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S1016 (s1016-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: S1016 (s1016-il)
Reynolds number: 100,000
Max Cl/Cd: 23.54 at α=10.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1016-il-100000-n5.txt
Download as CSV file: xf-s1016-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1016                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.8259   0.10432   0.09836  -0.0542   1.0000   0.0596
 -17.500  -0.8761   0.09169   0.08541  -0.0614   1.0000   0.0599
 -17.250  -0.9044   0.08366   0.07710  -0.0656   1.0000   0.0607
 -17.000  -0.9269   0.07701   0.07016  -0.0688   1.0000   0.0617
 -16.750  -0.9408   0.07192   0.06484  -0.0709   1.0000   0.0628
 -16.500  -0.9376   0.06939   0.06234  -0.0718   1.0000   0.0642
 -16.250  -0.9393   0.06629   0.05917  -0.0728   1.0000   0.0657
 -16.000  -0.9426   0.06306   0.05581  -0.0736   1.0000   0.0673
 -15.750  -0.9470   0.05987   0.05244  -0.0743   1.0000   0.0691
 -15.500  -0.9515   0.05676   0.04906  -0.0746   1.0000   0.0710
 -15.250  -0.9497   0.05447   0.04670  -0.0746   1.0000   0.0728
 -15.000  -0.9462   0.05258   0.04479  -0.0745   1.0000   0.0747
 -14.750  -0.9440   0.05067   0.04279  -0.0741   1.0000   0.0769
 -14.500  -0.9424   0.04881   0.04078  -0.0734   1.0000   0.0793
 -14.250  -0.9424   0.04705   0.03880  -0.0722   1.0000   0.0817
 -14.000  -0.9377   0.04570   0.03748  -0.0712   0.9969   0.0839
 -13.750  -0.9267   0.04422   0.03592  -0.0715   0.9857   0.0867
 -13.500  -0.9140   0.04271   0.03426  -0.0719   0.9800   0.0902
 -13.250  -0.9001   0.04123   0.03260  -0.0723   0.9752   0.0938
 -13.000  -0.8851   0.03996   0.03131  -0.0727   0.9715   0.0971
 -12.750  -0.8688   0.03871   0.02996  -0.0731   0.9686   0.1012
 -12.500  -0.8528   0.03755   0.02859  -0.0732   0.9655   0.1058
 -12.250  -0.8374   0.03648   0.02755  -0.0731   0.9625   0.1096
 -12.000  -0.8208   0.03548   0.02646  -0.0731   0.9598   0.1143
 -11.750  -0.8024   0.03451   0.02536  -0.0732   0.9575   0.1197
 -11.500  -0.7850   0.03358   0.02442  -0.0732   0.9554   0.1245
 -11.250  -0.7668   0.03276   0.02349  -0.0731   0.9533   0.1304
 -11.000  -0.7509   0.03199   0.02270  -0.0725   0.9508   0.1358
 -10.750  -0.7353   0.03128   0.02196  -0.0718   0.9483   0.1418
 -10.500  -0.7169   0.03063   0.02121  -0.0714   0.9462   0.1485
 -10.250  -0.7005   0.02992   0.02053  -0.0708   0.9438   0.1552
 -10.000  -0.6803   0.02933   0.01983  -0.0706   0.9418   0.1633
  -9.750  -0.6624   0.02866   0.01921  -0.0701   0.9399   0.1709
  -9.500  -0.6459   0.02820   0.01867  -0.0691   0.9379   0.1797
  -9.250  -0.6332   0.02770   0.01823  -0.0676   0.9356   0.1880
  -9.000  -0.6179   0.02729   0.01780  -0.0663   0.9334   0.1976
  -8.750  -0.6035   0.02686   0.01739  -0.0650   0.9314   0.2079
  -8.500  -0.5880   0.02643   0.01699  -0.0638   0.9295   0.2191
  -8.250  -0.5704   0.02602   0.01658  -0.0628   0.9276   0.2319
  -8.000  -0.5521   0.02559   0.01619  -0.0620   0.9258   0.2467
  -7.750  -0.5339   0.02519   0.01582  -0.0612   0.9242   0.2627
  -7.500  -0.5262   0.02497   0.01568  -0.0584   0.9219   0.2778
  -7.250  -0.5187   0.02476   0.01555  -0.0555   0.9194   0.2945
