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PSU 94-097 (AIAA 2001-2478) (psu94097-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: PSU 94-097 (AIAA 2001-2478) (psu94097-il)
Reynolds number: 1,000,000
Max Cl/Cd: 150.73 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-psu94097-il-1000000.txt
Download as CSV file: xf-psu94097-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: PSU 94-097 (AIAA 2001-2478)                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.250  -0.3117   0.08967   0.08802  -0.0382   0.9306   0.0061
  -8.000  -0.3081   0.08624   0.08454  -0.0396   0.9148   0.0062
  -7.750  -0.3037   0.08264   0.08090  -0.0416   0.9008   0.0064
  -7.500  -0.2989   0.07884   0.07706  -0.0441   0.8874   0.0065
  -7.250  -0.2939   0.07482   0.07301  -0.0474   0.8747   0.0067
  -7.000  -0.2813   0.06965   0.06780  -0.0539   0.8634   0.0070
  -6.750  -0.2635   0.06414   0.06223  -0.0619   0.8534   0.0071
  -6.500  -0.2425   0.05795   0.05595  -0.0709   0.8440   0.0072
  -6.250  -0.2187   0.05114   0.04903  -0.0795   0.8355   0.0072
  -6.000  -0.1940   0.04416   0.04186  -0.0865   0.8281   0.0073
  -5.750  -0.1685   0.03707   0.03452  -0.0918   0.8210   0.0073
  -5.000  -0.0870   0.01464   0.00997  -0.1017   0.8032   0.0049
  -4.750  -0.0573   0.01281   0.00778  -0.1022   0.7977   0.0049
  -4.500  -0.0281   0.01167   0.00647  -0.1026   0.7919   0.0053
  -4.250   0.0008   0.01118   0.00587  -0.1029   0.7866   0.0058
  -4.000   0.0303   0.01062   0.00522  -0.1033   0.7812   0.0064
  -3.750   0.0597   0.01008   0.00456  -0.1036   0.7759   0.0068
  -3.500   0.0892   0.00957   0.00395  -0.1040   0.7710   0.0070
  -3.250   0.1189   0.00917   0.00349  -0.1044   0.7659   0.0072
  -3.000   0.1490   0.00856   0.00276  -0.1049   0.7610   0.0083
  -2.750   0.1788   0.00827   0.00242  -0.1053   0.7563   0.0091
  -2.500   0.2087   0.00800   0.00207  -0.1057   0.7512   0.0100
  -2.250   0.2392   0.00755   0.00168  -0.1062   0.7465   0.0417
  -2.000   0.2690   0.00727   0.00156  -0.1068   0.7417   0.0925
  -1.750   0.2989   0.00694   0.00147  -0.1074   0.7365   0.1722
  -1.500   0.3288   0.00659   0.00141  -0.1082   0.7313   0.2842
  -1.250   0.3587   0.00632   0.00137  -0.1088   0.7260   0.3717
  -1.000   0.3887   0.00596   0.00136  -0.1096   0.7206   0.5085
  -0.750   0.4182   0.00575   0.00136  -0.1101   0.7149   0.6037
  -0.500   0.4475   0.00559   0.00138  -0.1104   0.7082   0.6777
  -0.250   0.4763   0.00552   0.00139  -0.1106   0.7020   0.7344
   0.000   0.5050   0.00541   0.00142  -0.1107   0.6960   0.7837
   0.250   0.5329   0.00536   0.00143  -0.1107   0.6899   0.8258
   0.500   0.5599   0.00529   0.00145  -0.1104   0.6836   0.8671
   0.750   0.5823   0.00517   0.00144  -0.1089   0.6770   0.9272
   1.000   0.6074   0.00507   0.00136  -0.1081   0.6705   1.0000
   1.250   0.6368   0.00513   0.00137  -0.1085   0.6632   1.0000
   1.500   0.6661   0.00518   0.00140  -0.1088   0.6560   1.0000
   1.750   0.6953   0.00526   0.00142  -0.1092   0.6481   1.0000
   2.000   0.7244   0.00532   0.00147  -0.1095   0.6397   1.0000
   2.250   0.7534   0.00540   0.00150  -0.1098   0.6307   1.0000
   2.500   0.7823   0.00548   0.00155  -0.1101   0.6203   1.0000
   2.750   0.8111   0.00556   0.00161  -0.1103   0.6089   1.0000
   3.000   0.8397   0.00567   0.00168  -0.1106   0.5962   1.0000
   3.250   0.8681   0.00580   0.00176  -0.1108   0.5806   1.0000
   3.750   0.9240   0.00613   0.00195  -0.1111   0.5408   1.0000
