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MB253515 15.0% smoothed (mb253515sm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MB253515 15.0% smoothed (mb253515sm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.78 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mb253515sm-il-1000000-n5.txt
Download as CSV file: xf-mb253515sm-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MB253515 15.0% smoothed                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.8828   0.09441   0.09221  -0.0464   1.0000   0.0049
 -17.500  -0.9460   0.07864   0.07619  -0.0555   1.0000   0.0048
 -17.250  -0.9922   0.06686   0.06417  -0.0628   1.0000   0.0047
 -17.000  -1.0097   0.06049   0.05766  -0.0666   1.0000   0.0048
 -16.750  -1.0298   0.05413   0.05114  -0.0703   1.0000   0.0047
 -16.500  -1.0437   0.04909   0.04595  -0.0728   1.0000   0.0047
 -16.250  -1.0542   0.04485   0.04157  -0.0746   1.0000   0.0048
 -16.000  -1.0551   0.04200   0.03865  -0.0755   1.0000   0.0049
 -15.750  -1.0623   0.03866   0.03517  -0.0762   1.0000   0.0050
 -15.500  -1.0650   0.03599   0.03239  -0.0764   1.0000   0.0050
 -15.250  -1.0656   0.03372   0.03001  -0.0761   1.0000   0.0051
 -15.000  -1.0634   0.03184   0.02802  -0.0755   1.0000   0.0052
 -14.750  -1.0607   0.03012   0.02620  -0.0746   1.0000   0.0053
 -14.500  -1.0574   0.02856   0.02455  -0.0733   1.0000   0.0053
 -14.250  -1.0509   0.02734   0.02325  -0.0720   1.0000   0.0055
 -14.000  -1.0464   0.02607   0.02189  -0.0703   1.0000   0.0056
 -13.750  -1.0405   0.02498   0.02071  -0.0684   1.0000   0.0057
 -13.500  -1.0360   0.02392   0.01956  -0.0660   1.0000   0.0058
 -13.250  -1.0288   0.02313   0.01869  -0.0637   1.0000   0.0059
 -13.000  -1.0191   0.02213   0.01760  -0.0619   0.9954   0.0059
 -12.750  -0.9989   0.02107   0.01645  -0.0621   0.9791   0.0064
 -12.500  -0.9634   0.02002   0.01531  -0.0652   0.9659   0.0066
 -12.250  -0.9194   0.01898   0.01419  -0.0701   0.9541   0.0071
 -12.000  -0.8735   0.01801   0.01311  -0.0752   0.9374   0.0074
 -11.750  -0.8389   0.01734   0.01228  -0.0777   0.9104   0.0079
 -11.500  -0.8229   0.01686   0.01163  -0.0761   0.8843   0.0081
 -11.250  -0.8093   0.01649   0.01113  -0.0738   0.8645   0.0083
 -11.000  -0.7969   0.01607   0.01059  -0.0712   0.8485   0.0086
 -10.750  -0.7839   0.01568   0.01011  -0.0688   0.8342   0.0092
 -10.500  -0.7672   0.01535   0.00971  -0.0670   0.8225   0.0097
 -10.250  -0.7495   0.01501   0.00929  -0.0654   0.8117   0.0102
 -10.000  -0.7304   0.01469   0.00891  -0.0640   0.8016   0.0109
  -9.750  -0.7112   0.01436   0.00849  -0.0626   0.7923   0.0114
  -9.500  -0.6913   0.01406   0.00812  -0.0614   0.7835   0.0121
  -9.250  -0.6691   0.01384   0.00789  -0.0605   0.7755   0.0131
  -8.750  -0.6249   0.01339   0.00735  -0.0588   0.7601   0.0145
  -8.500  -0.6022   0.01320   0.00709  -0.0579   0.7527   0.0153
  -8.250  -0.5790   0.01299   0.00683  -0.0573   0.7462   0.0158
  -8.000  -0.5570   0.01271   0.00651  -0.0563   0.7393   0.0167
  -7.750  -0.5326   0.01257   0.00635  -0.0558   0.7329   0.0175
  -7.500  -0.5086   0.01240   0.00615  -0.0553   0.7263   0.0183
  -7.250  -0.4845   0.01224   0.00595  -0.0547   0.7207   0.0191
  -7.000  -0.4605   0.01203   0.00570  -0.0541   0.7147   0.0198
