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S1014 (s1014-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: S1014 (s1014-il)
Reynolds number: 100,000
Max Cl/Cd: 23.23 at α=10.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1014-il-100000-n5.txt
Download as CSV file: xf-s1014-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1014                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.8655   0.09391   0.08792  -0.0539   1.0000   0.0469
 -16.750  -0.8816   0.08760   0.08151  -0.0575   1.0000   0.0475
 -16.500  -0.8909   0.08269   0.07651  -0.0600   1.0000   0.0482
 -16.250  -0.9040   0.07743   0.07110  -0.0625   1.0000   0.0487
 -16.000  -0.9143   0.07291   0.06645  -0.0645   1.0000   0.0495
 -15.750  -0.9249   0.06862   0.06199  -0.0660   1.0000   0.0503
 -15.500  -0.9348   0.06459   0.05777  -0.0670   1.0000   0.0513
 -15.250  -0.9434   0.06090   0.05384  -0.0676   1.0000   0.0523
 -15.000  -0.9507   0.05747   0.05015  -0.0678   1.0000   0.0535
 -14.750  -0.9562   0.05431   0.04668  -0.0676   1.0000   0.0548
 -14.500  -0.9509   0.05236   0.04473  -0.0676   1.0000   0.0562
 -14.250  -0.9457   0.05056   0.04290  -0.0674   1.0000   0.0578
 -14.000  -0.9409   0.04868   0.04091  -0.0670   1.0000   0.0594
 -13.750  -0.9368   0.04678   0.03882  -0.0665   1.0000   0.0615
 -13.500  -0.9293   0.04481   0.03653  -0.0665   0.9757   0.0639
 -13.250  -0.9131   0.04330   0.03500  -0.0673   0.9652   0.0660
 -13.000  -0.8980   0.04187   0.03349  -0.0680   0.9577   0.0687
 -12.750  -0.8823   0.04040   0.03182  -0.0683   0.9519   0.0719
 -12.500  -0.8657   0.03899   0.03020  -0.0685   0.9467   0.0751
 -12.250  -0.8491   0.03784   0.02903  -0.0687   0.9423   0.0780
 -12.000  -0.8325   0.03674   0.02781  -0.0686   0.9384   0.0815
 -11.750  -0.8154   0.03569   0.02653  -0.0683   0.9345   0.0855
 -11.500  -0.7985   0.03468   0.02555  -0.0680   0.9311   0.0890
 -11.250  -0.7811   0.03379   0.02458  -0.0677   0.9280   0.0931
 -11.000  -0.7620   0.03296   0.02354  -0.0674   0.9254   0.0981
 -10.750  -0.7447   0.03209   0.02271  -0.0670   0.9227   0.1022
 -10.500  -0.7271   0.03134   0.02190  -0.0665   0.9199   0.1076
 -10.250  -0.7079   0.03062   0.02110  -0.0660   0.9172   0.1132
 -10.000  -0.6907   0.02990   0.02037  -0.0654   0.9144   0.1186
  -9.750  -0.6710   0.02929   0.01964  -0.0649   0.9121   0.1255
  -9.500  -0.6535   0.02859   0.01900  -0.0642   0.9100   0.1319
  -9.250  -0.6340   0.02804   0.01836  -0.0637   0.9082   0.1400
  -9.000  -0.6168   0.02741   0.01779  -0.0629   0.9061   0.1477
  -8.750  -0.5978   0.02691   0.01725  -0.0623   0.9042   0.1574
  -8.500  -0.5805   0.02635   0.01674  -0.0615   0.9023   0.1673
  -8.250  -0.5628   0.02584   0.01626  -0.0606   0.9005   0.1788
  -8.000  -0.5449   0.02537   0.01581  -0.0598   0.8988   0.1923
  -7.750  -0.5269   0.02490   0.01539  -0.0589   0.8972   0.2077
  -7.500  -0.5093   0.02442   0.01499  -0.0580   0.8955   0.2266
  -7.250  -0.4921   0.02396   0.01463  -0.0569   0.8938   0.2488
  -7.000  -0.4769   0.02353   0.01433  -0.0555   0.8918   0.2749