  -7.000  -0.5090   0.02453   0.01540  -0.0529   0.9166   0.3136
  -6.750  -0.4976   0.02426   0.01524  -0.0506   0.9140   0.3355
  -6.500  -0.4858   0.02401   0.01510  -0.0484   0.9120   0.3609
  -6.250  -0.4714   0.02376   0.01499  -0.0465   0.9102   0.3895
  -6.000  -0.4529   0.02351   0.01491  -0.0453   0.9085   0.4237
  -5.750  -0.4570   0.02360   0.01516  -0.0398   0.9045   0.4500
  -5.500  -0.4505   0.02365   0.01538  -0.0360   0.9014   0.4829
  -5.250  -0.4286   0.02380   0.01575  -0.0346   0.8992   0.5242
  -5.000  -0.3876   0.02442   0.01659  -0.0360   0.8984   0.5659
  -4.750  -0.3471   0.02528   0.01755  -0.0371   0.8976   0.5983
  -4.500  -0.3095   0.02614   0.01845  -0.0378   0.8965   0.6215
  -4.250  -0.2783   0.02678   0.01906  -0.0378   0.8949   0.6407
  -4.000  -0.2495   0.02731   0.01956  -0.0376   0.8933   0.6577
  -3.750  -0.2405   0.02792   0.02016  -0.0339   0.8897   0.6723
  -3.500  -0.2423   0.02848   0.02071  -0.0284   0.8843   0.6861
  -3.000  -0.2104   0.02921   0.02135  -0.0240   0.8780   0.7143
  -2.750  -0.2145   0.02956   0.02168  -0.0183   0.8729   0.7286
  -2.500  -0.2364   0.02983   0.02195  -0.0093   0.8650   0.7434
  -2.000  -0.1713   0.03069   0.02271  -0.0105   0.8605   0.7610
  -1.750  -0.2092   0.03085   0.02287   0.0015   0.8499   0.7757
  -1.500  -0.1572   0.03153   0.02353  -0.0024   0.8483   0.7797
  -1.250  -0.1438   0.03150   0.02346   0.0002   0.8443   0.7919
  -1.000  -0.0855   0.03196   0.02389  -0.0051   0.8435   0.7945
  -0.750  -0.1221   0.03201   0.02395   0.0067   0.8315   0.8084
  -0.500  -0.0677   0.03235   0.02427   0.0021   0.8296   0.8109
  -0.250  -0.0104   0.03250   0.02442  -0.0032   0.8280   0.8132
   0.000  -0.0424   0.03245   0.02437   0.0077   0.8162   0.8263
   0.250   0.0105   0.03250   0.02442   0.0032   0.8132   0.8280
   0.500   0.0679   0.03234   0.02427  -0.0021   0.8109   0.8296
   0.750   0.1211   0.03203   0.02397  -0.0065   0.8083   0.8316
   1.000   0.0854   0.03196   0.02389   0.0051   0.7945   0.8435
   1.250   0.1442   0.03149   0.02345  -0.0002   0.7919   0.8443
   1.500   0.1572   0.03152   0.02352   0.0024   0.7797   0.8483
   1.750   0.1346   0.03122   0.02321   0.0117   0.7677   0.8581
   2.000   0.1710   0.03069   0.02271   0.0105   0.7610   0.8605
   2.250   0.1898   0.03051   0.02257   0.0122   0.7490   0.8636
   2.500   0.2362   0.02983   0.02195   0.0093   0.7434   0.8650
   3.000   0.2105   0.02920   0.02134   0.0240   0.7143   0.8780
   3.250   0.2291   0.02888   0.02107   0.0257   0.7003   0.8808
   3.500   0.2423   0.02847   0.02070   0.0284   0.6861   0.8844
   3.750   0.2401   0.02791   0.02014   0.0340   0.6721   0.8898
   4.000   0.2497   0.02730   0.01955   0.0375   0.6577   0.8934
   4.250   0.2784   0.02677   0.01906   0.0377   0.6411   0.8949
   4.500   0.3095   0.02614   0.01845   0.0378   0.6219   0.8966
   4.750   0.3472   0.02527   0.01754   0.0370   0.5984   0.8977
   5.000   0.3876   0.02441   0.01658   0.0360   0.5660   0.8984
   5.250   0.4285   0.02379   0.01574   0.0347   0.5240   0.8992
   5.500   0.4505   0.02364   0.01537   0.0360   0.4830   0.9014
   5.750   0.4571   0.02359   0.01515   0.0397   0.4504   0.9046
