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S3016-095-87 (s3016-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S3016-095-87 (s3016-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.28 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s3016-il-1000000-n5.txt
Download as CSV file: xf-s3016-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S3016-095-87                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.9406   0.03962   0.03756  -0.0484   1.0000   0.0028
 -12.000  -0.9651   0.03537   0.03306  -0.0469   1.0000   0.0028
 -11.750  -0.9706   0.03181   0.02922  -0.0459   1.0000   0.0028
 -11.500  -0.9656   0.02915   0.02633  -0.0451   1.0000   0.0029
 -11.250  -0.9550   0.02699   0.02396  -0.0442   1.0000   0.0029
 -11.000  -0.9411   0.02513   0.02189  -0.0435   1.0000   0.0030
 -10.750  -0.9236   0.02372   0.02031  -0.0428   1.0000   0.0031
 -10.500  -0.9057   0.02227   0.01868  -0.0422   1.0000   0.0031
 -10.250  -0.8794   0.02105   0.01730  -0.0430   0.9777   0.0032
 -10.000  -0.8542   0.01992   0.01601  -0.0433   0.9597   0.0034
  -9.750  -0.8332   0.01907   0.01500  -0.0425   0.9437   0.0035
  -9.500  -0.8133   0.01814   0.01389  -0.0414   0.9306   0.0036
  -9.250  -0.7918   0.01736   0.01296  -0.0406   0.9199   0.0038
  -9.000  -0.7698   0.01658   0.01203  -0.0398   0.9106   0.0039
  -8.750  -0.7470   0.01588   0.01117  -0.0390   0.9018   0.0040
  -8.500  -0.7237   0.01513   0.01027  -0.0384   0.8940   0.0041
  -8.000  -0.6750   0.01398   0.00888  -0.0373   0.8795   0.0044
  -7.500  -0.6261   0.01264   0.00729  -0.0363   0.8659   0.0049
  -7.250  -0.6005   0.01222   0.00679  -0.0359   0.8593   0.0053
  -7.000  -0.5743   0.01187   0.00638  -0.0356   0.8532   0.0057
  -6.750  -0.5480   0.01153   0.00597  -0.0353   0.8468   0.0061
  -6.500  -0.5215   0.01123   0.00562  -0.0351   0.8411   0.0066
  -6.250  -0.4946   0.01097   0.00531  -0.0349   0.8348   0.0071
  -6.000  -0.4684   0.01059   0.00486  -0.0345   0.8291   0.0078
  -5.750  -0.4413   0.01034   0.00460  -0.0344   0.8230   0.0086
  -5.500  -0.4142   0.01013   0.00434  -0.0342   0.8168   0.0095
  -5.250  -0.3869   0.00991   0.00407  -0.0340   0.8108   0.0104
  -5.000  -0.3596   0.00973   0.00384  -0.0339   0.8042   0.0110
  -4.750  -0.3324   0.00948   0.00353  -0.0337   0.7980   0.0117
  -4.500  -0.3054   0.00918   0.00320  -0.0335   0.7912   0.0130
  -4.250  -0.2780   0.00900   0.00298  -0.0333   0.7848   0.0142
  -4.000  -0.2504   0.00881   0.00275  -0.0332   0.7777   0.0151
  -3.750  -0.2229   0.00865   0.00253  -0.0331   0.7708   0.0159
  -3.500  -0.1951   0.00850   0.00235  -0.0330   0.7629   0.0165
  -3.250  -0.1675   0.00833   0.00213  -0.0328   0.7552   0.0171
  -3.000  -0.1399   0.00815   0.00188  -0.0326   0.7462   0.0191
  -2.750  -0.1122   0.00799   0.00170  -0.0325   0.7370   0.0214
  -2.500  -0.0845   0.00788   0.00155  -0.0324   0.7271   0.0246
  -2.000  -0.0300   0.00746   0.00126  -0.0321   0.7031   0.0766
  -1.750  -0.0031   0.00726   0.00114  -0.0319   0.6867   0.1177
  -1.500   0.0241   0.00712   0.00105  -0.0318   0.6690   0.1504
  -1.250   0.0514   0.00700   0.00097  -0.0317   0.6530   0.1845
  -1.000   0.0785   0.00684   0.00091  -0.0316   0.6368   0.2318
  -0.750   0.1051   0.00665   0.00086  -0.0314   0.6201   0.2962
  -0.500   0.1314   0.00641   0.00083  -0.0312   0.6030   0.3809
  -0.250   0.1577   0.00620   0.00081  -0.0310   0.5852   0.4592
   0.000   0.1847   0.00614   0.00080  -0.0308   0.5661   0.5040
   0.250   0.2115   0.00607   0.00081  -0.0306   0.5475   0.5540
   0.500   0.2380   0.00599   0.00083  -0.0304   0.5290   0.6106
   0.750   0.2643   0.00593   0.00085  -0.0300   0.5092   0.6634
   1.000   0.2903   0.00589   0.00089  -0.0296   0.4888   0.7144
   1.250   0.3160   0.00584   0.00094  -0.0291   0.4681   0.7673
   1.500   0.3408   0.00580   0.00100  -0.0284   0.4470   0.8254
   1.750   0.3651   0.00575   0.00107  -0.0275   0.4243   0.8897
   2.000   0.4016   0.00584   0.00118  -0.0293   0.3986   0.9494