  -6.750  -0.4631   0.02312   0.01410  -0.0539   0.8899   0.3069
  -6.500  -0.4509   0.02272   0.01392  -0.0520   0.8880   0.3459
  -6.250  -0.4400   0.02235   0.01380  -0.0498   0.8861   0.3915
  -6.000  -0.4273   0.02210   0.01388  -0.0474   0.8844   0.4482
  -5.750  -0.3948   0.02256   0.01476  -0.0471   0.8837   0.5186
  -5.500  -0.3416   0.02411   0.01653  -0.0489   0.8838   0.5742
  -5.250  -0.3068   0.02510   0.01754  -0.0489   0.8827   0.6039
  -5.000  -0.2808   0.02577   0.01817  -0.0479   0.8812   0.6256
  -4.750  -0.2610   0.02623   0.01855  -0.0464   0.8798   0.6443
  -4.500  -0.2464   0.02656   0.01881  -0.0442   0.8783   0.6627
  -4.250  -0.2393   0.02687   0.01907  -0.0410   0.8762   0.6797
  -3.750  -0.2252   0.02790   0.02003  -0.0338   0.8703   0.7065
  -3.500  -0.2175   0.02835   0.02044  -0.0303   0.8676   0.7189
  -3.250  -0.2135   0.02867   0.02071  -0.0261   0.8647   0.7320
  -3.000  -0.2142   0.02892   0.02091  -0.0212   0.8623   0.7458
  -2.750  -0.1565   0.02979   0.02173  -0.0255   0.8624   0.7503
  -2.500  -0.1815   0.03023   0.02217  -0.0164   0.8567   0.7636
  -2.250  -0.1266   0.03091   0.02282  -0.0206   0.8566   0.7681
  -2.000  -0.1426   0.03116   0.02306  -0.0129   0.8512   0.7804
  -1.750  -0.0968   0.03152   0.02338  -0.0160   0.8503   0.7837
  -1.500  -0.1007   0.03149   0.02331  -0.0106   0.8467   0.7950
  -1.250  -0.0576   0.03166   0.02345  -0.0133   0.8458   0.7975
  -0.750  -0.0690   0.03205   0.02384  -0.0019   0.8344   0.8129
  -0.500  -0.0308   0.03215   0.02393  -0.0039   0.8324   0.8150
  -0.250   0.0057   0.03217   0.02395  -0.0057   0.8306   0.8175
   0.000  -0.0402   0.03211   0.02389   0.0071   0.8205   0.8289
   0.250  -0.0057   0.03217   0.02395   0.0057   0.8175   0.8306
   0.500   0.0309   0.03214   0.02393   0.0039   0.8150   0.8324
   0.750   0.0688   0.03204   0.02384   0.0019   0.8129   0.8344
   1.250   0.0577   0.03165   0.02345   0.0133   0.7975   0.8458
   1.500   0.1005   0.03150   0.02332   0.0106   0.7949   0.8468
   1.750   0.0972   0.03152   0.02338   0.0159   0.7837   0.8503
   2.000   0.1426   0.03116   0.02306   0.0129   0.7804   0.8512
   2.250   0.1264   0.03091   0.02282   0.0206   0.7681   0.8566
   2.500   0.1809   0.03023   0.02218   0.0164   0.7637   0.8568
   2.750   0.1563   0.02980   0.02173   0.0255   0.7503   0.8624
   3.000   0.2144   0.02891   0.02090   0.0211   0.7458   0.8623
   3.250   0.2136   0.02866   0.02070   0.0261   0.7320   0.8647
   3.500   0.2173   0.02836   0.02045   0.0303   0.7190   0.8677
   3.750   0.2254   0.02790   0.02003   0.0338   0.7066   0.8703
   4.000   0.2556   0.02708   0.01927   0.0340   0.6981   0.8715
   4.250   0.2412   0.02684   0.01905   0.0407   0.6803   0.8761
   4.500   0.2465   0.02655   0.01881   0.0442   0.6627   0.8783
   4.750   0.2612   0.02623   0.01855   0.0464   0.6445   0.8798
   5.000   0.2810   0.02576   0.01815   0.0479   0.6255   0.8812
   5.250   0.3069   0.02509   0.01753   0.0488   0.6037   0.8828
   5.500   0.3420   0.02408   0.01651   0.0488   0.5740   0.8838
