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PW106 (pw106-pw) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: PW106 (pw106-pw)
Reynolds number: 1,000,000
Max Cl/Cd: 84.92 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-pw106-pw-1000000.txt
Download as CSV file: xf-pw106-pw-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: PW106                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -20.000  -0.8750   0.26807   0.26641   0.1108   1.0000   0.0061
 -19.750  -0.8653   0.26506   0.26340   0.1087   1.0000   0.0062
 -19.500  -0.8559   0.26198   0.26032   0.1065   1.0000   0.0063
 -19.250  -0.8465   0.25890   0.25724   0.1043   1.0000   0.0064
 -19.000  -0.8372   0.25578   0.25412   0.1022   1.0000   0.0065
 -18.750  -0.8280   0.25263   0.25098   0.1001   1.0000   0.0066
 -18.500  -0.8188   0.24945   0.24780   0.0980   1.0000   0.0066
 -18.250  -0.8097   0.24624   0.24459   0.0959   1.0000   0.0066
 -18.000  -0.8006   0.24300   0.24135   0.0938   1.0000   0.0067
 -17.750  -0.7915   0.23972   0.23807   0.0918   1.0000   0.0067
 -17.500  -0.7826   0.23642   0.23478   0.0897   1.0000   0.0067
 -17.250  -0.7737   0.23311   0.23147   0.0877   1.0000   0.0068
 -17.000  -0.7649   0.22977   0.22813   0.0857   1.0000   0.0068
 -16.750  -0.7561   0.22638   0.22474   0.0837   1.0000   0.0068
 -16.500  -0.7474   0.22294   0.22130   0.0817   1.0000   0.0068
 -16.250  -0.7387   0.21948   0.21785   0.0798   1.0000   0.0068
 -16.000  -0.7301   0.21600   0.21437   0.0778   1.0000   0.0068
 -15.750  -0.7217   0.21248   0.21086   0.0759   1.0000   0.0068
 -15.500  -0.7134   0.20892   0.20730   0.0741   1.0000   0.0068
 -15.250  -0.7052   0.20533   0.20370   0.0722   1.0000   0.0069
 -15.000  -0.6972   0.20173   0.20010   0.0704   1.0000   0.0069
 -14.750  -0.6894   0.19809   0.19646   0.0686   1.0000   0.0069
 -14.500  -0.6817   0.19443   0.19281   0.0668   1.0000   0.0069
 -14.250  -0.6741   0.19072   0.18910   0.0650   1.0000   0.0069
 -14.000  -0.6668   0.18694   0.18533   0.0633   1.0000   0.0069
 -13.750  -0.6597   0.18316   0.18155   0.0615   1.0000   0.0069
 -13.500  -0.6529   0.17930   0.17771   0.0599   1.0000   0.0068
 -13.250  -0.6465   0.17541   0.17381   0.0582   1.0000   0.0068
 -13.000  -0.6407   0.17134   0.16975   0.0566   1.0000   0.0067
 -12.750  -0.6356   0.16706   0.16548   0.0549   1.0000   0.0066
 -12.500  -0.6348   0.16182   0.16025   0.0534   1.0000   0.0058
 -12.250  -0.6317   0.15742   0.15586   0.0518   1.0000   0.0051
 -12.000  -0.6282   0.15303   0.15147   0.0501   1.0000   0.0046
 -11.750  -0.6249   0.14848   0.14693   0.0484   1.0000   0.0041
 -11.500  -0.6221   0.14385   0.14232   0.0467   1.0000   0.0038
 -11.250  -0.6206   0.13883   0.13731   0.0448   1.0000   0.0034
 -11.000  -0.6207   0.13331   0.13180   0.0427   1.0000   0.0031
 -10.750  -0.6241   0.12690   0.12540   0.0403   1.0000   0.0028
 -10.500  -0.6295   0.12008   0.11860   0.0376   1.0000   0.0026
 -10.250  -0.6345   0.11373   0.11226   0.0349   1.0000   0.0025
 -10.000  -0.6377   0.10807   0.10662   0.0323   1.0000   0.0025