   2.250   0.4442   0.00605   0.00128  -0.0326   0.3686   0.9741
   2.500   0.4790   0.00625   0.00137  -0.0342   0.3437   0.9855
   2.750   0.5121   0.00647   0.00146  -0.0355   0.3198   0.9934
   3.250   0.5797   0.00687   0.00167  -0.0383   0.2758   1.0000
   3.500   0.6049   0.00706   0.00179  -0.0379   0.2588   1.0000
   3.750   0.6302   0.00724   0.00192  -0.0374   0.2445   1.0000
   4.000   0.6554   0.00744   0.00205  -0.0369   0.2286   1.0000
   4.250   0.6806   0.00763   0.00218  -0.0364   0.2153   1.0000
   4.500   0.7057   0.00784   0.00233  -0.0359   0.2004   1.0000
   4.750   0.7310   0.00805   0.00250  -0.0355   0.1882   1.0000
   5.000   0.7560   0.00827   0.00267  -0.0350   0.1744   1.0000
   5.250   0.7810   0.00849   0.00284  -0.0345   0.1636   1.0000
   5.500   0.8060   0.00872   0.00302  -0.0340   0.1525   1.0000
   5.750   0.8307   0.00897   0.00323  -0.0335   0.1399   1.0000
   6.000   0.8557   0.00920   0.00345  -0.0330   0.1298   1.0000
   6.250   0.8806   0.00944   0.00366  -0.0325   0.1210   1.0000
   6.500   0.9051   0.00973   0.00390  -0.0320   0.1101   1.0000
   6.750   0.9294   0.01005   0.00417  -0.0315   0.0977   1.0000
   7.000   0.9531   0.01042   0.00447  -0.0309   0.0824   1.0000
   7.250   0.9764   0.01085   0.00482  -0.0303   0.0670   1.0000
   7.500   1.0004   0.01119   0.00513  -0.0297   0.0585   1.0000
   7.750   1.0239   0.01157   0.00548  -0.0291   0.0501   1.0000
   8.000   1.0471   0.01199   0.00586  -0.0285   0.0411   1.0000
   8.250   1.0697   0.01247   0.00627  -0.0278   0.0314   1.0000
   8.500   1.0923   0.01294   0.00671  -0.0271   0.0238   1.0000
   8.750   1.1142   0.01347   0.00722  -0.0263   0.0168   1.0000
   9.000   1.1353   0.01406   0.00777  -0.0255   0.0104   1.0000
   9.250   1.1563   0.01464   0.00835  -0.0246   0.0062   1.0000
   9.500   1.1775   0.01520   0.00893  -0.0237   0.0043   1.0000
   9.750   1.1989   0.01569   0.00946  -0.0229   0.0038   1.0000
  10.000   1.2194   0.01625   0.01007  -0.0219   0.0033   1.0000
  10.250   1.2392   0.01685   0.01073  -0.0209   0.0029   1.0000
  10.500   1.2586   0.01745   0.01141  -0.0198   0.0027   1.0000
  10.750   1.2777   0.01804   0.01206  -0.0187   0.0026   1.0000
  11.000   1.2962   0.01864   0.01273  -0.0176   0.0025   1.0000
  11.250   1.3135   0.01929   0.01344  -0.0163   0.0023   1.0000
  11.500   1.3294   0.01998   0.01421  -0.0148   0.0022   1.0000
  11.750   1.3435   0.02070   0.01500  -0.0131   0.0021   1.0000
  12.000   1.3538   0.02144   0.01582  -0.0107   0.0020   1.0000
  12.250   1.3623   0.02228   0.01673  -0.0083   0.0019   1.0000
  12.500   1.3706   0.02319   0.01773  -0.0061   0.0017   1.0000
  12.750   1.3789   0.02418   0.01879  -0.0041   0.0017   1.0000
  13.000   1.3846   0.02541   0.02012  -0.0021   0.0017   1.0000
  13.250   1.3857   0.02706   0.02190   0.0000   0.0016   1.0000
  13.500   1.3902   0.02855   0.02349   0.0015   0.0015   1.0000
  13.750   1.3864   0.03084   0.02592   0.0032   0.0014   1.0000
  14.000   1.3854   0.03303   0.02823   0.0043   0.0014   1.0000
  14.250   1.3842   0.03540   0.03072   0.0051   0.0014   1.0000
  14.500   1.3813   0.03811   0.03355   0.0055   0.0014   1.0000
  14.750   1.3807   0.04075   0.03630   0.0055   0.0014   1.0000
  15.000   1.3774   0.04387   0.03953   0.0052   0.0014   1.0000
  15.250   1.3724   0.04741   0.04319   0.0045   0.0014   1.0000
  15.500   1.3642   0.05158   0.04749   0.0032   0.0014   1.0000
  15.750   1.3540   0.05633   0.05238   0.0014   0.0014   1.0000
  16.000   1.3381   0.06225   0.05845  -0.0012   0.0014   1.0000
  16.250   1.3245   0.06817   0.06450  -0.0040   0.0014   1.0000
  16.500   1.3077   0.07492   0.07139  -0.0074   0.0013   1.0000
  16.750   1.2807   0.08381   0.08046  -0.0120   0.0014   1.0000
  17.000   1.2645   0.09095   0.08771  -0.0157   0.0014   1.0000
  17.250   1.2340   0.10109   0.09801  -0.0210   0.0014   1.0000
  17.500   1.2137   0.10945   0.10649  -0.0254   0.0014   1.0000
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