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PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: PSU-90-125WL (psu-90-125wl-il)
Reynolds number: 200,000
Max Cl/Cd: 75.81 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-psu-90-125wl-il-200000.txt
Download as CSV file: xf-psu-90-125wl-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.4169   0.09961   0.09605  -0.0486   1.0000   0.0665
 -10.250  -0.4442   0.09218   0.08873  -0.0564   1.0000   0.0671
 -10.000  -0.4524   0.08619   0.08281  -0.0570   1.0000   0.0680
  -9.750  -0.4361   0.08563   0.08225  -0.0525   1.0000   0.0691
  -9.500  -0.4246   0.08472   0.08135  -0.0498   1.0000   0.0710
  -9.250  -0.4283   0.08163   0.07830  -0.0499   1.0000   0.0727
  -9.000  -0.4412   0.07767   0.07442  -0.0509   1.0000   0.0740
  -8.750  -0.4711   0.07275   0.06965  -0.0522   1.0000   0.0735
  -8.500  -0.5305   0.07065   0.06767  -0.0480   1.0000   0.0721
  -8.250  -0.5465   0.06623   0.06318  -0.0511   0.9955   0.0730
  -8.000  -0.5637   0.05670   0.05276  -0.0640   0.9800   0.0810
  -7.750  -0.5636   0.03888   0.03384  -0.0656   0.9732   0.0420
  -7.500  -0.5453   0.03442   0.02890  -0.0664   0.9670   0.0402
  -7.250  -0.5239   0.02924   0.02277  -0.0666   0.9612   0.0368
  -7.000  -0.4905   0.02678   0.01987  -0.0682   0.9584   0.0362
  -6.750  -0.4649   0.02493   0.01778  -0.0682   0.9530   0.0364
  -6.500  -0.4346   0.02325   0.01594  -0.0691   0.9486   0.0370
  -6.250  -0.3998   0.02187   0.01447  -0.0707   0.9458   0.0383
  -6.000  -0.3623   0.02082   0.01334  -0.0729   0.9438   0.0408
  -5.750  -0.3382   0.01997   0.01241  -0.0723   0.9372   0.0424
  -5.500  -0.3049   0.01902   0.01136  -0.0735   0.9335   0.0441
  -5.250  -0.2708   0.01763   0.01001  -0.0752   0.9309   0.0476
  -5.000  -0.2334   0.01679   0.00912  -0.0772   0.9288   0.0544
  -4.750  -0.2144   0.01604   0.00842  -0.0759   0.9209   0.0695
  -4.500  -0.1862   0.01451   0.00755  -0.0768   0.9170   0.1847
  -4.250  -0.1521   0.01376   0.00712  -0.0785   0.9144   0.2718
  -4.000  -0.1320   0.01334   0.00700  -0.0774   0.9071   0.3482
  -3.750  -0.1039   0.01277   0.00681  -0.0777   0.9027   0.4447
  -3.500  -0.0722   0.01237   0.00673  -0.0783   0.8996   0.5351
  -3.250  -0.0503   0.01237   0.00683  -0.0770   0.8926   0.5884
  -3.000  -0.0213   0.01231   0.00681  -0.0768   0.8878   0.6297
  -2.750   0.0113   0.01223   0.00672  -0.0772   0.8844   0.6635
  -2.500   0.0338   0.01232   0.00682  -0.0759   0.8773   0.6876
  -2.250   0.0625   0.01230   0.00676  -0.0756   0.8722   0.7106
  -2.000   0.0942   0.01223   0.00666  -0.0758   0.8686   0.7315
  -1.750   0.1152   0.01234   0.00678  -0.0742   0.8606   0.7490
  -1.500   0.1441   0.01228   0.00670  -0.0739   0.8557   0.7664
  -1.250   0.1699   0.01230   0.00670  -0.0731   0.8499   0.7825
  -1.000   0.1945   0.01230   0.00670  -0.0720   0.8430   0.7979
  -0.750   0.2239   0.01222   0.00658  -0.0718   0.8385   0.8125
  -0.500   0.2453   0.01227   0.00665  -0.0702   0.8303   0.8267
  -0.250   0.2730   0.01218   0.00653  -0.0696   0.8246   0.8406
   0.000   0.2959   0.01219   0.00655  -0.0683   0.8170   0.8547
   0.250   0.3217   0.01211   0.00645  -0.0674   0.8104   0.8687
   0.500   0.3453   0.01209   0.00643  -0.0661   0.8030   0.8830
   0.750   0.3702   0.01201   0.00635  -0.0650   0.7956   0.8971
   1.000   0.3954   0.01196   0.00630  -0.0640   0.7882   0.9113
   1.250   0.4233   0.01187   0.00621  -0.0635   0.7803   0.9255
   1.500   0.4549   0.01182   0.00616  -0.0640   0.7722   0.9389
   1.750   0.4927   0.01172   0.00603  -0.0656   0.7641   0.9504
   2.000   0.5314   0.01167   0.00598  -0.0678   0.7542   0.9615
   2.250   0.5738   0.01155   0.00582  -0.0705   0.7460   0.9715
   2.500   0.6185   0.01147   0.00575  -0.0740   0.7346   0.9795
   2.750   0.6628   0.01137   0.00566  -0.0775   0.7227   0.9881
   3.000   0.7069   0.01125   0.00554  -0.0809   0.7102   0.9975
   3.250   0.7285   0.01117   0.00544  -0.0801   0.6979   1.0000
