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PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: PSU-90-125WL (psu-90-125wl-il)
Reynolds number: 100,000
Max Cl/Cd: 53.25 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-psu-90-125wl-il-100000-n5.txt
Download as CSV file: xf-psu-90-125wl-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.4388   0.09298   0.08782  -0.0492   1.0000   0.0297
 -10.500  -0.4532   0.08579   0.08072  -0.0525   1.0000   0.0291
 -10.250  -0.5305   0.06516   0.06000  -0.0672   1.0000   0.0272
 -10.000  -0.5723   0.05922   0.05392  -0.0695   1.0000   0.0267
  -9.750  -0.6040   0.05662   0.05123  -0.0667   1.0000   0.0265
  -9.500  -0.6283   0.05436   0.04887  -0.0629   1.0000   0.0264
  -9.250  -0.6478   0.05234   0.04669  -0.0589   1.0000   0.0263
  -8.750  -0.6554   0.04605   0.03983  -0.0568   0.9934   0.0263
  -8.500  -0.6391   0.04208   0.03540  -0.0588   0.9859   0.0265
  -8.250  -0.6194   0.03883   0.03177  -0.0603   0.9790   0.0268
  -8.000  -0.5963   0.03610   0.02871  -0.0616   0.9728   0.0272
  -7.750  -0.5730   0.03383   0.02614  -0.0624   0.9667   0.0277
  -7.500  -0.5471   0.03201   0.02407  -0.0633   0.9607   0.0286
  -7.250  -0.5168   0.03038   0.02218  -0.0649   0.9567   0.0304
  -7.000  -0.4933   0.02891   0.02043  -0.0648   0.9495   0.0318
  -6.750  -0.4632   0.02731   0.01857  -0.0657   0.9453   0.0328
  -6.500  -0.4332   0.02594   0.01701  -0.0665   0.9412   0.0336
  -6.250  -0.4087   0.02465   0.01565  -0.0664   0.9349   0.0347
  -6.000  -0.3785   0.02350   0.01446  -0.0675   0.9309   0.0365
  -5.750  -0.3498   0.02257   0.01341  -0.0682   0.9264   0.0388
  -5.500  -0.3245   0.02182   0.01253  -0.0680   0.9201   0.0423
  -5.250  -0.2944   0.02092   0.01161  -0.0690   0.9160   0.0489
  -5.000  -0.2677   0.02009   0.01076  -0.0692   0.9108   0.0596
  -4.750  -0.2427   0.01922   0.01000  -0.0691   0.9048   0.0869
  -4.500  -0.2127   0.01840   0.00940  -0.0700   0.9009   0.1409
  -4.250  -0.1889   0.01764   0.00906  -0.0700   0.8950   0.2245
  -4.000  -0.1647   0.01691   0.00879  -0.0699   0.8893   0.3207
  -3.750  -0.1353   0.01635   0.00851  -0.0704   0.8854   0.4047
  -3.500  -0.1127   0.01607   0.00844  -0.0695   0.8789   0.4694
  -3.250  -0.0860   0.01587   0.00840  -0.0690   0.8737   0.5306
  -3.000  -0.0548   0.01574   0.00830  -0.0693   0.8700   0.5818
  -2.750  -0.0327   0.01578   0.00833  -0.0679   0.8628   0.6175
  -2.500  -0.0042   0.01575   0.00826  -0.0676   0.8578   0.6501
  -2.250   0.0260   0.01570   0.00816  -0.0677   0.8537   0.6780
  -2.000   0.0481   0.01577   0.00818  -0.0663   0.8461   0.7018
  -1.750   0.0777   0.01572   0.00810  -0.0662   0.8414   0.7234
  -1.500   0.1021   0.01575   0.00809  -0.0652   0.8349   0.7431
  -1.250   0.1288   0.01574   0.00802  -0.0646   0.8287   0.7618
  -1.000   0.1596   0.01566   0.00789  -0.0647   0.8244   0.7792
  -0.750   0.1806   0.01573   0.00796  -0.0631   0.8160   0.7954
  -0.500   0.2102   0.01565   0.00783  -0.0630   0.8110   0.8114
  -0.250   0.2326   0.01570   0.00787  -0.0617   0.8030   0.8272
   0.000   0.2611   0.01563   0.00777  -0.0613   0.7971   0.8427
   0.250   0.2856   0.01563   0.00777  -0.0604   0.7894   0.8583
   0.500   0.3142   0.01557   0.00769  -0.0601   0.7827   0.8737
   0.750   0.3414   0.01555   0.00767  -0.0597   0.7749   0.8896
   1.000   0.3732   0.01547   0.00758  -0.0602   0.7676   0.9048
   1.250   0.4047   0.01546   0.00757  -0.0607   0.7590   0.9205
   1.500   0.4424   0.01536   0.00746  -0.0624   0.7516   0.9346
   1.750   0.4781   0.01536   0.00747  -0.0641   0.7417   0.9497
   2.000   0.5184   0.01527   0.00737  -0.0665   0.7333   0.9632
   2.250   0.5575   0.01522   0.00734  -0.0689   0.7229   0.9776
   2.500   0.5965   0.01518   0.00732  -0.0713   0.7112   0.9931
   2.750   0.6211   0.01518   0.00731  -0.0710   0.6996   1.0000
   3.000   0.6402   0.01519   0.00731  -0.0694   0.6879   1.0000
   3.250   0.6618   0.01521   0.00730  -0.0682   0.6756   1.0000
