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PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: PSU-90-125WL (psu-90-125wl-il)
Reynolds number: 500,000
Max Cl/Cd: 87.8 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-psu-90-125wl-il-500000-n5.txt
Download as CSV file: xf-psu-90-125wl-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: PSU-90-125WL                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.5601   0.08865   0.08620  -0.0481   1.0000   0.0102
 -12.500  -0.6604   0.06126   0.05850  -0.0659   1.0000   0.0098
 -12.250  -0.6863   0.05301   0.05007  -0.0722   1.0000   0.0097
 -12.000  -0.7084   0.04709   0.04397  -0.0759   1.0000   0.0097
 -11.750  -0.7290   0.04257   0.03928  -0.0775   1.0000   0.0096
 -11.500  -0.7461   0.03946   0.03602  -0.0770   1.0000   0.0097
 -11.250  -0.7666   0.03714   0.03357  -0.0742   1.0000   0.0098
 -11.000  -0.7680   0.03443   0.03063  -0.0744   0.9948   0.0098
 -10.750  -0.7550   0.03157   0.02748  -0.0761   0.9873   0.0100
 -10.500  -0.7369   0.02920   0.02484  -0.0775   0.9815   0.0101
 -10.250  -0.7181   0.02730   0.02269  -0.0782   0.9735   0.0103
 -10.000  -0.6961   0.02561   0.02076  -0.0789   0.9658   0.0105
  -9.750  -0.6712   0.02405   0.01899  -0.0800   0.9580   0.0107
  -9.500  -0.6461   0.02276   0.01751  -0.0807   0.9486   0.0108
  -9.250  -0.6183   0.02152   0.01609  -0.0818   0.9403   0.0109
  -9.000  -0.5903   0.02048   0.01488  -0.0827   0.9305   0.0111
  -8.750  -0.5673   0.01881   0.01304  -0.0829   0.9186   0.0115
  -8.500  -0.5431   0.01787   0.01198  -0.0830   0.9068   0.0119
  -8.250  -0.5194   0.01712   0.01112  -0.0827   0.8956   0.0121
  -8.000  -0.4963   0.01643   0.01032  -0.0822   0.8851   0.0124
  -7.750  -0.4736   0.01579   0.00958  -0.0816   0.8754   0.0127
  -7.500  -0.4505   0.01519   0.00888  -0.0810   0.8667   0.0129
  -7.250  -0.4273   0.01464   0.00822  -0.0804   0.8580   0.0133
  -7.000  -0.4036   0.01413   0.00762  -0.0799   0.8507   0.0136
  -6.750  -0.3796   0.01365   0.00706  -0.0793   0.8435   0.0139
  -6.500  -0.3552   0.01322   0.00654  -0.0789   0.8371   0.0142
  -6.250  -0.3304   0.01283   0.00606  -0.0785   0.8304   0.0146
  -5.750  -0.2798   0.01211   0.00519  -0.0777   0.8187   0.0152
  -5.500  -0.2548   0.01168   0.00469  -0.0774   0.8128   0.0162
  -5.250  -0.2290   0.01138   0.00433  -0.0771   0.8074   0.0173
  -5.000  -0.2028   0.01111   0.00401  -0.0769   0.8017   0.0183
  -4.750  -0.1763   0.01089   0.00371  -0.0766   0.7965   0.0192
  -4.500  -0.1496   0.01067   0.00345  -0.0764   0.7914   0.0209
  -4.250  -0.1232   0.01041   0.00319  -0.0762   0.7860   0.0261
  -4.000  -0.0974   0.01006   0.00293  -0.0760   0.7811   0.0514
  -3.750  -0.0714   0.00972   0.00271  -0.0758   0.7760   0.0842
  -3.500  -0.0455   0.00937   0.00252  -0.0757   0.7706   0.1266
  -3.250  -0.0196   0.00904   0.00235  -0.0755   0.7658   0.1763
  -3.000   0.0069   0.00877   0.00221  -0.0754   0.7606   0.2182
  -2.750   0.0334   0.00851   0.00208  -0.0753   0.7552   0.2637
  -2.250   0.0855   0.00788   0.00187  -0.0751   0.7451   0.3951
  -2.000   0.1115   0.00757   0.00180  -0.0749   0.7397   0.4671
  -1.750   0.1382   0.00742   0.00176  -0.0747   0.7347   0.5146
  -1.500   0.1655   0.00731   0.00174  -0.0746   0.7289   0.5511
  -1.250   0.1928   0.00725   0.00172  -0.0744   0.7229   0.5810
  -1.000   0.2203   0.00721   0.00172  -0.0743   0.7169   0.6040
  -0.750   0.2479   0.00719   0.00171  -0.0742   0.7103   0.6237
  -0.500   0.2755   0.00718   0.00170  -0.0741   0.7040   0.6404
  -0.250   0.3032   0.00717   0.00171  -0.0740   0.6969   0.6555
   0.000   0.3307   0.00717   0.00171  -0.0739   0.6900   0.6685
   0.250   0.3583   0.00717   0.00172  -0.0738   0.6819   0.6802
   0.500   0.3857   0.00718   0.00173  -0.0736   0.6734   0.6917
   0.750   0.4130   0.00721   0.00175  -0.0735   0.6634   0.7033
   1.000   0.4401   0.00722   0.00177  -0.0733   0.6525   0.7147
   1.250   0.4670   0.00725   0.00180  -0.0730   0.6405   0.7254
   1.500   0.4938   0.00729   0.00184  -0.0728   0.6270   0.7360
   1.750   0.5202   0.00735   0.00188  -0.0724   0.6112   0.7470
