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PSU 94-097 (AIAA 2001-2478) (psu94097-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: PSU 94-097 (AIAA 2001-2478) (psu94097-il)
Reynolds number: 100,000
Max Cl/Cd: 64.06 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-psu94097-il-100000-n5.txt
Download as CSV file: xf-psu94097-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.250  -0.3284   0.11093   0.10604  -0.0332   1.0000   0.0397
  -9.000  -0.3252   0.10792   0.10308  -0.0352   1.0000   0.0418
  -8.750  -0.3264   0.10533   0.10058  -0.0386   1.0000   0.0434
  -8.500  -0.2524   0.09296   0.08878  -0.0407   0.9956   0.0464
  -8.250  -0.2410   0.08862   0.08441  -0.0428   0.9903   0.0474
  -8.000  -0.2309   0.08418   0.07997  -0.0458   0.9852   0.0483
  -7.750  -0.2219   0.07967   0.07547  -0.0490   0.9794   0.0489
  -7.250  -0.3232   0.08736   0.08306  -0.0437   0.9864   0.0470
  -7.000  -0.3040   0.08270   0.07838  -0.0495   0.9781   0.0478
  -6.500  -0.2601   0.06964   0.06520  -0.0670   0.9602   0.0288
  -6.250  -0.2300   0.05940   0.05474  -0.0817   0.9499   0.0226
  -6.000  -0.2058   0.05413   0.04932  -0.0877   0.9430   0.0218
  -5.750  -0.1818   0.04865   0.04361  -0.0932   0.9344   0.0210
  -5.500  -0.1520   0.04274   0.03733  -0.0991   0.9283   0.0202
  -5.250  -0.1249   0.03770   0.03182  -0.1027   0.9203   0.0196
  -5.000  -0.0926   0.03302   0.02653  -0.1061   0.9150   0.0191
  -4.750  -0.0623   0.02943   0.02233  -0.1079   0.9085   0.0190
  -4.500  -0.0305   0.02657   0.01889  -0.1093   0.9028   0.0191
  -4.250   0.0019   0.02429   0.01612  -0.1103   0.8983   0.0196
  -4.000   0.0304   0.02264   0.01412  -0.1104   0.8913   0.0207
  -3.750   0.0617   0.02144   0.01257  -0.1108   0.8865   0.0235
  -3.500   0.0893   0.02018   0.01125  -0.1111   0.8802   0.0270
  -3.250   0.1188   0.01912   0.01003  -0.1112   0.8745   0.0308
  -3.000   0.1486   0.01822   0.00905  -0.1116   0.8695   0.0410
  -2.750   0.1772   0.01737   0.00822  -0.1119   0.8630   0.0660
  -2.500   0.2072   0.01639   0.00757  -0.1125   0.8583   0.1482
  -2.250   0.2342   0.01563   0.00735  -0.1130   0.8521   0.2955
  -2.000   0.2610   0.01491   0.00724  -0.1130   0.8466   0.4830
  -1.750   0.2846   0.01446   0.00722  -0.1115   0.8417   0.6486
  -1.500   0.3043   0.01428   0.00721  -0.1091   0.8348   0.7562
  -1.250   0.3236   0.01406   0.00704  -0.1063   0.8299   0.8441
  -1.000   0.3504   0.01385   0.00681  -0.1054   0.8232   0.9751
  -0.750   0.3808   0.01389   0.00663  -0.1060   0.8177   1.0000
  -0.500   0.4100   0.01400   0.00653  -0.1064   0.8122   1.0000
  -0.250   0.4385   0.01413   0.00650  -0.1067   0.8058   1.0000
   0.000   0.4682   0.01419   0.00639  -0.1069   0.8011   1.0000
   0.250   0.4956   0.01438   0.00647  -0.1071   0.7937   1.0000
   0.500   0.5247   0.01446   0.00641  -0.1072   0.7883   1.0000
   0.750   0.5523   0.01463   0.00650  -0.1073   0.7811   1.0000
   1.000   0.5808   0.01471   0.00649  -0.1074   0.7748   1.0000
   1.250   0.6083   0.01486   0.00658  -0.1074   0.7673   1.0000
   1.500   0.6366   0.01494   0.00659  -0.1073   0.7605   1.0000
   1.750   0.6637   0.01508   0.00670  -0.1072   0.7521   1.0000
   2.000   0.6923   0.01510   0.00667  -0.1071   0.7449   1.0000
   2.250   0.7188   0.01525   0.00681  -0.1068   0.7348   1.0000
   2.500   0.7461   0.01533   0.00687  -0.1066   0.7257   1.0000
   2.750   0.7741   0.01537   0.00688  -0.1064   0.7171   1.0000
   3.000   0.8005   0.01550   0.00704  -0.1061   0.7063   1.0000
   3.250   0.8273   0.01560   0.00719  -0.1058   0.6956   1.0000
   3.500   0.8544   0.01568   0.00727  -0.1055   0.6849   1.0000
