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WASP (smoothed) (waspsm-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WASP (smoothed) (waspsm-il)
Reynolds number: 50,000
Max Cl/Cd: 37.55 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-waspsm-il-50000-n5.txt
Download as CSV file: xf-waspsm-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WASP (smoothed)                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.4301   0.09727   0.09020  -0.0288   1.0000   0.0622
  -8.250  -0.4231   0.09379   0.08675  -0.0281   1.0000   0.0611
  -8.000  -0.4213   0.09028   0.08331  -0.0285   1.0000   0.0599
  -7.750  -0.4221   0.08658   0.07970  -0.0296   1.0000   0.0587
  -7.500  -0.4220   0.08245   0.07564  -0.0318   1.0000   0.0576
  -7.250  -0.4219   0.07798   0.07123  -0.0345   1.0000   0.0565
  -7.000  -0.4214   0.07309   0.06637  -0.0376   1.0000   0.0554
  -6.750  -0.4202   0.06778   0.06105  -0.0407   1.0000   0.0544
  -6.500  -0.4175   0.06249   0.05567  -0.0433   1.0000   0.0538
  -6.250  -0.4119   0.05810   0.05115  -0.0446   1.0000   0.0544
  -6.000  -0.4043   0.05406   0.04695  -0.0455   1.0000   0.0557
  -5.750  -0.3952   0.04995   0.04257  -0.0461   1.0000   0.0570
  -5.500  -0.3842   0.04584   0.03809  -0.0464   1.0000   0.0581
  -5.250  -0.3708   0.04200   0.03382  -0.0463   1.0000   0.0587
  -5.000  -0.3551   0.03850   0.02981  -0.0458   1.0000   0.0596
  -4.750  -0.3371   0.03539   0.02602  -0.0451   1.0000   0.0618
  -4.500  -0.3189   0.03338   0.02382  -0.0443   1.0000   0.0652
  -4.250  -0.2992   0.03168   0.02188  -0.0434   1.0000   0.0687
  -4.000  -0.2774   0.02971   0.01950  -0.0425   1.0000   0.0717
  -3.750  -0.2547   0.02808   0.01741  -0.0417   1.0000   0.0766
  -3.500  -0.2336   0.02701   0.01631  -0.0409   1.0000   0.0830
  -3.250  -0.2099   0.02580   0.01474  -0.0401   1.0000   0.0891
  -3.000  -0.1873   0.02493   0.01390  -0.0395   1.0000   0.0985
  -2.750  -0.1637   0.02409   0.01296  -0.0390   1.0000   0.1090
  -2.500  -0.1360   0.02340   0.01219  -0.0393   0.9982   0.1255
  -2.250  -0.0929   0.02256   0.01132  -0.0426   0.9889   0.1559
  -2.000  -0.0504   0.02169   0.01064  -0.0460   0.9789   0.2111
  -1.750  -0.0090   0.02071   0.01022  -0.0492   0.9688   0.3252
  -1.500   0.0277   0.01964   0.01006  -0.0510   0.9584   0.5335
  -1.250   0.0845   0.01834   0.00967  -0.0553   0.9503   1.0000
  -1.000   0.1286   0.01845   0.00934  -0.0587   0.9374   1.0000
  -0.750   0.1723   0.01852   0.00909  -0.0619   0.9244   1.0000
  -0.500   0.2135   0.01859   0.00889  -0.0644   0.9101   1.0000
  -0.250   0.2526   0.01863   0.00870  -0.0665   0.8950   1.0000
   0.000   0.2883   0.01868   0.00856  -0.0678   0.8785   1.0000
   0.250   0.3225   0.01872   0.00844  -0.0688   0.8613   1.0000
   0.500   0.3561   0.01875   0.00833  -0.0695   0.8438   1.0000
   0.750   0.3893   0.01878   0.00823  -0.0701   0.8262   1.0000
   1.000   0.4219   0.01880   0.00813  -0.0705   0.8085   1.0000
   1.250   0.4541   0.01883   0.00804  -0.0707   0.7908   1.0000
   1.500   0.4819   0.01895   0.00807  -0.0702   0.7704   1.0000
   1.750   0.5106   0.01905   0.00809  -0.0698   0.7508   1.0000
   2.000   0.5396   0.01916   0.00809  -0.0694   0.7318   1.0000
   2.250   0.5659   0.01935   0.00820  -0.0687   0.7113   1.0000
   2.500   0.5927   0.01955   0.00832  -0.0680   0.6911   1.0000