   6.000   0.4532   0.02350   0.01491   0.0452   0.4238   0.9085
   6.250   0.4716   0.02375   0.01498   0.0465   0.3895   0.9102
   6.500   0.4859   0.02400   0.01509   0.0484   0.3608   0.9120
   6.750   0.4979   0.02425   0.01522   0.0506   0.3357   0.9140
   7.000   0.5093   0.02452   0.01539   0.0529   0.3137   0.9166
   7.250   0.5188   0.02476   0.01554   0.0555   0.2943   0.9194
   7.500   0.5264   0.02496   0.01567   0.0583   0.2778   0.9219
   7.750   0.5343   0.02518   0.01581   0.0611   0.2627   0.9243
   8.000   0.5524   0.02559   0.01618   0.0620   0.2465   0.9258
   8.250   0.5707   0.02601   0.01657   0.0628   0.2317   0.9277
   8.500   0.5883   0.02642   0.01697   0.0637   0.2189   0.9296
   8.750   0.6039   0.02685   0.01737   0.0649   0.2079   0.9315
   9.000   0.6182   0.02728   0.01778   0.0663   0.1974   0.9335
   9.250   0.6336   0.02769   0.01822   0.0675   0.1879   0.9356
   9.500   0.6465   0.02819   0.01866   0.0691   0.1798   0.9379
   9.750   0.6630   0.02865   0.01920   0.0700   0.1709   0.9400
  10.000   0.6808   0.02932   0.01981   0.0705   0.1632   0.9418
  10.250   0.7010   0.02991   0.02051   0.0707   0.1550   0.9439
  10.500   0.7175   0.03063   0.02119   0.0713   0.1484   0.9462
  10.750   0.7361   0.03127   0.02195   0.0717   0.1418   0.9484
  11.000   0.7515   0.03199   0.02269   0.0724   0.1355   0.9509
  11.250   0.7675   0.03275   0.02349   0.0730   0.1301   0.9534
  11.500   0.7859   0.03357   0.02441   0.0731   0.1243   0.9555
  11.750   0.8032   0.03452   0.02535   0.0730   0.1194   0.9576
  12.000   0.8220   0.03547   0.02645   0.0729   0.1142   0.9599
  12.250   0.8385   0.03647   0.02753   0.0730   0.1094   0.9626
  12.500   0.8539   0.03754   0.02857   0.0730   0.1056   0.9656
  12.750   0.8702   0.03870   0.02995   0.0729   0.1011   0.9687
  13.000   0.8864   0.03995   0.03130   0.0724   0.0970   0.9717
  13.250   0.9017   0.04122   0.03257   0.0720   0.0937   0.9755
  13.500   0.9156   0.04269   0.03424   0.0717   0.0901   0.9803
  13.750   0.9282   0.04420   0.03590   0.0712   0.0865   0.9862
  14.000   0.9395   0.04570   0.03747   0.0709   0.0838   0.9980
  14.250   0.9436   0.04701   0.03875   0.0721   0.0817   1.0000
  14.500   0.9435   0.04878   0.04076   0.0732   0.0791   1.0000
  14.750   0.9453   0.05064   0.04276   0.0739   0.0768   1.0000
  15.000   0.9478   0.05254   0.04474   0.0743   0.0746   1.0000
  15.250   0.9515   0.05442   0.04664   0.0744   0.0728   1.0000
  15.500   0.9532   0.05673   0.04903   0.0743   0.0709   1.0000
  15.750   0.9488   0.05983   0.05239   0.0740   0.0690   1.0000
  16.000   0.9447   0.06302   0.05576   0.0734   0.0672   1.0000
  16.250   0.9413   0.06622   0.05908   0.0725   0.0656   1.0000
  16.500   0.9400   0.06930   0.06224   0.0715   0.0642   1.0000
  16.750   0.9435   0.07179   0.06470   0.0706   0.0627   1.0000
  17.000   0.9281   0.07708   0.07025   0.0685   0.0616   1.0000
  17.250   0.9062   0.08368   0.07713   0.0653   0.0606   1.0000
  17.500   0.8778   0.09174   0.08545   0.0611   0.0598   1.0000
  17.750   0.8278   0.10438   0.09842   0.0538   0.0596   1.0000
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