  -6.750  -0.4361   0.01189   0.00550  -0.0536   0.7086   0.0204
  -6.500  -0.4112   0.01174   0.00531  -0.0531   0.7032   0.0209
  -6.250  -0.3860   0.01161   0.00513  -0.0527   0.6977   0.0212
  -5.750  -0.3412   0.01092   0.00435  -0.0509   0.6871   0.0230
  -5.500  -0.3168   0.01072   0.00412  -0.0504   0.6815   0.0238
  -5.250  -0.2923   0.01055   0.00390  -0.0499   0.6766   0.0245
  -5.000  -0.2671   0.01036   0.00368  -0.0494   0.6716   0.0252
  -4.750  -0.2421   0.01019   0.00347  -0.0490   0.6662   0.0258
  -4.500  -0.2171   0.01004   0.00327  -0.0485   0.6615   0.0265
  -4.250  -0.1913   0.00989   0.00310  -0.0482   0.6568   0.0271
  -4.000  -0.1658   0.00974   0.00291  -0.0478   0.6517   0.0274
  -3.750  -0.1404   0.00963   0.00275  -0.0474   0.6469   0.0277
  -3.500  -0.1144   0.00950   0.00259  -0.0471   0.6415   0.0280
  -3.250  -0.0890   0.00938   0.00242  -0.0467   0.6340   0.0285
  -3.000  -0.0635   0.00926   0.00226  -0.0463   0.6252   0.0295
  -2.750  -0.0382   0.00917   0.00212  -0.0459   0.6162   0.0311
  -2.500  -0.0122   0.00906   0.00201  -0.0456   0.6093   0.0333
  -2.250   0.0137   0.00899   0.00191  -0.0453   0.6033   0.0358
  -2.000   0.0398   0.00888   0.00182  -0.0450   0.5988   0.0434
  -1.750   0.0630   0.00856   0.00167  -0.0443   0.5930   0.1036
  -1.250   0.1023   0.00749   0.00138  -0.0417   0.5824   0.3388
  -1.000   0.1244   0.00716   0.00130  -0.0407   0.5770   0.4169
  -0.750   0.1480   0.00697   0.00126  -0.0400   0.5716   0.4695
  -0.500   0.1722   0.00679   0.00123  -0.0394   0.5652   0.5187
  -0.250   0.1962   0.00667   0.00121  -0.0387   0.5590   0.5618
   0.000   0.2210   0.00657   0.00121  -0.0382   0.5534   0.5990
   0.250   0.2456   0.00649   0.00122  -0.0376   0.5467   0.6339
   0.500   0.2700   0.00642   0.00123  -0.0370   0.5404   0.6680
   0.750   0.2944   0.00637   0.00126  -0.0363   0.5324   0.7018
   1.000   0.3198   0.00637   0.00129  -0.0359   0.5255   0.7199
   1.250   0.3461   0.00640   0.00132  -0.0356   0.5177   0.7322
   1.500   0.3717   0.00643   0.00136  -0.0353   0.5094   0.7447
   1.750   0.3972   0.00648   0.00140  -0.0349   0.4996   0.7568
   2.000   0.4230   0.00651   0.00145  -0.0345   0.4906   0.7689
   2.250   0.4484   0.00657   0.00151  -0.0341   0.4812   0.7806
   2.500   0.4733   0.00665   0.00158  -0.0337   0.4694   0.7926
   2.750   0.4980   0.00672   0.00165  -0.0331   0.4570   0.8057
   3.000   0.5223   0.00680   0.00173  -0.0325   0.4443   0.8197
   3.250   0.5466   0.00689   0.00183  -0.0319   0.4322   0.8331
   3.500   0.5707   0.00700   0.00193  -0.0312   0.4191   0.8452
   3.750   0.5944   0.00714   0.00204  -0.0306   0.4043   0.8568
   4.000   0.6182   0.00726   0.00217  -0.0299   0.3919   0.8690
   4.250   0.6420   0.00739   0.00230  -0.0292   0.3803   0.8812
   4.500   0.6667   0.00751   0.00243  -0.0287   0.3699   0.8938
   4.750   0.6919   0.00765   0.00258  -0.0284   0.3599   0.9070
   5.250   0.7480   0.00796   0.00291  -0.0290   0.3416   0.9332
   5.500   0.7794   0.00822   0.00314  -0.0302   0.3258   0.9446
   5.750   0.8134   0.00851   0.00338  -0.0320   0.3096   0.9527
   6.000   0.8458   0.00879   0.00361  -0.0334   0.2946   0.9608
   6.250   0.8807   0.00910   0.00387  -0.0355   0.2786   0.9653
   6.500   0.9119   0.00949   0.00416  -0.0368   0.2538   0.9707