   2.000   0.5460   0.00743   0.00193  -0.0720   0.5930   0.7579
   2.250   0.5713   0.00754   0.00200  -0.0715   0.5736   0.7689
   2.500   0.5965   0.00767   0.00208  -0.0709   0.5523   0.7802
   2.750   0.6210   0.00784   0.00219  -0.0703   0.5309   0.7920
   3.000   0.6456   0.00799   0.00232  -0.0696   0.5097   0.8043
   3.250   0.6697   0.00816   0.00245  -0.0689   0.4886   0.8173
   3.500   0.6936   0.00833   0.00260  -0.0681   0.4676   0.8311
   3.750   0.7172   0.00852   0.00275  -0.0673   0.4466   0.8456
   4.000   0.7401   0.00872   0.00293  -0.0663   0.4256   0.8616
   4.250   0.7626   0.00891   0.00310  -0.0653   0.4041   0.8796
   4.500   0.7842   0.00912   0.00329  -0.0640   0.3837   0.9007
   5.000   0.8353   0.00959   0.00370  -0.0633   0.3408   0.9582
   5.250   0.8692   0.00990   0.00393  -0.0650   0.3181   1.0000
   5.500   0.8918   0.01021   0.00417  -0.0642   0.2982   1.0000
   5.750   0.9144   0.01054   0.00442  -0.0634   0.2799   1.0000
   6.000   0.9368   0.01087   0.00469  -0.0626   0.2599   1.0000
   6.250   0.9588   0.01123   0.00497  -0.0617   0.2409   1.0000
   6.500   0.9800   0.01163   0.00528  -0.0607   0.2204   1.0000
   6.750   1.0002   0.01209   0.00562  -0.0596   0.1965   1.0000
   7.000   1.0200   0.01256   0.00600  -0.0584   0.1734   1.0000
   7.250   1.0398   0.01302   0.00637  -0.0572   0.1548   1.0000
   7.500   1.0592   0.01349   0.00676  -0.0560   0.1381   1.0000
   7.750   1.0777   0.01400   0.00718  -0.0546   0.1192   1.0000
   8.000   1.0953   0.01453   0.00763  -0.0531   0.1020   1.0000
   8.250   1.1116   0.01504   0.00808  -0.0513   0.0885   1.0000
   8.500   1.1271   0.01557   0.00856  -0.0494   0.0759   1.0000
   8.750   1.1416   0.01616   0.00909  -0.0474   0.0633   1.0000
   9.000   1.1556   0.01679   0.00966  -0.0454   0.0515   1.0000
   9.250   1.1693   0.01745   0.01027  -0.0434   0.0413   1.0000
   9.500   1.1844   0.01804   0.01088  -0.0417   0.0351   1.0000
   9.750   1.1969   0.01880   0.01160  -0.0396   0.0267   1.0000
  10.000   1.2079   0.01965   0.01242  -0.0375   0.0186   1.0000
  10.250   1.2172   0.02064   0.01337  -0.0353   0.0115   1.0000
  10.500   1.2293   0.02147   0.01424  -0.0335   0.0097   1.0000
  10.750   1.2403   0.02240   0.01520  -0.0316   0.0083   1.0000
  11.000   1.2513   0.02335   0.01621  -0.0299   0.0075   1.0000
  11.250   1.2632   0.02427   0.01721  -0.0283   0.0071   1.0000
  11.500   1.2740   0.02529   0.01832  -0.0268   0.0068   1.0000
  11.750   1.2846   0.02636   0.01946  -0.0253   0.0065   1.0000
  12.000   1.2935   0.02758   0.02077  -0.0238   0.0062   1.0000
  12.250   1.3019   0.02887   0.02214  -0.0223   0.0059   1.0000
  12.500   1.3093   0.03029   0.02365  -0.0210   0.0058   1.0000
  12.750   1.3150   0.03189   0.02533  -0.0196   0.0056   1.0000
  13.000   1.3196   0.03364   0.02718  -0.0183   0.0055   1.0000
  13.250   1.3204   0.03579   0.02944  -0.0170   0.0053   1.0000
  13.500   1.3229   0.03785   0.03161  -0.0160   0.0052   1.0000
  13.750   1.3262   0.03991   0.03379  -0.0152   0.0052   1.0000
  14.000   1.3282   0.04217   0.03616  -0.0145   0.0051   1.0000
  14.250   1.3284   0.04471   0.03881  -0.0139   0.0050   1.0000
  14.500   1.3278   0.04745   0.04167  -0.0136   0.0050   1.0000
  14.750   1.3279   0.05024   0.04456  -0.0135   0.0048   1.0000
  15.000   1.3256   0.05344   0.04788  -0.0137   0.0048   1.0000
  15.250   1.3214   0.05703   0.05160  -0.0141   0.0048   1.0000
  15.500   1.3188   0.06058   0.05527  -0.0148   0.0047   1.0000
  15.750   1.3128   0.06477   0.05958  -0.0158   0.0046   1.0000
  16.000   1.3075   0.06904   0.06399  -0.0171   0.0045   1.0000
  16.250   1.3031   0.07333   0.06839  -0.0186   0.0044   1.0000
  16.500   1.2943   0.07845   0.07364  -0.0205   0.0044   1.0000
  16.750   1.2876   0.08342   0.07874  -0.0226   0.0043   1.0000
  17.000   1.2786   0.08891   0.08435  -0.0250   0.0043   1.0000
  17.250   1.2676   0.09486   0.09044  -0.0277   0.0043   1.0000
  17.500   1.2563   0.10104   0.09675  -0.0306   0.0043   1.0000
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