  -9.750  -0.6425   0.10210   0.10067   0.0293   1.0000   0.0024
  -9.500  -0.6476   0.09613   0.09473   0.0260   1.0000   0.0024
  -9.250  -0.6556   0.08953   0.08815   0.0218   1.0000   0.0024
  -9.000  -0.8295   0.02670   0.02373  -0.0144   1.0000   0.0025
  -8.750  -0.8091   0.02474   0.02153  -0.0141   1.0000   0.0028
  -8.500  -0.8031   0.01780   0.01348  -0.0125   1.0000   0.0027
  -8.250  -0.7828   0.01525   0.01041  -0.0117   1.0000   0.0027
  -8.000  -0.7583   0.01402   0.00891  -0.0112   1.0000   0.0026
  -7.750  -0.7325   0.01319   0.00790  -0.0109   1.0000   0.0026
  -7.500  -0.7061   0.01254   0.00712  -0.0106   1.0000   0.0026
  -7.250  -0.6792   0.01200   0.00647  -0.0104   1.0000   0.0025
  -7.000  -0.6519   0.01153   0.00588  -0.0103   1.0000   0.0026
  -6.750  -0.6244   0.01114   0.00542  -0.0102   1.0000   0.0026
  -6.500  -0.5967   0.01077   0.00501  -0.0102   1.0000   0.0026
  -6.250  -0.5681   0.01044   0.00464  -0.0103   0.9958   0.0027
  -6.000  -0.5356   0.01016   0.00432  -0.0112   0.9738   0.0027
  -5.750  -0.5104   0.00996   0.00406  -0.0104   0.9513   0.0028
  -5.500  -0.4873   0.00978   0.00382  -0.0091   0.9293   0.0028
  -5.250  -0.4629   0.00961   0.00357  -0.0081   0.9085   0.0028
  -4.750  -0.4114   0.00930   0.00312  -0.0067   0.8671   0.0030
  -4.500  -0.3846   0.00916   0.00287  -0.0063   0.8466   0.0030
  -4.250  -0.3575   0.00903   0.00267  -0.0059   0.8258   0.0031
  -4.000  -0.3301   0.00892   0.00249  -0.0057   0.8054   0.0032
  -3.750  -0.3025   0.00881   0.00233  -0.0055   0.7848   0.0032
  -3.500  -0.2747   0.00872   0.00220  -0.0053   0.7649   0.0034
  -3.250  -0.2468   0.00865   0.00210  -0.0052   0.7454   0.0037
  -3.000  -0.2187   0.00860   0.00203  -0.0052   0.7270   0.0039
  -2.750  -0.1906   0.00858   0.00202  -0.0052   0.7088   0.0043
  -2.500  -0.1623   0.00869   0.00219  -0.0052   0.6912   0.0050
  -2.250  -0.1338   0.00893   0.00253  -0.0055   0.6736   0.0059
  -1.750  -0.0768   0.00921   0.00285  -0.0057   0.6402   0.0075
  -1.500  -0.0494   0.00871   0.00223  -0.0055   0.6249   0.0078
  -1.250  -0.0216   0.00830   0.00167  -0.0052   0.6098   0.0091
  -1.000   0.0066   0.00813   0.00140  -0.0051   0.5945   0.0112
  -0.750   0.0351   0.00805   0.00124  -0.0051   0.5796   0.0107
  -0.500   0.0636   0.00801   0.00111  -0.0051   0.5648   0.0105
  -0.250   0.0921   0.00798   0.00100  -0.0050   0.5502   0.0105
   0.000   0.1206   0.00797   0.00092  -0.0050   0.5356   0.0110
   0.500   0.1756   0.00733   0.00087  -0.0051   0.5071   0.2210
   0.750   0.2007   0.00651   0.00085  -0.0050   0.4935   0.4956
   1.000   0.2212   0.00550   0.00088  -0.0036   0.4805   0.8168
   1.250   0.2823   0.00533   0.00110  -0.0100   0.4617   0.9988
   1.500   0.3137   0.00542   0.00111  -0.0108   0.4468   1.0000
   1.750   0.3408   0.00550   0.00112  -0.0106   0.4331   1.0000
   2.000   0.3678   0.00560   0.00114  -0.0105   0.4188   1.0000
   2.250   0.3948   0.00570   0.00117  -0.0103   0.4049   1.0000
   2.500   0.4217   0.00581   0.00122  -0.0101   0.3905   1.0000
   3.000   0.4753   0.00604   0.00132  -0.0097   0.3619   1.0000
