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PSU 94-097 (AIAA 2001-2478) (psu94097-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: PSU 94-097 (AIAA 2001-2478) (psu94097-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.54 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-psu94097-il-1000000-n5.txt
Download as CSV file: xf-psu94097-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.2526   0.11464   0.11283  -0.0335   0.8948   0.0045
 -10.750  -0.2497   0.11128   0.10944  -0.0343   0.8862   0.0045
  -7.250  -0.3078   0.07023   0.06807  -0.0498   0.8046   0.0024
  -7.000  -0.2944   0.06407   0.06188  -0.0586   0.7972   0.0024
  -6.750  -0.2755   0.05638   0.05412  -0.0701   0.7897   0.0023
  -6.250  -0.2305   0.01573   0.01121  -0.0990   0.7790   0.0021
  -6.000  -0.2022   0.01417   0.00931  -0.0996   0.7734   0.0023
  -5.750  -0.1735   0.01325   0.00820  -0.1000   0.7680   0.0024
  -5.500  -0.1448   0.01267   0.00747  -0.1004   0.7624   0.0025
  -5.250  -0.1157   0.01154   0.00610  -0.1009   0.7573   0.0027
  -5.000  -0.0867   0.01094   0.00538  -0.1013   0.7520   0.0030
  -4.750  -0.0576   0.01054   0.00489  -0.1017   0.7469   0.0031
  -4.500  -0.0285   0.01015   0.00441  -0.1021   0.7424   0.0033
  -4.250   0.0008   0.00977   0.00397  -0.1024   0.7375   0.0035
  -4.000   0.0302   0.00944   0.00355  -0.1028   0.7326   0.0037
  -3.750   0.0596   0.00912   0.00315  -0.1032   0.7283   0.0039
  -3.500   0.0891   0.00886   0.00284  -0.1036   0.7236   0.0042
  -3.250   0.1183   0.00870   0.00263  -0.1039   0.7190   0.0045
  -3.000   0.1480   0.00839   0.00224  -0.1043   0.7147   0.0051
  -2.750   0.1777   0.00817   0.00198  -0.1047   0.7102   0.0056
  -2.500   0.2072   0.00800   0.00176  -0.1050   0.7055   0.0067
  -2.250   0.2368   0.00782   0.00158  -0.1054   0.7012   0.0137
  -2.000   0.2664   0.00764   0.00145  -0.1058   0.6964   0.0315
  -1.750   0.2959   0.00742   0.00135  -0.1063   0.6912   0.0702
  -1.500   0.3256   0.00718   0.00126  -0.1069   0.6859   0.1290
  -1.250   0.3552   0.00703   0.00120  -0.1073   0.6798   0.1699
  -1.000   0.3847   0.00684   0.00116  -0.1079   0.6741   0.2360
  -0.750   0.4143   0.00667   0.00113  -0.1084   0.6672   0.2968
  -0.500   0.4438   0.00651   0.00111  -0.1089   0.6591   0.3642
  -0.250   0.4734   0.00633   0.00111  -0.1094   0.6506   0.4418
   0.000   0.5029   0.00617   0.00113  -0.1100   0.6433   0.5239
   0.250   0.5322   0.00608   0.00114  -0.1104   0.6347   0.5815
   0.500   0.5613   0.00601   0.00117  -0.1107   0.6255   0.6311
   0.750   0.5903   0.00595   0.00122  -0.1110   0.6156   0.6898
   1.000   0.6189   0.00591   0.00128  -0.1112   0.6043   0.7431
   1.250   0.6473   0.00591   0.00132  -0.1114   0.5916   0.7767
   1.500   0.6753   0.00593   0.00138  -0.1114   0.5781   0.8101
   1.750   0.7027   0.00596   0.00145  -0.1113   0.5631   0.8460
   2.000   0.7271   0.00595   0.00152  -0.1105   0.5462   0.9018
   2.250   0.7487   0.00590   0.00151  -0.1090   0.5280   1.0000
   2.500   0.7769   0.00610   0.00160  -0.1092   0.5066   1.0000
   2.750   0.8048   0.00631   0.00171  -0.1094   0.4824   1.0000
   3.000   0.8325   0.00656   0.00185  -0.1095   0.4562   1.0000
   3.250   0.8598   0.00686   0.00200  -0.1096   0.4260   1.0000
   3.500   0.8868   0.00717   0.00218  -0.1097   0.3956   1.0000
   3.750   0.9136   0.00751   0.00237  -0.1097   0.3655   1.0000
   4.000   0.9403   0.00784   0.00258  -0.1097   0.3371   1.0000
   4.250   0.9669   0.00818   0.00279  -0.1097   0.3093   1.0000
   4.500   0.9935   0.00849   0.00300  -0.1097   0.2858   1.0000
   4.750   1.0200   0.00881   0.00324  -0.1097   0.2643   1.0000
