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PSU 94-097 (AIAA 2001-2478) (psu94097-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: PSU 94-097 (AIAA 2001-2478) (psu94097-il)
Reynolds number: 200,000
Max Cl/Cd: 86.75 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-psu94097-il-200000-n5.txt
Download as CSV file: xf-psu94097-il-200000-n5.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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.3249   0.09946   0.09607  -0.0373   1.0000   0.0171
  -8.500  -0.3207   0.09621   0.09287  -0.0386   1.0000   0.0172
  -8.250  -0.3187   0.09309   0.08981  -0.0397   1.0000   0.0172
  -8.000  -0.3063   0.08863   0.08536  -0.0445   0.9842   0.0172
  -7.750  -0.2940   0.08336   0.08010  -0.0508   0.9689   0.0169
  -7.500  -0.2818   0.07765   0.07435  -0.0550   0.9552   0.0108
  -7.250  -0.2712   0.07387   0.07056  -0.0588   0.9422   0.0104
  -7.000  -0.2586   0.06935   0.06602  -0.0643   0.9295   0.0101
  -6.750  -0.2444   0.06417   0.06081  -0.0711   0.9173   0.0098
  -6.500  -0.2273   0.05824   0.05477  -0.0789   0.9062   0.0095
  -6.250  -0.2075   0.05165   0.04803  -0.0867   0.8967   0.0091
  -6.000  -0.1854   0.04459   0.04072  -0.0934   0.8877   0.0088
  -5.750  -0.1613   0.03739   0.03311  -0.0986   0.8796   0.0086
  -5.500  -0.1356   0.03163   0.02684  -0.1017   0.8728   0.0088
  -5.250  -0.1080   0.02740   0.02204  -0.1036   0.8659   0.0100
  -5.000  -0.0788   0.02417   0.01809  -0.1046   0.8598   0.0110
  -4.750  -0.0504   0.02172   0.01512  -0.1052   0.8538   0.0110
  -4.500  -0.0219   0.01966   0.01266  -0.1056   0.8475   0.0111
  -4.250   0.0064   0.01785   0.01051  -0.1058   0.8424   0.0113
  -4.000   0.0348   0.01650   0.00897  -0.1061   0.8360   0.0117
  -3.750   0.0630   0.01550   0.00780  -0.1061   0.8307   0.0122
  -3.500   0.0917   0.01470   0.00689  -0.1064   0.8249   0.0131
  -3.250   0.1206   0.01401   0.00608  -0.1066   0.8191   0.0146
  -3.000   0.1497   0.01340   0.00532  -0.1068   0.8144   0.0177
  -2.750   0.1791   0.01288   0.00478  -0.1072   0.8083   0.0273
  -2.500   0.2085   0.01228   0.00428  -0.1076   0.8032   0.0669
  -2.250   0.2376   0.01176   0.00402  -0.1082   0.7982   0.1453
  -2.000   0.2666   0.01128   0.00386  -0.1089   0.7924   0.2480
  -1.750   0.2955   0.01083   0.00373  -0.1094   0.7878   0.3664
  -1.500   0.3237   0.01038   0.00370  -0.1097   0.7823   0.5084
  -1.250   0.3506   0.01008   0.00371  -0.1094   0.7769   0.6285
  -1.000   0.3758   0.00990   0.00369  -0.1085   0.7723   0.7141
  -0.750   0.4001   0.00977   0.00368  -0.1074   0.7662   0.7780
  -0.500   0.4225   0.00966   0.00362  -0.1058   0.7610   0.8388
  -0.250   0.4429   0.00949   0.00351  -0.1036   0.7554   0.9162
   0.000   0.4739   0.00941   0.00337  -0.1041   0.7492   1.0000
   0.250   0.5032   0.00949   0.00331  -0.1044   0.7439   1.0000
   0.500   0.5322   0.00957   0.00332  -0.1048   0.7367   1.0000
   0.750   0.5612   0.00965   0.00328  -0.1050   0.7308   1.0000
   1.000   0.5900   0.00973   0.00332  -0.1053   0.7228   1.0000
   1.250   0.6186   0.00981   0.00330  -0.1054   0.7155   1.0000
   1.500   0.6470   0.00989   0.00333  -0.1055   0.7064   1.0000
   1.750   0.6754   0.00998   0.00337  -0.1057   0.6981   1.0000
   2.000   0.7038   0.01007   0.00341  -0.1058   0.6897   1.0000
   2.250   0.7320   0.01016   0.00349  -0.1059   0.6801   1.0000
   2.500   0.7601   0.01026   0.00355  -0.1059   0.6708   1.0000
   2.750   0.7881   0.01036   0.00361  -0.1060   0.6608   1.0000