   3.250   0.5022   0.00617   0.00139  -0.0095   0.3480   1.0000
   3.500   0.5290   0.00630   0.00146  -0.0093   0.3352   1.0000
   3.750   0.5554   0.00654   0.00155  -0.0092   0.3033   1.0000
   4.000   0.5807   0.00712   0.00174  -0.0091   0.2289   1.0000
   4.250   0.6061   0.00765   0.00195  -0.0090   0.1714   1.0000
   4.500   0.6304   0.00846   0.00233  -0.0088   0.0951   1.0000
   4.750   0.6537   0.00962   0.00301  -0.0085   0.0024   1.0000
   5.000   0.6789   0.01028   0.00370  -0.0081   0.0022   1.0000
   5.250   0.7033   0.01109   0.00448  -0.0077   0.0021   1.0000
   5.750   0.7579   0.01103   0.00431  -0.0076   0.0021   1.0000
   6.250   0.8130   0.01091   0.00423  -0.0076   0.0019   1.0000
   6.500   0.8396   0.01112   0.00447  -0.0075   0.0019   1.0000
   6.750   0.8662   0.01135   0.00474  -0.0074   0.0020   1.0000
   7.000   0.8930   0.01155   0.00508  -0.0073   0.0020   1.0000
   7.250   0.9196   0.01180   0.00535  -0.0072   0.0021   1.0000
   7.500   0.9460   0.01209   0.00566  -0.0071   0.0022   1.0000
   7.750   0.9722   0.01242   0.00604  -0.0070   0.0023   1.0000
   8.000   0.9982   0.01279   0.00646  -0.0068   0.0024   1.0000
   8.250   1.0240   0.01320   0.00695  -0.0066   0.0025   1.0000
   8.500   1.0494   0.01368   0.00753  -0.0064   0.0026   1.0000
   8.750   1.0743   0.01422   0.00818  -0.0061   0.0027   1.0000
   9.000   1.0987   0.01483   0.00889  -0.0058   0.0029   1.0000
   9.250   1.1226   0.01550   0.00966  -0.0054   0.0031   1.0000
   9.500   1.1460   0.01623   0.01049  -0.0051   0.0034   1.0000
   9.750   1.1682   0.01710   0.01154  -0.0046   0.0035   1.0000
  10.000   1.1896   0.01805   0.01261  -0.0041   0.0038   1.0000
  10.250   1.2092   0.01919   0.01391  -0.0034   0.0042   1.0000
  10.500   1.2255   0.02072   0.01565  -0.0024   0.0046   1.0000
  10.750   1.2359   0.02290   0.01808  -0.0008   0.0052   1.0000
  11.000   1.2409   0.02558   0.02101   0.0011   0.0058   1.0000
  11.250   1.2411   0.02867   0.02435   0.0032   0.0064   1.0000
  11.500   1.2349   0.03189   0.02780   0.0055   0.0069   1.0000
  11.750   1.2240   0.03590   0.03205   0.0070   0.0074   1.0000
  12.000   1.2080   0.04083   0.03724   0.0074   0.0077   1.0000
  15.000   1.0193   0.12189   0.12003  -0.0362   0.0080   1.0000
  15.250   1.0107   0.12903   0.12724  -0.0402   0.0079   1.0000
  15.500   1.0024   0.13626   0.13453  -0.0442   0.0077   1.0000
  15.750   0.9918   0.14427   0.14260  -0.0485   0.0076   1.0000
  16.000   0.9816   0.15243   0.15081  -0.0528   0.0074   1.0000
  16.250   0.9716   0.16084   0.15927  -0.0571   0.0071   1.0000
  16.500   0.9589   0.17055   0.16902  -0.0619   0.0068   1.0000
  16.750   0.9444   0.18148   0.17996  -0.0670   0.0065   1.0000
  17.000   0.9301   0.19357   0.19203  -0.0722   0.0067   1.0000
  17.250   0.9246   0.20280   0.20124  -0.0764   0.0072   1.0000
  19.500   0.6726   0.21202   0.21053  -0.0559   0.0083   1.0000
  19.750   0.6741   0.21547   0.21398  -0.0572   0.0083   1.0000
  20.000   0.6760   0.21890   0.21741  -0.0584   0.0083   1.0000
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