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PW1211 (pw1211-pw) Xfoil prediction polar at RE=5,000,000 Ncrit=9


Details Polar file
Airfoil: PW1211 (pw1211-pw)
Reynolds number: 5,000,000
Max Cl/Cd: 114.18 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-pw1211-pw-5000000.txt
Download as CSV file: xf-pw1211-pw-5000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: PW1211                                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     5.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -1.4884   0.03988   0.03840  -0.0072   1.0000   0.0020
 -15.250  -1.4909   0.03616   0.03450  -0.0071   1.0000   0.0020
 -15.000  -1.4846   0.03344   0.03163  -0.0066   1.0000   0.0021
 -14.750  -1.4804   0.03005   0.02802  -0.0060   1.0000   0.0023
 -14.500  -1.4656   0.02825   0.02612  -0.0054   1.0000   0.0025
 -14.250  -1.4442   0.02754   0.02542  -0.0050   1.0000   0.0027
 -14.000  -1.4205   0.02721   0.02512  -0.0046   1.0000   0.0028
 -13.750  -1.3967   0.02686   0.02479  -0.0042   1.0000   0.0030
 -13.500  -1.3717   0.02674   0.02470  -0.0038   1.0000   0.0031
 -13.250  -1.3472   0.02649   0.02447  -0.0035   1.0000   0.0032
 -13.000  -1.3219   0.02640   0.02441  -0.0031   1.0000   0.0033
 -12.750  -1.2961   0.02640   0.02444  -0.0028   1.0000   0.0033
 -12.500  -1.2705   0.02634   0.02441  -0.0025   1.0000   0.0034
 -12.250  -1.2449   0.02626   0.02435  -0.0022   1.0000   0.0035
 -12.000  -1.2190   0.02625   0.02437  -0.0019   1.0000   0.0035
 -11.750  -1.1929   0.02628   0.02444  -0.0016   1.0000   0.0036
 -11.500  -1.1669   0.02628   0.02446  -0.0014   1.0000   0.0036
 -11.250  -1.1407   0.02631   0.02451  -0.0011   1.0000   0.0036
 -11.000  -1.1146   0.02631   0.02454  -0.0009   1.0000   0.0037
 -10.750  -1.0884   0.02633   0.02458  -0.0006   1.0000   0.0037
 -10.500  -1.0619   0.02642   0.02470  -0.0004   1.0000   0.0037
 -10.250  -1.0359   0.02636   0.02466  -0.0002   1.0000   0.0038
 -10.000  -1.0101   0.02623   0.02453   0.0000   1.0000   0.0038
  -9.750  -0.9842   0.02608   0.02439   0.0001   1.0000   0.0038
  -9.500  -0.9580   0.02605   0.02437   0.0003   1.0000   0.0038
  -9.250  -0.9326   0.02567   0.02397   0.0004   1.0000   0.0038
  -9.000  -0.9074   0.02517   0.02344   0.0005   1.0000   0.0039
  -8.750  -0.8823   0.02460   0.02283   0.0006   1.0000   0.0039
  -8.500  -0.8570   0.02415   0.02235   0.0008   0.9759   0.0039
  -8.250  -0.8364   0.02376   0.02186   0.0020   0.9438   0.0039
  -8.000  -0.8327   0.01462   0.01160   0.0032   0.9228   0.0043
  -7.750  -0.8081   0.01373   0.01055   0.0037   0.9046   0.0044
  -7.500  -0.7820   0.01324   0.00995   0.0040   0.8879   0.0045
  -7.250  -0.7553   0.01293   0.00958   0.0042   0.8737   0.0046
  -7.000  -0.7282   0.01265   0.00924   0.0043   0.8610   0.0047
  -6.750  -0.7012   0.01234   0.00886   0.0045   0.8484   0.0047
  -6.500  -0.6742   0.01194   0.00838   0.0047   0.8349   0.0048
  -6.250  -0.6473   0.01142   0.00775   0.0049   0.8201   0.0049
  -6.000  -0.6204   0.01079   0.00700   0.0051   0.8040   0.0050
  -5.750  -0.5935   0.01014   0.00623   0.0053   0.7880   0.0050
  -5.500  -0.5663   0.00965   0.00563   0.0055   0.7733   0.0051
  -5.250  -0.5383   0.00956   0.00550   0.0055   0.7600   0.0053
