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PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=50,000 Ncrit=9


Details Polar file
Airfoil: PSU-90-125WL (psu-90-125wl-il)
Reynolds number: 50,000
Max Cl/Cd: 32.22 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-psu-90-125wl-il-50000.txt
Download as CSV file: xf-psu-90-125wl-il-50000.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 =     0.050 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.3624   0.10421   0.09737  -0.0271   1.0000   0.3032
  -8.750  -0.3610   0.10164   0.09487  -0.0261   1.0000   0.3145
  -8.500  -0.3566   0.09816   0.09146  -0.0254   1.0000   0.3201
  -8.250  -0.3553   0.09526   0.08863  -0.0245   1.0000   0.3259
  -8.000  -0.3723   0.09340   0.08693  -0.0232   1.0000   0.3333
  -7.500  -0.5375   0.07262   0.06662  -0.0401   1.0000   0.1438
  -7.250  -0.5747   0.06710   0.06091  -0.0403   1.0000   0.1337
  -7.000  -0.5826   0.06300   0.05671  -0.0390   1.0000   0.1287
  -6.750  -0.6004   0.05718   0.05027  -0.0389   1.0000   0.1204
  -6.500  -0.5959   0.05349   0.04639  -0.0377   1.0000   0.1180
  -6.250  -0.5907   0.04965   0.04217  -0.0368   1.0000   0.1160
  -6.000  -0.5817   0.04615   0.03820  -0.0359   1.0000   0.1159
  -5.750  -0.5688   0.04304   0.03462  -0.0350   1.0000   0.1167
  -5.500  -0.5526   0.04016   0.03123  -0.0342   1.0000   0.1182
  -5.250  -0.5333   0.03753   0.02807  -0.0333   1.0000   0.1196
  -5.000  -0.5120   0.03528   0.02521  -0.0324   1.0000   0.1219
  -4.750  -0.4912   0.03326   0.02325  -0.0315   1.0000   0.1278
  -4.500  -0.4696   0.03168   0.02137  -0.0305   1.0000   0.1378
  -4.250  -0.4481   0.03016   0.01979  -0.0293   1.0000   0.1523
  -4.000  -0.4272   0.02866   0.01844  -0.0280   1.0000   0.1779
  -3.750  -0.4073   0.02693   0.01711  -0.0267   1.0000   0.2402
  -3.500  -0.3912   0.02504   0.01633  -0.0251   1.0000   0.3793
  -3.250  -0.3805   0.02421   0.01653  -0.0209   1.0000   0.5311
  -3.000  -0.3737   0.02444   0.01714  -0.0151   1.0000   0.6358
  -2.750  -0.3692   0.02476   0.01761  -0.0087   1.0000   0.7103
  -2.500  -0.3663   0.02494   0.01783  -0.0020   1.0000   0.7729
  -2.250  -0.3638   0.02496   0.01787   0.0047   1.0000   0.8315
  -2.000  -0.3492   0.02506   0.01790   0.0092   1.0000   0.8986
  -1.750  -0.1613   0.02747   0.01928  -0.0183   1.0000   0.9951
  -1.500  -0.1616   0.02678   0.01846  -0.0173   1.0000   1.0000
  -1.250  -0.1742   0.02596   0.01756  -0.0136   1.0000   1.0000
  -1.000  -0.1800   0.02534   0.01681  -0.0108   1.0000   1.0000
  -0.750  -0.1726   0.02516   0.01643  -0.0098   1.0000   1.0000
  -0.500  -0.1576   0.02530   0.01634  -0.0099   1.0000   1.0000
  -0.250  -0.1397   0.02562   0.01642  -0.0102   1.0000   1.0000
   0.000  -0.1209   0.02606   0.01665  -0.0106   1.0000   1.0000
   0.250  -0.1018   0.02658   0.01699  -0.0110   1.0000   1.0000
   0.500  -0.0766   0.02737   0.01760  -0.0125   0.9973   1.0000
   0.750  -0.0244   0.02911   0.01910  -0.0189   0.9831   1.0000
   1.000   0.0188   0.03039   0.02023  -0.0235   0.9686   1.0000
   1.250   0.0597   0.03162   0.02131  -0.0275   0.9542   1.0000
   1.500   0.0988   0.03277   0.02235  -0.0311   0.9395   1.0000