   3.500   0.7427   0.01113   0.00536  -0.0776   0.6851   1.0000
   3.750   0.7595   0.01113   0.00533  -0.0756   0.6712   1.0000
   4.000   0.7787   0.01115   0.00533  -0.0739   0.6553   1.0000
   4.250   0.7997   0.01120   0.00536  -0.0725   0.6377   1.0000
   4.500   0.8219   0.01126   0.00539  -0.0714   0.6185   1.0000
   4.750   0.8449   0.01136   0.00543  -0.0703   0.5983   1.0000
   5.000   0.8669   0.01152   0.00554  -0.0691   0.5755   1.0000
   5.250   0.8891   0.01174   0.00565  -0.0680   0.5521   1.0000
   5.500   0.9105   0.01201   0.00587  -0.0667   0.5271   1.0000
   5.750   0.9315   0.01234   0.00610  -0.0655   0.5020   1.0000
   6.000   0.9520   0.01271   0.00637  -0.0641   0.4769   1.0000
   6.250   0.9719   0.01309   0.00668  -0.0627   0.4512   1.0000
   6.500   0.9912   0.01351   0.00704  -0.0613   0.4254   1.0000
   6.750   1.0099   0.01397   0.00741  -0.0597   0.4003   1.0000
   7.000   1.0278   0.01446   0.00781  -0.0581   0.3747   1.0000
   7.250   1.0454   0.01495   0.00825  -0.0564   0.3494   1.0000
   7.500   1.0620   0.01550   0.00873  -0.0546   0.3249   1.0000
   7.750   1.0778   0.01608   0.00924  -0.0527   0.3008   1.0000
   8.000   1.0933   0.01667   0.00977  -0.0509   0.2773   1.0000
   8.250   1.1071   0.01733   0.01035  -0.0487   0.2554   1.0000
   8.500   1.1204   0.01796   0.01095  -0.0465   0.2342   1.0000
   8.750   1.1315   0.01866   0.01160  -0.0440   0.2142   1.0000
   9.000   1.1417   0.01944   0.01231  -0.0415   0.1948   1.0000
   9.250   1.1528   0.02021   0.01304  -0.0392   0.1746   1.0000
   9.500   1.1617   0.02111   0.01384  -0.0368   0.1551   1.0000
   9.750   1.1723   0.02199   0.01468  -0.0347   0.1360   1.0000
  10.000   1.1825   0.02294   0.01560  -0.0327   0.1203   1.0000
  10.250   1.1919   0.02398   0.01665  -0.0307   0.1066   1.0000
  10.500   1.2007   0.02510   0.01776  -0.0288   0.0937   1.0000
  10.750   1.2086   0.02634   0.01898  -0.0269   0.0804   1.0000
  11.000   1.2145   0.02777   0.02038  -0.0249   0.0667   1.0000
  11.250   1.2151   0.02966   0.02218  -0.0228   0.0528   1.0000
  11.500   1.2123   0.03196   0.02445  -0.0204   0.0409   1.0000
  11.750   1.2109   0.03420   0.02672  -0.0185   0.0349   1.0000
  12.000   1.2096   0.03657   0.02917  -0.0167   0.0319   1.0000
  12.250   1.2113   0.03874   0.03144  -0.0153   0.0294   1.0000
  12.500   1.2098   0.04128   0.03402  -0.0140   0.0275   1.0000
  12.750   1.2067   0.04415   0.03694  -0.0127   0.0262   1.0000
  13.000   1.2115   0.04632   0.03927  -0.0119   0.0251   1.0000
  13.250   1.2153   0.04862   0.04169  -0.0111   0.0241   1.0000
  13.500   1.2179   0.05105   0.04422  -0.0106   0.0228   1.0000
  13.750   1.2199   0.05363   0.04685  -0.0103   0.0219   1.0000
  14.000   1.2218   0.05639   0.04966  -0.0098   0.0211   1.0000
  14.250   1.2271   0.05920   0.05255  -0.0089   0.0205   1.0000
  14.500   1.2299   0.06204   0.05557  -0.0087   0.0203   1.0000
  14.750   1.2311   0.06516   0.05888  -0.0087   0.0200   1.0000
  15.000   1.2308   0.06856   0.06249  -0.0088   0.0197   1.0000
  15.250   1.2285   0.07231   0.06644  -0.0092   0.0196   1.0000
  15.500   1.2223   0.07668   0.07105  -0.0101   0.0193   1.0000
  15.750   1.2155   0.08126   0.07585  -0.0113   0.0192   1.0000
  16.000   1.2060   0.08641   0.08122  -0.0130   0.0192   1.0000
  16.250   1.1934   0.09222   0.08727  -0.0153   0.0191   1.0000
  16.500   1.1801   0.09837   0.09363  -0.0182   0.0192   1.0000
  16.750   1.1635   0.10538   0.10087  -0.0218   0.0192   1.0000
  17.000   1.1457   0.11296   0.10867  -0.0260   0.0193   1.0000
  17.250   1.1274   0.12099   0.11690  -0.0308   0.0195   1.0000
  17.500   1.1075   0.12977   0.12587  -0.0363   0.0197   1.0000
  17.750   1.0845   0.13978   0.13605  -0.0429   0.0199   1.0000
  18.000   1.0623   0.15013   0.14655  -0.0496   0.0202   1.0000
  18.250   1.0376   0.16175   0.15829  -0.0571   0.0205   1.0000
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