  -5.000  -0.5104   0.00940   0.00530   0.0056   0.7471   0.0054
  -4.750  -0.4830   0.00886   0.00466   0.0058   0.7342   0.0055
  -4.500  -0.4559   0.00813   0.00379   0.0061   0.7205   0.0056
  -4.000  -0.4005   0.00726   0.00272   0.0064   0.6900   0.0058
  -3.750  -0.3724   0.00705   0.00244   0.0065   0.6737   0.0060
  -3.500  -0.3441   0.00693   0.00227   0.0065   0.6557   0.0063
  -3.250  -0.3157   0.00691   0.00222   0.0065   0.6377   0.0064
  -3.000  -0.2872   0.00691   0.00219   0.0065   0.6203   0.0065
  -2.750  -0.2593   0.00651   0.00168   0.0066   0.6050   0.0073
  -2.500  -0.2310   0.00635   0.00145   0.0066   0.5880   0.0078
  -2.250  -0.2026   0.00624   0.00128   0.0066   0.5702   0.0080
  -2.000  -0.1741   0.00614   0.00114   0.0066   0.5546   0.0082
  -1.750  -0.1456   0.00606   0.00100   0.0066   0.5380   0.0083
  -1.500  -0.1171   0.00600   0.00087   0.0066   0.5200   0.0084
  -1.250  -0.0885   0.00595   0.00077   0.0066   0.5011   0.0086
  -1.000  -0.0599   0.00591   0.00068   0.0066   0.4863   0.0087
  -0.750  -0.0313   0.00588   0.00061   0.0066   0.4708   0.0091
  -0.500  -0.0027   0.00587   0.00054   0.0065   0.4521   0.0099
  -0.250   0.0257   0.00575   0.00047   0.0064   0.4284   0.0448
   0.250   0.0823   0.00546   0.00040   0.0063   0.3929   0.1621
   0.500   0.1106   0.00531   0.00038   0.0062   0.3731   0.2380
   0.750   0.1387   0.00516   0.00038   0.0060   0.3522   0.3228
   1.000   0.1665   0.00488   0.00039   0.0059   0.3341   0.4561
   1.250   0.1943   0.00467   0.00041   0.0058   0.3194   0.5645
   1.500   0.2210   0.00424   0.00043   0.0059   0.3062   0.7493
   1.750   0.2478   0.00400   0.00045   0.0062   0.2934   0.8556
   2.000   0.2708   0.00380   0.00050   0.0075   0.2770   0.9600
   2.250   0.3022   0.00390   0.00056   0.0068   0.2571   0.9891
   2.500   0.3356   0.00405   0.00062   0.0056   0.2336   0.9961
   2.750   0.3687   0.00417   0.00067   0.0044   0.2188   0.9990
   3.000   0.3989   0.00427   0.00072   0.0040   0.2080   1.0000
   3.250   0.4268   0.00439   0.00079   0.0040   0.1932   1.0000
   3.500   0.4546   0.00455   0.00086   0.0040   0.1746   1.0000
   3.750   0.4825   0.00469   0.00094   0.0040   0.1603   1.0000
   4.000   0.5105   0.00486   0.00103   0.0040   0.1428   1.0000
   4.250   0.5384   0.00507   0.00115   0.0039   0.1213   1.0000
   4.500   0.5664   0.00523   0.00125   0.0039   0.1087   1.0000
   4.750   0.5944   0.00540   0.00136   0.0038   0.0961   1.0000
   5.000   0.6223   0.00560   0.00149   0.0038   0.0816   1.0000
   5.250   0.6503   0.00581   0.00164   0.0037   0.0692   1.0000
   5.500   0.6782   0.00602   0.00179   0.0036   0.0572   1.0000
   5.750   0.7061   0.00625   0.00195   0.0035   0.0462   1.0000
   6.000   0.7339   0.00649   0.00213   0.0035   0.0367   1.0000
   6.250   0.7617   0.00674   0.00233   0.0034   0.0283   1.0000
   6.500   0.7895   0.00693   0.00250   0.0033   0.0235   1.0000
   6.750   0.8172   0.00720   0.00272   0.0032   0.0172   1.0000
   7.000   0.8449   0.00740   0.00290   0.0031   0.0150   1.0000
   7.250   0.8724   0.00774   0.00319   0.0030   0.0094   1.0000
   7.500   0.8999   0.00799   0.00343   0.0030   0.0069   1.0000
