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PW51 (pw51-pw) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: PW51 (pw51-pw)
Reynolds number: 1,000,000
Max Cl/Cd: 90.75 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-pw51-pw-1000000.txt
Download as CSV file: xf-pw51-pw-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: PW51                                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.8731   0.25751   0.25588   0.1039   1.0000   0.0043
 -19.250  -0.8649   0.25452   0.25289   0.1021   1.0000   0.0044
 -19.000  -0.8565   0.25144   0.24981   0.1001   1.0000   0.0044
 -18.750  -0.8480   0.24832   0.24668   0.0981   1.0000   0.0045
 -18.500  -0.8395   0.24515   0.24351   0.0960   1.0000   0.0046
 -18.250  -0.8310   0.24190   0.24026   0.0940   1.0000   0.0047
 -18.000  -0.8226   0.23857   0.23694   0.0920   1.0000   0.0049
 -17.750  -0.8142   0.23519   0.23355   0.0900   1.0000   0.0050
 -17.500  -0.8058   0.23174   0.23010   0.0880   1.0000   0.0052
 -17.250  -0.7975   0.22817   0.22654   0.0859   1.0000   0.0055
 -17.000  -0.7891   0.22445   0.22282   0.0839   1.0000   0.0059
 -16.750  -0.7804   0.21966   0.21804   0.0809   1.0000   0.0063
 -16.500  -0.7730   0.21558   0.21396   0.0784   1.0000   0.0063
 -16.250  -0.7653   0.21178   0.21016   0.0763   1.0000   0.0064
 -16.000  -0.7578   0.20796   0.20635   0.0742   1.0000   0.0064
 -15.750  -0.7504   0.20411   0.20250   0.0722   1.0000   0.0064
 -15.500  -0.7431   0.20023   0.19862   0.0702   1.0000   0.0064
 -15.250  -0.7379   0.19614   0.19453   0.0691   1.0000   0.0066
 -15.000  -0.7303   0.19309   0.19148   0.0678   1.0000   0.0067
 -14.750  -0.7230   0.18987   0.18826   0.0662   1.0000   0.0068
 -14.500  -0.7160   0.18654   0.18494   0.0647   1.0000   0.0070
 -14.250  -0.7092   0.18304   0.18144   0.0630   1.0000   0.0071
 -14.000  -0.7027   0.17939   0.17779   0.0613   1.0000   0.0073
 -13.750  -0.6965   0.17562   0.17402   0.0596   1.0000   0.0074
 -13.500  -0.6905   0.17177   0.17018   0.0579   1.0000   0.0076
 -13.250  -0.6850   0.16786   0.16627   0.0562   1.0000   0.0078
 -13.000  -0.6799   0.16386   0.16228   0.0545   1.0000   0.0080
 -12.750  -0.6751   0.15974   0.15816   0.0528   1.0000   0.0083
 -12.500  -0.6707   0.15524   0.15367   0.0509   1.0000   0.0086
 -12.250  -0.6680   0.14983   0.14826   0.0480   1.0000   0.0090
 -12.000  -0.6645   0.14526   0.14370   0.0460   1.0000   0.0090
 -11.750  -0.6610   0.14078   0.13923   0.0441   1.0000   0.0091
 -11.500  -0.6580   0.13618   0.13464   0.0423   1.0000   0.0091
 -11.250  -0.6557   0.13152   0.12998   0.0404   1.0000   0.0091
 -11.000  -0.6541   0.12671   0.12518   0.0384   1.0000   0.0091
  -8.750  -0.8120   0.03292   0.03021  -0.0128   1.0000   0.0064
  -8.500  -0.8114   0.02605   0.02262  -0.0120   1.0000   0.0065
  -8.250  -0.7975   0.02223   0.01833  -0.0112   1.0000   0.0067
  -8.000  -0.7775   0.01995   0.01577  -0.0106   1.0000   0.0068
  -7.750  -0.7548   0.01838   0.01398  -0.0101   1.0000   0.0069
  -7.500  -0.7308   0.01713   0.01258  -0.0097   1.0000   0.0071
  -7.250  -0.7060   0.01605   0.01136  -0.0093   1.0000   0.0072
  -7.000  -0.6808   0.01506   0.01025  -0.0090   1.0000   0.0074
  -6.750  -0.6552   0.01416   0.00923  -0.0087   1.0000   0.0076