   3.750   0.8815   0.01574   0.00734  -0.1051   0.6736   1.0000
   4.000   0.9079   0.01584   0.00749  -0.1047   0.6609   1.0000
   4.250   0.9340   0.01595   0.00769  -0.1043   0.6470   1.0000
   4.500   0.9601   0.01606   0.00784  -0.1038   0.6323   1.0000
   4.750   0.9855   0.01622   0.00808  -0.1033   0.6150   1.0000
   5.000   1.0108   0.01636   0.00832  -0.1028   0.5961   1.0000
   5.250   1.0361   0.01650   0.00849  -0.1021   0.5757   1.0000
   5.500   1.0606   0.01670   0.00872  -0.1014   0.5514   1.0000
   5.750   1.0845   0.01695   0.00896  -0.1005   0.5236   1.0000
   6.000   1.1076   0.01729   0.00928  -0.0995   0.4922   1.0000
   6.250   1.1294   0.01775   0.00966  -0.0984   0.4567   1.0000
   6.500   1.1500   0.01833   0.01013  -0.0972   0.4203   1.0000
   6.750   1.1695   0.01903   0.01071  -0.0959   0.3844   1.0000
   7.000   1.1880   0.01981   0.01138  -0.0946   0.3513   1.0000
   7.250   1.2062   0.02063   0.01213  -0.0933   0.3205   1.0000
   7.500   1.2237   0.02150   0.01298  -0.0919   0.2923   1.0000
   7.750   1.2405   0.02241   0.01384  -0.0904   0.2664   1.0000
   8.000   1.2566   0.02335   0.01475  -0.0889   0.2417   1.0000
   8.250   1.2724   0.02429   0.01570  -0.0874   0.2185   1.0000
   8.500   1.2867   0.02531   0.01671  -0.0857   0.1969   1.0000
   8.750   1.3002   0.02636   0.01777  -0.0840   0.1753   1.0000
   9.000   1.3123   0.02748   0.01894  -0.0821   0.1553   1.0000
   9.250   1.3220   0.02864   0.02012  -0.0799   0.1359   1.0000
   9.500   1.3297   0.02997   0.02142  -0.0776   0.1187   1.0000
   9.750   1.3383   0.03134   0.02283  -0.0755   0.1008   1.0000
  10.000   1.3449   0.03292   0.02442  -0.0734   0.0856   1.0000
  10.250   1.3503   0.03465   0.02618  -0.0713   0.0727   1.0000
  10.500   1.3545   0.03655   0.02814  -0.0693   0.0627   1.0000
  10.750   1.3567   0.03867   0.03031  -0.0673   0.0546   1.0000
  11.000   1.3584   0.04091   0.03261  -0.0654   0.0473   1.0000
  11.250   1.3598   0.04327   0.03513  -0.0636   0.0419   1.0000
  11.500   1.3592   0.04585   0.03781  -0.0621   0.0375   1.0000
  11.750   1.3578   0.04863   0.04076  -0.0606   0.0335   1.0000
  12.000   1.3575   0.05136   0.04367  -0.0594   0.0299   1.0000
  12.250   1.3526   0.05463   0.04704  -0.0583   0.0273   1.0000
  12.500   1.3496   0.05785   0.05045  -0.0573   0.0247   1.0000
  12.750   1.3466   0.06116   0.05397  -0.0566   0.0224   1.0000
  13.000   1.3413   0.06479   0.05776  -0.0562   0.0208   1.0000
  13.250   1.3327   0.06891   0.06199  -0.0561   0.0194   1.0000
  13.500   1.3249   0.07313   0.06639  -0.0560   0.0181   1.0000
  13.750   1.3190   0.07731   0.07084  -0.0562   0.0166   1.0000
  14.000   1.3112   0.08190   0.07563  -0.0569   0.0155   1.0000
  14.250   1.3025   0.08677   0.08069  -0.0579   0.0148   1.0000
  14.500   1.2932   0.09194   0.08603  -0.0593   0.0142   1.0000
  14.750   1.2831   0.09741   0.09165  -0.0612   0.0137   1.0000
  15.000   1.2723   0.10320   0.09758  -0.0633   0.0133   1.0000
  15.250   1.2604   0.10933   0.10386  -0.0658   0.0129   1.0000
  15.500   1.2488   0.11592   0.11065  -0.0688   0.0126   1.0000
  15.750   1.2368   0.12294   0.11790  -0.0724   0.0124   1.0000
  16.000   1.2239   0.13049   0.12567  -0.0766   0.0123   1.0000
  16.250   1.2113   0.13832   0.13369  -0.0811   0.0122   1.0000
  16.500   1.1985   0.14653   0.14207  -0.0860   0.0123   1.0000
  16.750   1.1858   0.15516   0.15085  -0.0914   0.0124   1.0000
  17.000   1.1735   0.16402   0.15983  -0.0969   0.0125   1.0000
  17.250   1.1617   0.17321   0.16912  -0.1027   0.0127   1.0000
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