   7.750   0.9271   0.00849   0.00390   0.0029   0.0012   1.0000
   8.000   0.9545   0.00875   0.00417   0.0028   0.0010   1.0000
   8.250   0.9819   0.00903   0.00446   0.0027   0.0010   1.0000
   8.500   1.0092   0.00932   0.00476   0.0027   0.0009   1.0000
   8.750   1.0363   0.00963   0.00510   0.0026   0.0009   1.0000
   9.000   1.0634   0.00995   0.00545   0.0026   0.0009   1.0000
   9.250   1.0903   0.01030   0.00583   0.0025   0.0009   1.0000
   9.500   1.1170   0.01067   0.00623   0.0025   0.0009   1.0000
   9.750   1.1436   0.01108   0.00667   0.0024   0.0009   1.0000
  10.000   1.1700   0.01151   0.00715   0.0024   0.0009   1.0000
  10.250   1.1961   0.01198   0.00766   0.0024   0.0009   1.0000
  10.500   1.2220   0.01249   0.00822   0.0024   0.0009   1.0000
  10.750   1.2476   0.01304   0.00884   0.0024   0.0009   1.0000
  11.000   1.2729   0.01365   0.00950   0.0024   0.0009   1.0000
  11.250   1.2977   0.01430   0.01022   0.0024   0.0009   1.0000
  11.500   1.3222   0.01498   0.01096   0.0025   0.0009   1.0000
  11.750   1.3463   0.01569   0.01175   0.0025   0.0009   1.0000
  12.000   1.3698   0.01648   0.01261   0.0026   0.0008   1.0000
  12.250   1.3926   0.01736   0.01358   0.0027   0.0008   1.0000
  12.500   1.4144   0.01835   0.01466   0.0029   0.0008   1.0000
  12.750   1.4351   0.01945   0.01587   0.0030   0.0009   1.0000
  13.000   1.4546   0.02066   0.01720   0.0033   0.0009   1.0000
  13.250   1.4724   0.02201   0.01867   0.0036   0.0009   1.0000
  13.500   1.4883   0.02352   0.02030   0.0039   0.0009   1.0000
  13.750   1.5014   0.02523   0.02215   0.0042   0.0009   1.0000
  14.000   1.5112   0.02715   0.02421   0.0046   0.0009   1.0000
  14.250   1.5128   0.02959   0.02679   0.0048   0.0009   1.0000
  14.500   1.5074   0.03256   0.02989   0.0043   0.0009   1.0000
  14.750   1.4996   0.03664   0.03411   0.0022   0.0009   1.0000
  15.000   1.4892   0.04181   0.03943  -0.0012   0.0009   1.0000
  15.250   1.4712   0.04881   0.04658  -0.0061   0.0009   1.0000
  15.500   1.4507   0.05659   0.05449  -0.0113   0.0009   1.0000
  15.750   1.4246   0.06543   0.06346  -0.0168   0.0009   1.0000
  16.000   1.3938   0.07509   0.07325  -0.0221   0.0009   1.0000
  16.250   1.3581   0.08563   0.08390  -0.0276   0.0009   1.0000
  16.500   1.3232   0.09606   0.09443  -0.0328   0.0009   1.0000
  16.750   1.2853   0.10734   0.10581  -0.0384   0.0009   1.0000
  17.000   1.2516   0.11810   0.11665  -0.0436   0.0009   1.0000
  17.250   1.2174   0.12941   0.12804  -0.0492   0.0009   1.0000
  17.500   1.1893   0.13984   0.13855  -0.0545   0.0009   1.0000
  17.750   1.1603   0.15093   0.14971  -0.0602   0.0009   1.0000
  18.000   1.1371   0.16113   0.15999  -0.0655   0.0009   1.0000
  18.250   1.1194   0.17048   0.16939  -0.0705   0.0009   1.0000
  18.500   1.0996   0.18078   0.17976  -0.0762   0.0009   1.0000
  18.750   1.0904   0.18859   0.18761  -0.0806   0.0009   1.0000
  19.000   1.0762   0.19851   0.19759  -0.0861   0.0010   1.0000
  19.250   1.0614   0.20946   0.20861  -0.0922   0.0010   1.0000
  19.500   1.0571   0.21691   0.21610  -0.0965   0.0010   1.0000
  19.750   1.0425   0.22972   0.22898  -0.1033   0.0010   1.0000
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