   5.000   1.0464   0.00912   0.00346  -0.1097   0.2443   1.0000
   5.250   1.0725   0.00945   0.00371  -0.1096   0.2247   1.0000
   5.500   1.0985   0.00979   0.00397  -0.1095   0.2047   1.0000
   5.750   1.1242   0.01014   0.00425  -0.1093   0.1872   1.0000
   6.000   1.1498   0.01048   0.00453  -0.1092   0.1711   1.0000
   6.250   1.1751   0.01085   0.00483  -0.1090   0.1536   1.0000
   6.500   1.1997   0.01128   0.00516  -0.1087   0.1348   1.0000
   6.750   1.2239   0.01173   0.00552  -0.1083   0.1159   1.0000
   7.000   1.2472   0.01227   0.00595  -0.1078   0.0948   1.0000
   7.250   1.2696   0.01287   0.00643  -0.1072   0.0720   1.0000
   7.500   1.2910   0.01355   0.00696  -0.1064   0.0501   1.0000
   7.750   1.3128   0.01417   0.00749  -0.1057   0.0356   1.0000
   8.000   1.3352   0.01469   0.00797  -0.1051   0.0273   1.0000
   8.250   1.3566   0.01528   0.00852  -0.1043   0.0190   1.0000
   8.500   1.3777   0.01587   0.00910  -0.1034   0.0127   1.0000
   8.750   1.3988   0.01643   0.00966  -0.1026   0.0092   1.0000
   9.000   1.4196   0.01698   0.01022  -0.1017   0.0066   1.0000
   9.250   1.4394   0.01760   0.01084  -0.1007   0.0041   1.0000
   9.500   1.4578   0.01829   0.01154  -0.0995   0.0020   1.0000
   9.750   1.4757   0.01897   0.01227  -0.0981   0.0010   1.0000
  10.000   1.4928   0.01967   0.01301  -0.0967   0.0006   1.0000
  10.250   1.5081   0.02040   0.01382  -0.0950   0.0004   1.0000
  10.500   1.5203   0.02116   0.01466  -0.0927   0.0003   1.0000
  10.750   1.5328   0.02195   0.01552  -0.0906   0.0002   1.0000
  11.000   1.5450   0.02279   0.01644  -0.0886   0.0002   1.0000
  11.250   1.5567   0.02372   0.01745  -0.0867   0.0002   1.0000
  11.500   1.5676   0.02474   0.01855  -0.0848   0.0002   1.0000
  11.750   1.5773   0.02588   0.01979  -0.0829   0.0002   1.0000
  12.000   1.5868   0.02709   0.02109  -0.0811   0.0002   1.0000
  12.250   1.5952   0.02844   0.02253  -0.0793   0.0002   1.0000
  12.500   1.6027   0.02989   0.02410  -0.0776   0.0002   1.0000
  12.750   1.6092   0.03149   0.02580  -0.0760   0.0002   1.0000
  13.000   1.6148   0.03320   0.02762  -0.0744   0.0002   1.0000
  13.250   1.6191   0.03509   0.02963  -0.0729   0.0001   1.0000
  13.500   1.6222   0.03716   0.03181  -0.0714   0.0001   1.0000
  13.750   1.6244   0.03936   0.03412  -0.0701   0.0001   1.0000
  14.000   1.6248   0.04182   0.03671  -0.0689   0.0001   1.0000
  14.250   1.6247   0.04439   0.03940  -0.0678   0.0001   1.0000
  14.500   1.6228   0.04723   0.04236  -0.0669   0.0001   1.0000
  14.750   1.6193   0.05035   0.04561  -0.0661   0.0001   1.0000
  15.000   1.6147   0.05367   0.04906  -0.0655   0.0001   1.0000
  15.250   1.6083   0.05739   0.05292  -0.0652   0.0001   1.0000
  15.500   1.6008   0.06144   0.05711  -0.0652   0.0001   1.0000
  15.750   1.5923   0.06578   0.06159  -0.0654   0.0001   1.0000
  16.000   1.5818   0.07059   0.06654  -0.0661   0.0001   1.0000
  16.250   1.5697   0.07589   0.07198  -0.0671   0.0001   1.0000
  16.500   1.5581   0.08132   0.07756  -0.0685   0.0001   1.0000
  16.750   1.5424   0.08757   0.08397  -0.0703   0.0001   1.0000
  17.000   1.5273   0.09400   0.09055  -0.0725   0.0001   1.0000
  17.250   1.5094   0.10116   0.09786  -0.0751   0.0001   1.0000
  17.500   1.4901   0.10874   0.10558  -0.0782   0.0001   1.0000
  17.750   1.4702   0.11667   0.11366  -0.0816   0.0001   1.0000
  18.000   1.4507   0.12475   0.12187  -0.0853   0.0001   1.0000
  18.250   1.4291   0.13349   0.13075  -0.0896   0.0001   1.0000
  18.500   1.4091   0.14206   0.13944  -0.0939   0.0001   1.0000
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