  -6.500  -0.6292   0.01339   0.00838  -0.0084   1.0000   0.0078
  -6.250  -0.6027   0.01277   0.00767  -0.0082   1.0000   0.0082
  -6.000  -0.5760   0.01216   0.00700  -0.0080   1.0000   0.0086
  -5.750  -0.5492   0.01160   0.00636  -0.0078   1.0000   0.0090
  -5.500  -0.5236   0.01064   0.00530  -0.0074   1.0000   0.0096
  -5.250  -0.4965   0.01008   0.00471  -0.0073   0.9990   0.0105
  -4.750  -0.4327   0.00942   0.00397  -0.0088   0.9649   0.0125
  -4.500  -0.4089   0.00896   0.00344  -0.0077   0.9438   0.0146
  -4.250  -0.3849   0.00877   0.00319  -0.0066   0.9232   0.0168
  -4.000  -0.3604   0.00848   0.00285  -0.0057   0.9022   0.0214
  -3.750  -0.3348   0.00825   0.00257  -0.0050   0.8818   0.0276
  -3.500  -0.3084   0.00805   0.00233  -0.0045   0.8604   0.0354
  -3.250  -0.2818   0.00786   0.00211  -0.0041   0.8392   0.0477
  -3.000  -0.2548   0.00766   0.00191  -0.0038   0.8168   0.0673
  -2.750  -0.2278   0.00744   0.00173  -0.0036   0.7948   0.0969
  -2.500  -0.2006   0.00719   0.00158  -0.0034   0.7726   0.1397
  -2.250  -0.1734   0.00697   0.00143  -0.0033   0.7511   0.1869
  -2.000  -0.1461   0.00670   0.00130  -0.0032   0.7301   0.2462
  -1.500  -0.0921   0.00606   0.00109  -0.0031   0.6907   0.4154
  -1.250  -0.0653   0.00570   0.00101  -0.0029   0.6713   0.5201
  -1.000  -0.0389   0.00536   0.00095  -0.0027   0.6524   0.6252
  -0.750  -0.0127   0.00510   0.00091  -0.0023   0.6339   0.7164
  -0.500   0.0135   0.00491   0.00090  -0.0017   0.6159   0.7891
  -0.250   0.0392   0.00480   0.00091  -0.0010   0.5972   0.8475
   0.000   0.0647   0.00476   0.00093  -0.0002   0.5789   0.8915
   0.500   0.1171   0.00483   0.00097   0.0012   0.5432   0.9496
   0.750   0.1469   0.00491   0.00099   0.0010   0.5250   0.9670
   1.000   0.1803   0.00501   0.00101  -0.0001   0.5063   0.9798
   1.500   0.2534   0.00524   0.00106  -0.0037   0.4682   0.9936
   1.750   0.2924   0.00536   0.00109  -0.0061   0.4477   0.9974
   2.000   0.3276   0.00548   0.00112  -0.0078   0.4277   1.0000
   2.250   0.3542   0.00558   0.00115  -0.0075   0.4090   1.0000
   2.500   0.3809   0.00570   0.00119  -0.0073   0.3904   1.0000
   2.750   0.4074   0.00583   0.00124  -0.0071   0.3731   1.0000
   3.000   0.4340   0.00597   0.00131  -0.0068   0.3554   1.0000
   3.250   0.4606   0.00610   0.00139  -0.0066   0.3389   1.0000
   3.500   0.4872   0.00625   0.00147  -0.0063   0.3215   1.0000
   3.750   0.5138   0.00640   0.00156  -0.0061   0.3057   1.0000
   4.000   0.5404   0.00657   0.00167  -0.0058   0.2895   1.0000
   4.250   0.5672   0.00674   0.00179  -0.0057   0.2732   1.0000
   4.500   0.5940   0.00693   0.00192  -0.0055   0.2575   1.0000
   5.000   0.6479   0.00733   0.00221  -0.0052   0.2253   1.0000
   5.250   0.6749   0.00755   0.00237  -0.0051   0.2090   1.0000
   5.500   0.7018   0.00779   0.00255  -0.0050   0.1911   1.0000
   5.750   0.7286   0.00807   0.00276  -0.0050   0.1721   1.0000
   6.000   0.7555   0.00835   0.00297  -0.0049   0.1554   1.0000
   6.250   0.7823   0.00862   0.00320  -0.0048   0.1408   1.0000
   6.500   0.8091   0.00892   0.00344  -0.0048   0.1265   1.0000
   6.750   0.8358   0.00923   0.00371  -0.0047   0.1122   1.0000
   7.000   0.8624   0.00957   0.00400  -0.0046   0.0982   1.0000