   5.750   0.3952   0.02255   0.01475   0.0470   0.5181   0.8837
   6.000   0.4274   0.02210   0.01388   0.0474   0.4479   0.8844
   6.250   0.4400   0.02235   0.01379   0.0497   0.3912   0.8861
   6.500   0.4511   0.02271   0.01391   0.0520   0.3459   0.8880
   6.750   0.4633   0.02312   0.01409   0.0539   0.3067   0.8899
   7.000   0.4771   0.02353   0.01432   0.0555   0.2748   0.8918
   7.250   0.4923   0.02395   0.01462   0.0569   0.2487   0.8938
   7.500   0.5095   0.02442   0.01499   0.0580   0.2261   0.8955
   7.750   0.5272   0.02489   0.01538   0.0589   0.2077   0.8972
   8.000   0.5451   0.02536   0.01580   0.0597   0.1922   0.8988
   8.250   0.5631   0.02583   0.01625   0.0606   0.1788   0.9005
   8.500   0.5809   0.02635   0.01673   0.0614   0.1673   0.9023
   8.750   0.5981   0.02690   0.01724   0.0622   0.1574   0.9042
   9.000   0.6172   0.02740   0.01778   0.0629   0.1477   0.9062
   9.250   0.6344   0.02803   0.01835   0.0636   0.1399   0.9082
   9.500   0.6539   0.02859   0.01899   0.0641   0.1318   0.9101
   9.750   0.6714   0.02928   0.01963   0.0648   0.1253   0.9121
  10.000   0.6912   0.02988   0.02036   0.0653   0.1186   0.9145
  10.250   0.7083   0.03061   0.02108   0.0659   0.1131   0.9172
  10.500   0.7276   0.03133   0.02190   0.0664   0.1075   0.9200
  10.750   0.7453   0.03208   0.02271   0.0669   0.1022   0.9228
  11.000   0.7624   0.03295   0.02354   0.0673   0.0979   0.9255
  11.250   0.7820   0.03379   0.02458   0.0676   0.0931   0.9280
  11.500   0.7990   0.03467   0.02554   0.0679   0.0889   0.9312
  11.750   0.8161   0.03568   0.02653   0.0682   0.0854   0.9346
  12.000   0.8333   0.03673   0.02781   0.0685   0.0813   0.9385
  12.250   0.8498   0.03782   0.02901   0.0686   0.0779   0.9425
  12.500   0.8666   0.03898   0.03019   0.0684   0.0750   0.9469
  12.750   0.8828   0.04039   0.03182   0.0682   0.0717   0.9521
  13.000   0.8990   0.04185   0.03347   0.0678   0.0686   0.9580
  13.250   0.9146   0.04329   0.03500   0.0671   0.0661   0.9656
  13.500   0.9302   0.04484   0.03657   0.0663   0.0638   0.9764
  13.750   0.9379   0.04677   0.03881   0.0663   0.0615   1.0000
  14.000   0.9422   0.04867   0.04089   0.0669   0.0594   1.0000
  14.250   0.9468   0.05053   0.04286   0.0672   0.0577   1.0000
  14.500   0.9523   0.05233   0.04470   0.0674   0.0562   1.0000
  14.750   0.9588   0.05424   0.04659   0.0674   0.0549   1.0000
  15.000   0.9521   0.05745   0.05013   0.0676   0.0535   1.0000
  15.250   0.9447   0.06088   0.05382   0.0674   0.0522   1.0000
  15.500   0.9363   0.06455   0.05772   0.0668   0.0512   1.0000
  15.750   0.9266   0.06854   0.06190   0.0658   0.0502   1.0000
  16.000   0.9155   0.07294   0.06647   0.0643   0.0495   1.0000
  16.250   0.9050   0.07748   0.07115   0.0623   0.0487   1.0000
  16.500   0.8978   0.08179   0.07555   0.0603   0.0479   1.0000
  16.750   0.8867   0.08698   0.08085   0.0576   0.0474   1.0000
  17.000   0.8690   0.09354   0.08754   0.0540   0.0470   1.0000
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