   3.000   0.8159   0.01046   0.00374  -0.1060   0.6495   1.0000
   3.250   0.8437   0.01057   0.00385  -0.1060   0.6378   1.0000
   3.500   0.8712   0.01069   0.00396  -0.1060   0.6251   1.0000
   3.750   0.8986   0.01082   0.00409  -0.1059   0.6109   1.0000
   4.000   0.9257   0.01097   0.00424  -0.1058   0.5950   1.0000
   4.250   0.9524   0.01114   0.00438  -0.1056   0.5768   1.0000
   4.500   0.9788   0.01133   0.00455  -0.1054   0.5553   1.0000
   4.750   1.0046   0.01158   0.00474  -0.1051   0.5307   1.0000
   5.000   1.0296   0.01190   0.00499  -0.1046   0.5015   1.0000
   5.250   1.0537   0.01229   0.00527  -0.1040   0.4685   1.0000
   5.500   1.0769   0.01278   0.00562  -0.1034   0.4327   1.0000
   5.750   1.0992   0.01335   0.00604  -0.1026   0.3958   1.0000
   6.000   1.1213   0.01394   0.00653  -0.1019   0.3617   1.0000
   6.250   1.1430   0.01456   0.00705  -0.1011   0.3298   1.0000
   6.500   1.1644   0.01521   0.00759  -0.1003   0.3007   1.0000
   6.750   1.1856   0.01585   0.00817  -0.0995   0.2743   1.0000
   7.000   1.2063   0.01652   0.00877  -0.0986   0.2490   1.0000
   7.250   1.2266   0.01721   0.00943  -0.0977   0.2260   1.0000
   7.500   1.2469   0.01789   0.01007  -0.0968   0.2040   1.0000
   7.750   1.2661   0.01862   0.01076  -0.0957   0.1827   1.0000
   8.000   1.2849   0.01937   0.01148  -0.0946   0.1621   1.0000
   8.250   1.3026   0.02017   0.01224  -0.0934   0.1424   1.0000
   8.500   1.3194   0.02103   0.01306  -0.0920   0.1221   1.0000
   8.750   1.3350   0.02194   0.01396  -0.0905   0.1036   1.0000
   9.000   1.3498   0.02287   0.01488  -0.0889   0.0872   1.0000
   9.250   1.3624   0.02386   0.01586  -0.0870   0.0733   1.0000
   9.500   1.3726   0.02493   0.01693  -0.0847   0.0607   1.0000
   9.750   1.3824   0.02610   0.01811  -0.0825   0.0499   1.0000
  10.000   1.3917   0.02736   0.01942  -0.0804   0.0415   1.0000
  10.250   1.3994   0.02880   0.02088  -0.0783   0.0345   1.0000
  10.500   1.4072   0.03026   0.02240  -0.0763   0.0284   1.0000
  10.750   1.4143   0.03182   0.02406  -0.0744   0.0241   1.0000
  11.000   1.4201   0.03353   0.02587  -0.0726   0.0202   1.0000
  11.250   1.4252   0.03537   0.02783  -0.0708   0.0170   1.0000
  11.500   1.4304   0.03722   0.02976  -0.0693   0.0139   1.0000
  11.750   1.4336   0.03934   0.03200  -0.0677   0.0114   1.0000
  12.000   1.4369   0.04148   0.03424  -0.0664   0.0093   1.0000
  12.250   1.4350   0.04423   0.03713  -0.0649   0.0081   1.0000
  12.500   1.4357   0.04679   0.03987  -0.0637   0.0068   1.0000
  12.750   1.4360   0.04944   0.04265  -0.0628   0.0059   1.0000
  13.000   1.4316   0.05272   0.04605  -0.0619   0.0052   1.0000
  13.250   1.4305   0.05568   0.04921  -0.0613   0.0045   1.0000
  13.500   1.4287   0.05880   0.05249  -0.0609   0.0040   1.0000
  13.750   1.4253   0.06222   0.05606  -0.0607   0.0036   1.0000
  14.000   1.4173   0.06637   0.06036  -0.0608   0.0033   1.0000
  14.250   1.4079   0.07094   0.06511  -0.0613   0.0032   1.0000
  14.500   1.3988   0.07570   0.07007  -0.0620   0.0030   1.0000
  14.750   1.3885   0.08086   0.07543  -0.0632   0.0029   1.0000
  15.000   1.3770   0.08642   0.08119  -0.0647   0.0029   1.0000
  15.250   1.3650   0.09234   0.08734  -0.0667   0.0028   1.0000
  15.500   1.3524   0.09860   0.09379  -0.0690   0.0027   1.0000
  15.750   1.3391   0.10519   0.10057  -0.0717   0.0027   1.0000
  16.000   1.3252   0.11216   0.10771  -0.0748   0.0026   1.0000
  16.250   1.3113   0.11936   0.11509  -0.0782   0.0026   1.0000
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