   1.750   0.1365   0.03387   0.02336  -0.0343   0.9246   1.0000
   2.000   0.1729   0.03493   0.02435  -0.0371   0.9092   1.0000
   2.250   0.2082   0.03596   0.02533  -0.0397   0.8937   1.0000
   2.500   0.2429   0.03696   0.02629  -0.0419   0.8777   1.0000
   2.750   0.2767   0.03793   0.02724  -0.0440   0.8616   1.0000
   3.000   0.3101   0.03888   0.02819  -0.0458   0.8452   1.0000
   3.250   0.3433   0.03979   0.02912  -0.0475   0.8288   1.0000
   3.500   0.3774   0.04066   0.03001  -0.0491   0.8121   1.0000
   3.750   0.4123   0.04146   0.03085  -0.0507   0.7954   1.0000
   4.000   0.4484   0.04218   0.03164  -0.0522   0.7788   1.0000
   4.250   0.4857   0.04278   0.03231  -0.0537   0.7624   1.0000
   4.500   0.5105   0.04354   0.03314  -0.0536   0.7445   1.0000
   4.750   0.5344   0.04430   0.03399  -0.0534   0.7262   1.0000
   5.000   0.5642   0.04485   0.03464  -0.0536   0.7084   1.0000
   5.250   0.5985   0.04514   0.03504  -0.0540   0.6910   1.0000
   5.500   0.6368   0.04512   0.03518  -0.0545   0.6741   1.0000
   5.750   0.6795   0.04464   0.03487  -0.0551   0.6577   1.0000
   6.000   0.7039   0.04496   0.03531  -0.0540   0.6387   1.0000
   6.250   0.7306   0.04505   0.03557  -0.0530   0.6197   1.0000
   6.500   0.7775   0.04357   0.03431  -0.0528   0.6027   1.0000
   6.750   0.8424   0.04072   0.03177  -0.0536   0.5858   1.0000
   7.000   0.9160   0.03706   0.02837  -0.0549   0.5668   1.0000
   7.250   0.9485   0.03628   0.02776  -0.0535   0.5427   1.0000
   7.500   0.9944   0.03474   0.02634  -0.0531   0.5162   1.0000
   7.750   1.0339   0.03384   0.02547  -0.0524   0.4869   1.0000
   8.000   1.0649   0.03367   0.02530  -0.0512   0.4566   1.0000
   8.250   1.0908   0.03396   0.02555  -0.0496   0.4262   1.0000
   8.500   1.1133   0.03455   0.02608  -0.0479   0.3961   1.0000
   8.750   1.1336   0.03539   0.02686  -0.0460   0.3671   1.0000
   9.000   1.1525   0.03637   0.02779  -0.0441   0.3388   1.0000
   9.250   1.1716   0.03748   0.02878  -0.0423   0.3113   1.0000
   9.500   1.1862   0.03885   0.03014  -0.0402   0.2860   1.0000
   9.750   1.1962   0.04049   0.03183  -0.0376   0.2632   1.0000
  10.000   1.2162   0.04198   0.03312  -0.0363   0.2390   1.0000
  10.250   1.2204   0.04403   0.03537  -0.0333   0.2204   1.0000
  10.500   1.2289   0.04596   0.03738  -0.0308   0.2013   1.0000
  10.750   1.2446   0.04798   0.03922  -0.0292   0.1810   1.0000
  11.000   1.2461   0.05025   0.04163  -0.0262   0.1658   1.0000
  11.250   1.2464   0.05249   0.04396  -0.0233   0.1515   1.0000
  11.500   1.2469   0.05480   0.04629  -0.0206   0.1381   1.0000
  11.750   1.2494   0.05719   0.04865  -0.0182   0.1256   1.0000
  12.000   1.2278   0.06034   0.05226  -0.0139   0.1226   1.0000
  12.250   1.2342   0.06312   0.05495  -0.0123   0.1120   1.0000
  12.500   1.2099   0.06689   0.05910  -0.0092   0.1106   1.0000
  12.750   1.1851   0.07119   0.06373  -0.0072   0.1097   1.0000
  13.000   1.1588   0.07609   0.06892  -0.0062   0.1095   1.0000
  13.250   1.1314   0.08174   0.07481  -0.0064   0.1101   1.0000
  13.500   1.1021   0.08824   0.08150  -0.0078   0.1110   1.0000
  13.750   1.0741   0.09543   0.08884  -0.0101   0.1121   1.0000
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