   4.000   0.9515   0.00637   0.00210  -0.1111   0.5154   1.0000
   4.250   0.9784   0.00665   0.00227  -0.1112   0.4849   1.0000
   4.500   1.0050   0.00699   0.00246  -0.1111   0.4516   1.0000
   4.750   1.0310   0.00738   0.00270  -0.1110   0.4142   1.0000
   5.000   1.0568   0.00780   0.00296  -0.1109   0.3791   1.0000
   5.250   1.0824   0.00822   0.00323  -0.1108   0.3436   1.0000
   5.750   1.1330   0.00908   0.00383  -0.1104   0.2826   1.0000
   6.000   1.1583   0.00949   0.00412  -0.1102   0.2564   1.0000
   6.250   1.1834   0.00991   0.00444  -0.1100   0.2310   1.0000
   6.500   1.2081   0.01034   0.00477  -0.1097   0.2068   1.0000
   6.750   1.2323   0.01081   0.00512  -0.1093   0.1833   1.0000
   7.000   1.2560   0.01132   0.00552  -0.1089   0.1590   1.0000
   7.250   1.2789   0.01189   0.00595  -0.1084   0.1325   1.0000
   7.500   1.3010   0.01252   0.00642  -0.1077   0.1062   1.0000
   7.750   1.3236   0.01306   0.00687  -0.1071   0.0872   1.0000
   8.000   1.3454   0.01367   0.00738  -0.1064   0.0702   1.0000
   8.250   1.3667   0.01429   0.00791  -0.1056   0.0536   1.0000
   8.500   1.3870   0.01498   0.00852  -0.1047   0.0391   1.0000
   8.750   1.4072   0.01565   0.00913  -0.1037   0.0284   1.0000
   9.000   1.4273   0.01629   0.00974  -0.1028   0.0209   1.0000
   9.250   1.4473   0.01689   0.01034  -0.1018   0.0159   1.0000
   9.500   1.4664   0.01755   0.01098  -0.1006   0.0117   1.0000
   9.750   1.4837   0.01831   0.01173  -0.0992   0.0071   1.0000
  10.000   1.4939   0.01962   0.01302  -0.0967   0.0015   1.0000
  10.250   1.5071   0.02050   0.01400  -0.0946   0.0010   1.0000
  10.500   1.5155   0.02154   0.01517  -0.0917   0.0009   1.0000
  10.750   1.5252   0.02256   0.01629  -0.0892   0.0008   1.0000
  11.000   1.5354   0.02359   0.01741  -0.0870   0.0008   1.0000
  11.250   1.5445   0.02475   0.01867  -0.0848   0.0007   1.0000
  11.500   1.5525   0.02604   0.02006  -0.0827   0.0007   1.0000
  11.750   1.5588   0.02752   0.02166  -0.0805   0.0007   1.0000
  12.000   1.5643   0.02912   0.02337  -0.0784   0.0007   1.0000
  12.250   1.5685   0.03090   0.02528  -0.0764   0.0007   1.0000
  12.500   1.5711   0.03288   0.02738  -0.0745   0.0007   1.0000
  12.750   1.5723   0.03506   0.02970  -0.0727   0.0006   1.0000
  13.000   1.5724   0.03743   0.03221  -0.0711   0.0006   1.0000
  13.250   1.5704   0.04010   0.03501  -0.0695   0.0006   1.0000
  13.500   1.5671   0.04301   0.03807  -0.0682   0.0006   1.0000
  13.750   1.5624   0.04613   0.04133  -0.0670   0.0006   1.0000
  14.000   1.5558   0.04962   0.04496  -0.0661   0.0006   1.0000
  14.250   1.5487   0.05327   0.04876  -0.0654   0.0006   1.0000
  14.500   1.5398   0.05730   0.05293  -0.0650   0.0006   1.0000
  14.750   1.5298   0.06172   0.05750  -0.0650   0.0006   1.0000
  15.000   1.5190   0.06644   0.06238  -0.0653   0.0006   1.0000
  15.250   1.5063   0.07166   0.06776  -0.0661   0.0006   1.0000
  15.500   1.4928   0.07729   0.07354  -0.0672   0.0006   1.0000
  15.750   1.4787   0.08325   0.07965  -0.0688   0.0006   1.0000
  16.000   1.4633   0.08966   0.08621  -0.0708   0.0006   1.0000
  16.250   1.4466   0.09655   0.09326  -0.0732   0.0007   1.0000
  16.500   1.4314   0.10341   0.10026  -0.0758   0.0007   1.0000
  16.750   1.4139   0.11086   0.10785  -0.0789   0.0007   1.0000
  17.000   1.3975   0.11833   0.11547  -0.0822   0.0007   1.0000
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