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PSU 94-097 (AIAA 2001-2478) (psu94097-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: PSU 94-097 (AIAA 2001-2478) (psu94097-il)
Reynolds number: 200,000
Max Cl/Cd: 90.79 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-psu94097-il-200000.txt
Download as CSV file: xf-psu94097-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.250  -0.3159   0.09655   0.09330  -0.0406   1.0000   0.0320
  -8.000  -0.3278   0.09525   0.09210  -0.0395   1.0000   0.0323
  -7.750  -0.3540   0.09560   0.09257  -0.0334   1.0000   0.0322
  -7.500  -0.3379   0.09107   0.08806  -0.0430   0.9925   0.0326
  -7.250  -0.3085   0.08482   0.08178  -0.0556   0.9853   0.0328
  -7.000  -0.2974   0.07792   0.07492  -0.0587   0.9818   0.0340
  -6.750  -0.2786   0.07464   0.07161  -0.0599   0.9767   0.0354
  -6.500  -0.2507   0.06989   0.06683  -0.0674   0.9722   0.0374
  -6.250  -0.2198   0.06405   0.06093  -0.0780   0.9660   0.0400
  -6.000  -0.1685   0.05573   0.05209  -0.0984   0.9574   0.0443
  -5.750  -0.1519   0.04896   0.04533  -0.1023   0.9510   0.0460
  -5.500  -0.1279   0.04626   0.04264  -0.1040   0.9453   0.0486
  -5.000  -0.0713   0.03842   0.03432  -0.1118   0.9319   0.0617
  -4.750  -0.0405   0.03508   0.03063  -0.1150   0.9271   0.0736
  -4.250   0.0294   0.02436   0.01815  -0.1170   0.9147   0.0334
  -4.000   0.0572   0.02118   0.01468  -0.1173   0.9082   0.0300
  -3.750   0.0871   0.01897   0.01205  -0.1173   0.9026   0.0283
  -3.500   0.1164   0.01741   0.01021  -0.1170   0.8976   0.0281
  -3.250   0.1442   0.01627   0.00894  -0.1167   0.8909   0.0293
  -3.000   0.1730   0.01533   0.00788  -0.1164   0.8862   0.0323
  -2.750   0.2014   0.01437   0.00691  -0.1166   0.8797   0.0460
  -2.500   0.2317   0.01285   0.00600  -0.1175   0.8744   0.1778
  -2.250   0.2601   0.01189   0.00583  -0.1182   0.8698   0.4048
  -2.000   0.2850   0.01127   0.00595  -0.1177   0.8632   0.6271
  -1.750   0.3068   0.01099   0.00594  -0.1156   0.8584   0.7506
  -1.500   0.3246   0.01087   0.00597  -0.1127   0.8518   0.8356
  -1.250   0.3402   0.01068   0.00582  -0.1091   0.8460   0.9183
  -1.000   0.3729   0.01057   0.00557  -0.1098   0.8410   1.0000
  -0.750   0.4024   0.01067   0.00551  -0.1104   0.8345   1.0000
  -0.500   0.4319   0.01071   0.00537  -0.1106   0.8298   1.0000
  -0.250   0.4607   0.01085   0.00540  -0.1110   0.8229   1.0000
   0.000   0.4896   0.01089   0.00532  -0.1111   0.8173   1.0000
   0.250   0.5180   0.01100   0.00533  -0.1113   0.8108   1.0000
   0.500   0.5465   0.01107   0.00530  -0.1114   0.8043   1.0000
   0.750   0.5749   0.01115   0.00530  -0.1114   0.7981   1.0000
   1.000   0.6030   0.01121   0.00529  -0.1114   0.7905   1.0000
   1.250   0.6311   0.01126   0.00527  -0.1112   0.7832   1.0000
   1.500   0.6591   0.01130   0.00524  -0.1111   0.7754   1.0000
   1.750   0.6870   0.01138   0.00529  -0.1111   0.7675   1.0000
   2.000   0.7152   0.01140   0.00526  -0.1109   0.7602   1.0000
   2.250   0.7427   0.01148   0.00533  -0.1108   0.7512   1.0000
   2.500   0.7710   0.01149   0.00527  -0.1106   0.7440   1.0000
   2.750   0.7984   0.01156   0.00535  -0.1105   0.7341   1.0000
   3.000   0.8261   0.01162   0.00543  -0.1103   0.7249   1.0000
   3.250   0.8542   0.01163   0.00539  -0.1101   0.7166   1.0000