   3.500   0.6836   0.01526   0.00734  -0.0670   0.6620   1.0000
   3.750   0.7059   0.01532   0.00739  -0.0660   0.6471   1.0000
   4.000   0.7280   0.01541   0.00750  -0.0649   0.6307   1.0000
   4.250   0.7507   0.01550   0.00760  -0.0638   0.6131   1.0000
   4.500   0.7741   0.01560   0.00767  -0.0629   0.5945   1.0000
   4.750   0.7981   0.01570   0.00773  -0.0620   0.5752   1.0000
   5.000   0.8209   0.01588   0.00790  -0.0610   0.5539   1.0000
   5.250   0.8440   0.01610   0.00805  -0.0600   0.5322   1.0000
   5.500   0.8660   0.01637   0.00828  -0.0589   0.5093   1.0000
   5.750   0.8878   0.01669   0.00852  -0.0577   0.4864   1.0000
   6.000   0.9084   0.01706   0.00887  -0.0565   0.4625   1.0000
   6.250   0.9287   0.01747   0.00922  -0.0552   0.4390   1.0000
   6.500   0.9482   0.01792   0.00962  -0.0538   0.4153   1.0000
   6.750   0.9671   0.01841   0.01006  -0.0524   0.3919   1.0000
   7.000   0.9852   0.01894   0.01053  -0.0508   0.3691   1.0000
   7.250   1.0029   0.01948   0.01108  -0.0493   0.3459   1.0000
   7.500   1.0194   0.02009   0.01162  -0.0476   0.3241   1.0000
   7.750   1.0356   0.02070   0.01223  -0.0459   0.3018   1.0000
   8.000   1.0504   0.02139   0.01286  -0.0440   0.2809   1.0000
   8.250   1.0649   0.02208   0.01355  -0.0422   0.2599   1.0000
   8.500   1.0771   0.02281   0.01427  -0.0400   0.2406   1.0000
   8.750   1.0882   0.02361   0.01504  -0.0377   0.2227   1.0000
   9.000   1.1000   0.02443   0.01588  -0.0356   0.2048   1.0000
   9.250   1.1110   0.02532   0.01677  -0.0335   0.1881   1.0000
   9.500   1.1213   0.02629   0.01775  -0.0314   0.1722   1.0000
   9.750   1.1311   0.02733   0.01880  -0.0294   0.1577   1.0000
  10.000   1.1404   0.02844   0.01993  -0.0275   0.1441   1.0000
  10.250   1.1491   0.02963   0.02119  -0.0256   0.1318   1.0000
  10.500   1.1566   0.03092   0.02251  -0.0238   0.1192   1.0000
  10.750   1.1630   0.03233   0.02391  -0.0221   0.1048   1.0000
  11.000   1.1684   0.03386   0.02542  -0.0206   0.0902   1.0000
  11.250   1.1731   0.03552   0.02705  -0.0191   0.0763   1.0000
  11.500   1.1776   0.03728   0.02882  -0.0178   0.0650   1.0000
  11.750   1.1813   0.03918   0.03079  -0.0165   0.0564   1.0000
  12.000   1.1822   0.04140   0.03303  -0.0152   0.0489   1.0000
  12.250   1.1825   0.04375   0.03548  -0.0142   0.0428   1.0000
  12.500   1.1805   0.04643   0.03827  -0.0132   0.0382   1.0000
  12.750   1.1779   0.04927   0.04123  -0.0125   0.0342   1.0000
  13.000   1.1713   0.05264   0.04463  -0.0120   0.0316   1.0000
  13.250   1.1680   0.05582   0.04801  -0.0117   0.0286   1.0000
  13.500   1.1636   0.05926   0.05158  -0.0118   0.0266   1.0000
  13.750   1.1569   0.06311   0.05553  -0.0123   0.0252   1.0000
  14.000   1.1490   0.06731   0.05982  -0.0131   0.0242   1.0000
  14.250   1.1444   0.07130   0.06402  -0.0139   0.0230   1.0000
  14.500   1.1387   0.07559   0.06849  -0.0151   0.0220   1.0000
  14.750   1.1328   0.08007   0.07313  -0.0164   0.0213   1.0000
  15.000   1.1264   0.08478   0.07799  -0.0181   0.0207   1.0000
  15.250   1.1198   0.08967   0.08302  -0.0199   0.0202   1.0000
  15.500   1.1134   0.09466   0.08816  -0.0220   0.0198   1.0000
  15.750   1.1067   0.09984   0.09346  -0.0242   0.0195   1.0000
  16.000   1.0998   0.10512   0.09887  -0.0266   0.0191   1.0000
  16.250   1.0938   0.11031   0.10416  -0.0290   0.0188   1.0000
  16.500   1.0882   0.11553   0.10949  -0.0314   0.0186   1.0000
  16.750   1.0808   0.12142   0.11557  -0.0344   0.0184   1.0000
  17.000   1.0721   0.12776   0.12210  -0.0378   0.0182   1.0000
  17.250   1.0622   0.13459   0.12911  -0.0416   0.0181   1.0000
  17.500   1.0504   0.14213   0.13682  -0.0460   0.0181   1.0000
  17.750   1.0360   0.15068   0.14555  -0.0512   0.0181   1.0000
  18.000   1.0207   0.15992   0.15494  -0.0568   0.0182   1.0000
  18.250   1.0030   0.17037   0.16552  -0.0631   0.0183   1.0000
  18.500   0.9811   0.18307   0.17831  -0.0703   0.0185   1.0000
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