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PSU 94-097 (AIAA 2001-2478) (psu94097-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: PSU 94-097 (AIAA 2001-2478) (psu94097-il)
Reynolds number: 500,000
Max Cl/Cd: 112.92 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-psu94097-il-500000-n5.txt
Download as CSV file: xf-psu94097-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.3529   0.11451   0.11224  -0.0274   1.0000   0.0072
  -9.750  -0.3469   0.11092   0.10866  -0.0291   1.0000   0.0072
  -9.500  -0.3409   0.10731   0.10507  -0.0308   0.9999   0.0073
  -9.250  -0.3306   0.10321   0.10096  -0.0341   0.9723   0.0073
  -9.000  -0.3218   0.09924   0.09698  -0.0368   0.9533   0.0073
  -8.750  -0.3163   0.09562   0.09334  -0.0384   0.9351   0.0073
  -8.000  -0.2174   0.07102   0.06859  -0.0475   0.8563   0.0062
  -7.750  -0.2184   0.06658   0.06414  -0.0490   0.8479   0.0056
  -7.500  -0.2253   0.06005   0.05760  -0.0514   0.8404   0.0044
  -7.250  -0.2952   0.07185   0.06937  -0.0512   0.8585   0.0044
  -7.000  -0.2839   0.06686   0.06435  -0.0577   0.8485   0.0043
  -6.750  -0.2680   0.06096   0.05839  -0.0662   0.8395   0.0042
  -6.500  -0.2480   0.05412   0.05143  -0.0757   0.8311   0.0040
  -6.250  -0.2249   0.04643   0.04356  -0.0847   0.8237   0.0039
  -6.000  -0.2001   0.03797   0.03477  -0.0919   0.8169   0.0038
  -5.750  -0.1735   0.02749   0.02363  -0.0975   0.8110   0.0036
  -5.500  -0.1444   0.01877   0.01381  -0.1003   0.8053   0.0038
  -5.250  -0.1154   0.01627   0.01077  -0.1010   0.7999   0.0041
  -5.000  -0.0863   0.01491   0.00906  -0.1014   0.7940   0.0044
  -4.750  -0.0576   0.01403   0.00793  -0.1017   0.7884   0.0046
  -4.500  -0.0286   0.01279   0.00648  -0.1021   0.7832   0.0049
  -4.250   0.0001   0.01232   0.00593  -0.1025   0.7775   0.0054
  -4.000   0.0288   0.01198   0.00550  -0.1028   0.7726   0.0062
  -3.750   0.0581   0.01148   0.00489  -0.1031   0.7673   0.0068
  -3.500   0.0875   0.01092   0.00422  -0.1035   0.7622   0.0070
  -3.250   0.1170   0.01047   0.00367  -0.1039   0.7575   0.0072
  -3.000   0.1468   0.01001   0.00311  -0.1043   0.7524   0.0078
  -2.750   0.1764   0.00972   0.00274  -0.1046   0.7475   0.0093
  -2.500   0.2059   0.00944   0.00241  -0.1050   0.7430   0.0150
  -2.250   0.2356   0.00914   0.00220  -0.1055   0.7380   0.0396
  -2.000   0.2651   0.00881   0.00205  -0.1060   0.7332   0.0972
  -1.750   0.2946   0.00855   0.00194  -0.1066   0.7287   0.1540
  -1.500   0.3242   0.00828   0.00185  -0.1072   0.7235   0.2249
  -1.250   0.3536   0.00802   0.00179  -0.1077   0.7186   0.3060
  -1.000   0.3832   0.00775   0.00175  -0.1083   0.7135   0.3952
  -0.750   0.4127   0.00748   0.00173  -0.1089   0.7076   0.4995
  -0.500   0.4418   0.00728   0.00174  -0.1093   0.7021   0.5913
  -0.250   0.4707   0.00714   0.00177  -0.1095   0.6957   0.6567
   0.000   0.4990   0.00707   0.00178  -0.1096   0.6891   0.7069
   0.250   0.5268   0.00697   0.00181  -0.1095   0.6810   0.7619
   0.500   0.5531   0.00688   0.00183  -0.1090   0.6734   0.8184
   0.750   0.5786   0.00681   0.00185  -0.1083   0.6655   0.8616
   1.000   0.6014   0.00673   0.00183  -0.1070   0.6581   0.9103
   1.250   0.6271   0.00663   0.00175  -0.1063   0.6493   1.0000
   1.500   0.6561   0.00671   0.00178  -0.1066   0.6401   1.0000
   1.750   0.6850   0.00680   0.00181  -0.1069   0.6304   1.0000
   2.000   0.7137   0.00690   0.00186  -0.1071   0.6194   1.0000
   2.250   0.7424   0.00700   0.00191  -0.1074   0.6074   1.0000
   2.500   0.7708   0.00711   0.00198  -0.1076   0.5942   1.0000
   2.750   0.7990   0.00725   0.00205  -0.1077   0.5790   1.0000
   3.000   0.8270   0.00740   0.00216  -0.1078   0.5620   1.0000