   2.750   0.6200   0.01975   0.00845  -0.0674   0.6718   1.0000
   3.000   0.6454   0.02002   0.00867  -0.0665   0.6513   1.0000
   3.250   0.6710   0.02030   0.00889  -0.0657   0.6313   1.0000
   3.500   0.6970   0.02058   0.00910  -0.0650   0.6123   1.0000
   3.750   0.7219   0.02091   0.00943  -0.0641   0.5926   1.0000
   4.000   0.7465   0.02127   0.00976  -0.0632   0.5732   1.0000
   4.250   0.7714   0.02164   0.01009  -0.0624   0.5545   1.0000
   4.500   0.7964   0.02201   0.01046  -0.0615   0.5364   1.0000
   4.750   0.8199   0.02246   0.01093  -0.0606   0.5174   1.0000
   5.000   0.8436   0.02292   0.01140  -0.0596   0.4990   1.0000
   5.250   0.8673   0.02339   0.01189  -0.0587   0.4813   1.0000
   5.500   0.8909   0.02388   0.01243  -0.0578   0.4639   1.0000
   5.750   0.9144   0.02439   0.01296  -0.0568   0.4472   1.0000
   6.000   0.9372   0.02496   0.01359  -0.0558   0.4303   1.0000
   6.250   0.9595   0.02556   0.01427  -0.0548   0.4134   1.0000
   6.500   0.9818   0.02619   0.01502  -0.0538   0.3972   1.0000
   6.750   1.0038   0.02684   0.01577  -0.0528   0.3814   1.0000
   7.000   1.0255   0.02753   0.01656  -0.0517   0.3660   1.0000
   7.250   1.0470   0.02826   0.01741  -0.0506   0.3512   1.0000
   7.500   1.0680   0.02902   0.01832  -0.0495   0.3364   1.0000
   7.750   1.0888   0.02982   0.01925  -0.0484   0.3224   1.0000
   8.000   1.1089   0.03065   0.02022  -0.0471   0.3083   1.0000
   8.250   1.1285   0.03151   0.02123  -0.0459   0.2944   1.0000
   8.500   1.1468   0.03238   0.02226  -0.0444   0.2798   1.0000
   8.750   1.1625   0.03322   0.02328  -0.0427   0.2632   1.0000
   9.000   1.1748   0.03395   0.02410  -0.0406   0.2441   1.0000
   9.250   1.1843   0.03476   0.02496  -0.0382   0.2238   1.0000
   9.500   1.1919   0.03578   0.02612  -0.0358   0.2031   1.0000
   9.750   1.1978   0.03693   0.02730  -0.0334   0.1839   1.0000
  10.000   1.2013   0.03840   0.02891  -0.0309   0.1627   1.0000
  10.250   1.2006   0.04009   0.03061  -0.0281   0.1440   1.0000
  10.750   1.1926   0.04459   0.03517  -0.0231   0.1109   1.0000
  11.000   1.1867   0.04737   0.03794  -0.0214   0.0990   1.0000
  11.250   1.1800   0.05044   0.04099  -0.0202   0.0901   1.0000
  11.500   1.1753   0.05370   0.04437  -0.0194   0.0820   1.0000
  11.750   1.1687   0.05719   0.04782  -0.0190   0.0772   1.0000
  12.000   1.1647   0.06078   0.05163  -0.0188   0.0717   1.0000
  12.250   1.1589   0.06453   0.05543  -0.0190   0.0677   1.0000
  12.500   1.1537   0.06842   0.05939  -0.0193   0.0643   1.0000
  12.750   1.1491   0.07251   0.06372  -0.0198   0.0611   1.0000
  13.000   1.1445   0.07661   0.06798  -0.0203   0.0587   1.0000
  13.250   1.1402   0.08065   0.07210  -0.0209   0.0566   1.0000
  13.500   1.1375   0.08438   0.07579  -0.0212   0.0545   1.0000
  13.750   1.1276   0.08988   0.08161  -0.0230   0.0532   1.0000
  14.000   1.1156   0.09589   0.08789  -0.0253   0.0521   1.0000
  14.250   1.1014   0.10252   0.09477  -0.0282   0.0513   1.0000
  14.500   1.0846   0.11001   0.10249  -0.0318   0.0509   1.0000
  14.750   1.0638   0.11886   0.11154  -0.0364   0.0509   1.0000
  15.000   1.0377   0.12979   0.12265  -0.0425   0.0516   1.0000
  15.250   1.0093   0.14239   0.13532  -0.0495   0.0525   1.0000
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