   7.250   0.8888   0.00992   0.00431  -0.0046   0.0855   1.0000
   7.500   0.9151   0.01031   0.00464  -0.0045   0.0726   1.0000
   7.750   0.9411   0.01073   0.00502  -0.0044   0.0600   1.0000
   8.000   0.9669   0.01119   0.00542  -0.0043   0.0480   1.0000
   8.250   0.9925   0.01166   0.00585  -0.0042   0.0388   1.0000
   8.500   1.0180   0.01216   0.00632  -0.0040   0.0317   1.0000
   8.750   1.0435   0.01262   0.00678  -0.0039   0.0273   1.0000
   9.000   1.0688   0.01311   0.00730  -0.0037   0.0236   1.0000
   9.250   1.0943   0.01352   0.00774  -0.0036   0.0214   1.0000
   9.500   1.1187   0.01416   0.00838  -0.0033   0.0182   1.0000
   9.750   1.1438   0.01459   0.00887  -0.0032   0.0170   1.0000
  10.000   1.1687   0.01504   0.00936  -0.0030   0.0154   1.0000
  10.250   1.1921   0.01574   0.01009  -0.0027   0.0133   1.0000
  10.500   1.2161   0.01630   0.01071  -0.0024   0.0122   1.0000
  10.750   1.2401   0.01679   0.01126  -0.0022   0.0110   1.0000
  11.000   1.2625   0.01754   0.01203  -0.0018   0.0095   1.0000
  11.250   1.2848   0.01825   0.01281  -0.0015   0.0085   1.0000
  11.500   1.3073   0.01888   0.01349  -0.0011   0.0075   1.0000
  11.750   1.3253   0.02011   0.01481  -0.0004   0.0062   1.0000
  12.000   1.3465   0.02082   0.01561   0.0000   0.0057   1.0000
  12.250   1.3660   0.02171   0.01658   0.0006   0.0052   1.0000
  12.500   1.3830   0.02282   0.01776   0.0013   0.0047   1.0000
  12.750   1.3908   0.02486   0.01997   0.0026   0.0042   1.0000
  13.000   1.4026   0.02625   0.02150   0.0035   0.0041   1.0000
  13.250   1.4118   0.02762   0.02299   0.0047   0.0040   1.0000
  13.500   1.4155   0.02932   0.02481   0.0060   0.0039   1.0000
  13.750   1.4164   0.03153   0.02716   0.0065   0.0038   1.0000
  14.000   1.4153   0.03434   0.03012   0.0061   0.0037   1.0000
  14.250   1.4122   0.03783   0.03376   0.0047   0.0037   1.0000
  14.500   1.4065   0.04209   0.03819   0.0024   0.0036   1.0000
  14.750   1.3978   0.04710   0.04335  -0.0004   0.0036   1.0000
  15.000   1.3852   0.05287   0.04927  -0.0037   0.0036   1.0000
  15.250   1.3688   0.05935   0.05590  -0.0073   0.0036   1.0000
  15.500   1.3492   0.06643   0.06313  -0.0111   0.0036   1.0000
  15.750   1.3268   0.07398   0.07082  -0.0149   0.0036   1.0000
  16.000   1.3027   0.08190   0.07887  -0.0188   0.0036   1.0000
  16.250   1.2774   0.09013   0.08722  -0.0228   0.0037   1.0000
  16.500   1.2525   0.09858   0.09578  -0.0269   0.0037   1.0000
  16.750   1.2290   0.10697   0.10428  -0.0310   0.0037   1.0000
  17.000   1.2068   0.11533   0.11275  -0.0351   0.0037   1.0000
  17.250   1.1866   0.12346   0.12098  -0.0390   0.0038   1.0000
  17.500   1.1676   0.13159   0.12920  -0.0431   0.0038   1.0000
  17.750   1.1504   0.13947   0.13717  -0.0470   0.0038   1.0000
  18.000   1.1353   0.14715   0.14494  -0.0510   0.0038   1.0000
  18.250   1.1216   0.15477   0.15264  -0.0550   0.0038   1.0000
  18.500   1.1084   0.16249   0.16044  -0.0592   0.0038   1.0000
  18.750   1.0957   0.17037   0.16840  -0.0636   0.0038   1.0000
  19.000   1.0836   0.17844   0.17655  -0.0681   0.0039   1.0000
  19.250   1.0713   0.18697   0.18517  -0.0730   0.0039   1.0000
  19.500   1.0565   0.19676   0.19506  -0.0787   0.0039   1.0000
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