   3.250   0.8547   0.00758   0.00226  -0.1079   0.5421   1.0000
   3.500   0.8819   0.00781   0.00240  -0.1080   0.5197   1.0000
   3.750   0.9089   0.00808   0.00256  -0.1079   0.4942   1.0000
   4.000   0.9352   0.00840   0.00277  -0.1079   0.4640   1.0000
   4.250   0.9612   0.00876   0.00299  -0.1077   0.4314   1.0000
   4.500   0.9867   0.00918   0.00326  -0.1075   0.3972   1.0000
   4.750   1.0119   0.00962   0.00355  -0.1073   0.3640   1.0000
   5.000   1.0371   0.01006   0.00387  -0.1071   0.3334   1.0000
   5.250   1.0622   0.01049   0.00419  -0.1069   0.3061   1.0000
   5.500   1.0871   0.01092   0.00452  -0.1067   0.2806   1.0000
   5.750   1.1120   0.01135   0.00486  -0.1064   0.2573   1.0000
   6.000   1.1365   0.01179   0.00523  -0.1061   0.2342   1.0000
   6.500   1.1850   0.01269   0.00599  -0.1054   0.1943   1.0000
   6.750   1.2085   0.01318   0.00641  -0.1049   0.1741   1.0000
   7.000   1.2318   0.01368   0.00686  -0.1044   0.1557   1.0000
   7.250   1.2544   0.01423   0.00733  -0.1038   0.1353   1.0000
   7.500   1.2762   0.01483   0.00784  -0.1031   0.1152   1.0000
   7.750   1.2981   0.01538   0.00835  -0.1025   0.0998   1.0000
   8.000   1.3193   0.01599   0.00891  -0.1016   0.0846   1.0000
   8.250   1.3393   0.01667   0.00953  -0.1007   0.0697   1.0000
   8.500   1.3589   0.01736   0.01019  -0.0997   0.0565   1.0000
   8.750   1.3773   0.01812   0.01090  -0.0985   0.0431   1.0000
   9.000   1.3938   0.01899   0.01170  -0.0970   0.0300   1.0000
   9.250   1.4093   0.01989   0.01254  -0.0955   0.0204   1.0000
   9.500   1.4244   0.02075   0.01338  -0.0938   0.0140   1.0000
   9.750   1.4381   0.02156   0.01421  -0.0919   0.0103   1.0000
  10.000   1.4503   0.02240   0.01508  -0.0898   0.0080   1.0000
  10.250   1.4628   0.02327   0.01601  -0.0878   0.0060   1.0000
  10.500   1.4743   0.02424   0.01706  -0.0858   0.0043   1.0000
  10.750   1.4843   0.02537   0.01824  -0.0838   0.0028   1.0000
  11.000   1.4933   0.02662   0.01957  -0.0819   0.0019   1.0000
  11.250   1.5025   0.02789   0.02095  -0.0800   0.0014   1.0000
  11.500   1.5108   0.02928   0.02244  -0.0782   0.0011   1.0000
  11.750   1.5165   0.03095   0.02422  -0.0763   0.0009   1.0000
  12.000   1.5229   0.03261   0.02600  -0.0746   0.0008   1.0000
  12.250   1.5292   0.03431   0.02784  -0.0731   0.0007   1.0000
  12.500   1.5343   0.03617   0.02983  -0.0716   0.0007   1.0000
  12.750   1.5384   0.03818   0.03198  -0.0702   0.0006   1.0000
  13.000   1.5414   0.04034   0.03427  -0.0689   0.0006   1.0000
  13.250   1.5430   0.04272   0.03682  -0.0677   0.0005   1.0000
  13.500   1.5433   0.04529   0.03953  -0.0667   0.0005   1.0000
  13.750   1.5425   0.04805   0.04243  -0.0657   0.0005   1.0000
  14.000   1.5402   0.05108   0.04561  -0.0650   0.0005   1.0000
  14.250   1.5369   0.05428   0.04896  -0.0644   0.0005   1.0000
  14.500   1.5321   0.05778   0.05261  -0.0640   0.0004   1.0000
  14.750   1.5261   0.06162   0.05661  -0.0639   0.0004   1.0000
  15.000   1.5188   0.06578   0.06092  -0.0642   0.0004   1.0000
  15.250   1.5100   0.07035   0.06565  -0.0647   0.0004   1.0000
  15.500   1.5000   0.07532   0.07078  -0.0656   0.0004   1.0000
  15.750   1.4889   0.08067   0.07629  -0.0670   0.0004   1.0000
  16.000   1.4761   0.08649   0.08227  -0.0686   0.0004   1.0000
  16.250   1.4618   0.09281   0.08876  -0.0708   0.0004   1.0000
  16.500   1.4476   0.09934   0.09545  -0.0732   0.0004   1.0000
  16.750   1.4312   0.10647   0.10274  -0.0761   0.0004   1.0000
  17.000   1.4147   0.11382   0.11025  -0.0793   0.0004   1.0000
  17.250   1.3974   0.12157   0.11816  -0.0828   0.0004   1.0000
  17.500   1.3799   0.12958   0.12631  -0.0867   0.0004   1.0000
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