0000
  11.750   1.3967   0.02394   0.01749  -0.0295   0.0075   1.0000
  12.000   1.4066   0.02486   0.01850  -0.0273   0.0067   1.0000
  12.250   1.4147   0.02589   0.01962  -0.0251   0.0062   1.0000
  12.500   1.4214   0.02708   0.02090  -0.0231   0.0058   1.0000
  12.750   1.4258   0.02851   0.02242  -0.0211   0.0054   1.0000
  13.000   1.4308   0.02999   0.02401  -0.0194   0.0051   1.0000
  13.250   1.4362   0.03152   0.02566  -0.0181   0.0048   1.0000
  13.500   1.4399   0.03329   0.02755  -0.0169   0.0047   1.0000
  13.750   1.4422   0.03530   0.02968  -0.0160   0.0045   1.0000
  14.000   1.4430   0.03758   0.03209  -0.0153   0.0044   1.0000
  14.250   1.4424   0.04016   0.03481  -0.0149   0.0043   1.0000
  14.500   1.4400   0.04309   0.03787  -0.0149   0.0042   1.0000
  14.750   1.4366   0.04632   0.04124  -0.0153   0.0041   1.0000
  15.000   1.4300   0.05018   0.04525  -0.0162   0.0040   1.0000
  15.250   1.4224   0.05440   0.04961  -0.0175   0.0040   1.0000
  15.500   1.4114   0.05940   0.05476  -0.0194   0.0039   1.0000
  15.750   1.3993   0.06486   0.06038  -0.0219   0.0039   1.0000
  16.000   1.3835   0.07131   0.06699  -0.0250   0.0038   1.0000
  16.250   1.3667   0.07831   0.07416  -0.0287   0.0038   1.0000
  16.500   1.3484   0.08598   0.08198  -0.0329   0.0038   1.0000
  16.750   1.3256   0.09483   0.09101  -0.0378   0.0038   1.0000
  17.000   1.3027   0.10405   0.10040  -0.0429   0.0039   1.0000
  17.250   1.2785   0.11375   0.11026  -0.0484   0.0039   1.0000
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