   6.750   0.9390   0.01006   0.00454  -0.0374   0.2199   0.9763
   7.000   0.9595   0.01084   0.00508  -0.0368   0.1729   0.9843
   7.250   0.9642   0.01297   0.00654  -0.0343   0.0494   0.9953
   7.500   0.9899   0.01363   0.00711  -0.0348   0.0286   0.9997
   7.750   0.9967   0.01397   0.00742  -0.0311   0.0223   1.0000
   8.000   1.0029   0.01432   0.00776  -0.0272   0.0177   1.0000
   8.250   1.0122   0.01469   0.00813  -0.0241   0.0150   1.0000
   8.500   1.0230   0.01511   0.00855  -0.0214   0.0128   1.0000
   8.750   1.0359   0.01552   0.00899  -0.0192   0.0119   1.0000
   9.000   1.0483   0.01601   0.00950  -0.0170   0.0109   1.0000
   9.250   1.0606   0.01655   0.01006  -0.0149   0.0100   1.0000
   9.500   1.0723   0.01718   0.01072  -0.0129   0.0092   1.0000
   9.750   1.0854   0.01778   0.01136  -0.0112   0.0087   1.0000
  10.000   1.0988   0.01842   0.01203  -0.0097   0.0083   1.0000
  10.250   1.1116   0.01913   0.01278  -0.0081   0.0080   1.0000
  10.500   1.1236   0.01992   0.01362  -0.0067   0.0077   1.0000
  10.750   1.1361   0.02073   0.01446  -0.0053   0.0072   1.0000
  11.000   1.1467   0.02171   0.01548  -0.0039   0.0069   1.0000
  11.250   1.1556   0.02284   0.01666  -0.0025   0.0064   1.0000
  11.500   1.1641   0.02407   0.01794  -0.0012   0.0062   1.0000
  11.750   1.1765   0.02504   0.01895  -0.0003   0.0061   1.0000
  12.000   1.1865   0.02623   0.02019   0.0007   0.0059   1.0000
  12.250   1.1957   0.02752   0.02154   0.0017   0.0057   1.0000
  12.500   1.2038   0.02893   0.02302   0.0027   0.0056   1.0000
  12.750   1.2114   0.03042   0.02457   0.0035   0.0054   1.0000
  13.000   1.2190   0.03194   0.02615   0.0043   0.0053   1.0000
  13.250   1.2262   0.03354   0.02779   0.0050   0.0050   1.0000
  13.500   1.2312   0.03536   0.02968   0.0057   0.0050   1.0000
  13.750   1.2363   0.03723   0.03160   0.0063   0.0047   1.0000
  14.000   1.2408   0.03922   0.03364   0.0068   0.0046   1.0000
  14.250   1.2427   0.04152   0.03602   0.0072   0.0045   1.0000
  14.500   1.2432   0.04403   0.03860   0.0076   0.0045   1.0000
  14.750   1.2395   0.04705   0.04172   0.0079   0.0043   1.0000
  15.000   1.2430   0.04940   0.04415   0.0080   0.0042   1.0000
  15.250   1.2432   0.05215   0.04698   0.0080   0.0042   1.0000
  15.500   1.2416   0.05517   0.05008   0.0079   0.0041   1.0000
  15.750   1.2445   0.05774   0.05272   0.0077   0.0041   1.0000
  16.000   1.2400   0.06125   0.05632   0.0074   0.0041   1.0000
  16.250   1.2409   0.06413   0.05929   0.0070   0.0040   1.0000
  16.500   1.2390   0.06743   0.06266   0.0066   0.0039   1.0000
  16.750   1.2415   0.07021   0.06551   0.0060   0.0038   1.0000
  17.000   1.2375   0.07390   0.06929   0.0054   0.0038   1.0000
  17.250   1.2287   0.07825   0.07374   0.0045   0.0038   1.0000
  17.500   1.2316   0.08110   0.07665   0.0038   0.0036   1.0000
  17.750   1.2287   0.08478   0.08041   0.0029   0.0036   1.0000
  18.000   1.2191   0.08942   0.08515   0.0017   0.0036   1.0000
  18.250   1.2159   0.09324   0.08905   0.0006   0.0035   1.0000
  18.500   1.2193   0.09615   0.09202  -0.0004   0.0034   1.0000
  18.750   1.2114   0.10065   0.09661  -0.0017   0.0034   1.0000
  19.000   1.2064   0.10481   0.10085  -0.0030   0.0033   1.0000
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