   3.500   0.8814   0.01169   0.00549  -0.1099   0.7055   1.0000
   3.750   0.9086   0.01174   0.00556  -0.1097   0.6946   1.0000
   4.000   0.9360   0.01178   0.00563  -0.1095   0.6835   1.0000
   4.250   0.9632   0.01181   0.00568  -0.1092   0.6715   1.0000
   4.500   0.9902   0.01185   0.00574  -0.1089   0.6582   1.0000
   4.750   1.0168   0.01190   0.00583  -0.1085   0.6430   1.0000
   5.000   1.0431   0.01196   0.00595  -0.1081   0.6254   1.0000
   5.250   1.0692   0.01203   0.00602  -0.1076   0.6060   1.0000
   5.500   1.0947   0.01215   0.00616  -0.1071   0.5823   1.0000
   5.750   1.1195   0.01233   0.00632  -0.1064   0.5544   1.0000
   6.000   1.1432   0.01263   0.00655  -0.1055   0.5213   1.0000
   6.250   1.1657   0.01306   0.00687  -0.1046   0.4819   1.0000
   6.500   1.1865   0.01365   0.00729  -0.1034   0.4383   1.0000
   6.750   1.2060   0.01439   0.00783  -0.1022   0.3951   1.0000
   7.000   1.2250   0.01519   0.00845  -0.1009   0.3548   1.0000
   7.250   1.2436   0.01600   0.00916  -0.0997   0.3191   1.0000
   7.500   1.2620   0.01684   0.00988  -0.0984   0.2874   1.0000
   7.750   1.2798   0.01768   0.01064  -0.0971   0.2584   1.0000
   8.000   1.2974   0.01852   0.01141  -0.0958   0.2317   1.0000
   8.250   1.3143   0.01939   0.01222  -0.0944   0.2065   1.0000
   8.500   1.3301   0.02030   0.01306  -0.0928   0.1820   1.0000
   8.750   1.3443   0.02129   0.01401  -0.0911   0.1588   1.0000
   9.000   1.3585   0.02226   0.01496  -0.0893   0.1355   1.0000
   9.250   1.3694   0.02340   0.01605  -0.0872   0.1136   1.0000
   9.500   1.3749   0.02476   0.01730  -0.0842   0.0940   1.0000
   9.750   1.3811   0.02623   0.01875  -0.0815   0.0758   1.0000
  10.000   1.3849   0.02795   0.02045  -0.0787   0.0624   1.0000
  10.250   1.3882   0.02979   0.02230  -0.0761   0.0523   1.0000
  10.500   1.3887   0.03193   0.02444  -0.0735   0.0450   1.0000
  10.750   1.3946   0.03367   0.02627  -0.0716   0.0383   1.0000
  11.000   1.3946   0.03607   0.02877  -0.0692   0.0335   1.0000
  11.250   1.3972   0.03820   0.03098  -0.0675   0.0281   1.0000
  11.500   1.3972   0.04076   0.03369  -0.0655   0.0239   1.0000
  11.750   1.3965   0.04332   0.03628  -0.0641   0.0198   1.0000
  12.000   1.3929   0.04648   0.03962  -0.0620   0.0172   1.0000
  12.250   1.3935   0.04912   0.04239  -0.0608   0.0149   1.0000
  12.500   1.3874   0.05256   0.04588  -0.0595   0.0133   1.0000
  12.750   1.3852   0.05574   0.04926  -0.0583   0.0119   1.0000
  13.000   1.3853   0.05860   0.05230  -0.0578   0.0106   1.0000
  13.250   1.3828   0.06179   0.05561  -0.0575   0.0097   1.0000
  13.500   1.3771   0.06549   0.05942  -0.0571   0.0091   1.0000
  13.750   1.3683   0.06979   0.06385  -0.0563   0.0087   1.0000
  14.000   1.3577   0.07458   0.06886  -0.0556   0.0084   1.0000
  14.250   1.3506   0.07901   0.07352  -0.0560   0.0082   1.0000
  14.500   1.3417   0.08387   0.07863  -0.0567   0.0081   1.0000
  14.750   1.3311   0.08920   0.08420  -0.0579   0.0080   1.0000
  15.000   1.3191   0.09495   0.09018  -0.0596   0.0079   1.0000
  15.250   1.3058   0.10122   0.09669  -0.0619   0.0078   1.0000
  15.500   1.2917   0.10797   0.10366  -0.0648   0.0078   1.0000
  15.750   1.2773   0.11509   0.11099  -0.0683   0.0078   1.0000
  16.000   1.2621   0.12272   0.11883  -0.0724   0.0078   1.0000
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