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PSU 94-097 (AIAA 2001-2478) (psu94097-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: PSU 94-097 (AIAA 2001-2478) (psu94097-il)
Reynolds number: 500,000
Max Cl/Cd: 126.62 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-psu94097-il-500000.txt
Download as CSV file: xf-psu94097-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.3207   0.09792   0.09577  -0.0377   1.0000   0.0110
  -8.500  -0.3155   0.09436   0.09224  -0.0397   1.0000   0.0111
  -8.250  -0.3166   0.08931   0.08724  -0.0418   0.9965   0.0114
  -8.000  -0.3016   0.08552   0.08345  -0.0456   0.9854   0.0117
  -7.750  -0.2865   0.08182   0.07975  -0.0495   0.9723   0.0120
  -7.500  -0.2759   0.07823   0.07615  -0.0526   0.9559   0.0123
  -7.250  -0.2714   0.07498   0.07286  -0.0546   0.9379   0.0126
  -7.000  -0.2633   0.07122   0.06906  -0.0583   0.9233   0.0129
  -6.750  -0.2514   0.06684   0.06463  -0.0638   0.9110   0.0133
  -6.500  -0.2353   0.06173   0.05945  -0.0709   0.9000   0.0137
  -6.250  -0.2146   0.05584   0.05347  -0.0791   0.8895   0.0143
  -6.000  -0.1891   0.04914   0.04659  -0.0873   0.8808   0.0153
  -5.750  -0.1575   0.04287   0.04000  -0.0932   0.8730   0.0161
  -5.500  -0.1325   0.03795   0.03473  -0.0968   0.8654   0.0162
  -5.250  -0.1142   0.03092   0.02738  -0.1009   0.8587   0.0174
  -5.000  -0.0890   0.02866   0.02495  -0.1022   0.8519   0.0183
  -4.750  -0.0617   0.02605   0.02205  -0.1034   0.8457   0.0197
  -4.500  -0.0255   0.01854   0.01334  -0.1041   0.8405   0.0112
  -4.250   0.0040   0.01597   0.01041  -0.1047   0.8344   0.0108
  -3.750   0.0622   0.01286   0.00679  -0.1054   0.8234   0.0123
  -3.500   0.0909   0.01233   0.00620  -0.1056   0.8179   0.0137
  -3.250   0.1204   0.01143   0.00515  -0.1058   0.8128   0.0139
  -3.000   0.1503   0.01070   0.00432  -0.1061   0.8071   0.0142
  -2.750   0.1801   0.01017   0.00367  -0.1064   0.8022   0.0153
  -2.500   0.2106   0.00959   0.00300  -0.1069   0.7971   0.0208
  -2.250   0.2413   0.00886   0.00258  -0.1077   0.7917   0.1103
  -2.000   0.2709   0.00836   0.00246  -0.1085   0.7872   0.2344
  -1.750   0.3008   0.00791   0.00239  -0.1093   0.7818   0.3623
  -1.500   0.3305   0.00743   0.00236  -0.1100   0.7766   0.5253
  -1.250   0.3591   0.00715   0.00238  -0.1103   0.7720   0.6472
  -1.000   0.3872   0.00696   0.00240  -0.1102   0.7661   0.7291
  -0.750   0.4139   0.00684   0.00239  -0.1097   0.7608   0.7921
  -0.500   0.4389   0.00673   0.00239  -0.1088   0.7552   0.8494
  -0.250   0.4607   0.00659   0.00234  -0.1071   0.7492   0.9044
   0.000   0.4846   0.00644   0.00218  -0.1059   0.7435   1.0000
   0.250   0.5144   0.00647   0.00214  -0.1063   0.7362   1.0000
   0.500   0.5438   0.00655   0.00211  -0.1067   0.7300   1.0000
   0.750   0.5732   0.00658   0.00212  -0.1071   0.7229   1.0000
   1.000   0.6024   0.00666   0.00210  -0.1073   0.7167   1.0000
   1.250   0.6317   0.00670   0.00213  -0.1077   0.7093   1.0000
   1.750   0.6897   0.00683   0.00217  -0.1082   0.6947   1.0000
   2.000   0.7184   0.00692   0.00220  -0.1084   0.6875   1.0000
   2.250   0.7473   0.00697   0.00225  -0.1087   0.6791   1.0000
   2.500   0.7760   0.00705   0.00229  -0.1089   0.6710   1.0000
   2.750   0.8045   0.00712   0.00234  -0.1091   0.6620   1.0000
   3.000   0.8331   0.00719   0.00243  -0.1093   0.6522   1.0000
   3.250   0.8615   0.00728   0.00250  -0.1094   0.6421   1.0000
   3.500   0.8896   0.00738   0.00257  -0.1095   0.6309   1.0000
   3.750   0.9176   0.00748   0.00265  -0.1096   0.6183   1.0000
   4.000   0.9455   0.00759   0.00277  -0.1097   0.6032   1.0000
   4.250   0.9732   0.00772   0.00288  -0.1097   0.5855   1.0000
   4.500   1.0003   0.00790   0.00301  -0.1097   0.5645   1.0000
   4.750   1.0269   0.00813   0.00319  -0.1095   0.5387   1.0000
   5.000   1.0528   0.00844   0.00339  -0.1093   0.5089   1.0000
   5.250   1.0781   0.00881   0.00364  -0.1090   0.4742   1.0000
   5.500   1.1025   0.00928   0.00394  -0.1086   0.4347   1.0000
   5.750   1.1263   0.00982   0.00432  -0.1082   0.3944   1.0000
   6.000   1.1497   0.01039   0.00472  -0.1077   0.3546   1.0000
   6.250   1.1731   0.01095   0.00513  -0.1072   0.3196   1.0000
   6.500   1.1964   0.01150   0.00556  -0.1067   0.2884   1.0000
   6.750   1.2194   0.01207   0.00601  -0.1062   0.2590   1.0000
   7.000   1.2422   0.01263   0.00648  -0.1056   0.2325   1.0000
   7.250   1.2646   0.01322   0.00696  -0.1050   0.2065   1.0000
   7.500   1.2866   0.01382   0.00746  -0.1043   0.1827   1.0000
   7.750   1.3086   0.01439   0.00797  -0.1036   0.1624   1.0000
   8.000   1.3299   0.01500   0.00852  -0.1029   0.1422   1.0000
   8.250   1.3503   0.01567   0.00911  -0.1019   0.1213   1.0000
   8.500   1.3699   0.01638   0.00976  -0.1009   0.1010   1.0000
   8.750   1.3875   0.01724   0.01048  -0.0996   0.0794   1.0000
   9.000   1.4035   0.01818   0.01129  -0.0981   0.0581   1.0000
   9.250   1.4191   0.01910   0.01213  -0.0966   0.0419   1.0000
   9.500   1.4336   0.02005   0.01301  -0.0949   0.0304   1.0000
   9.750   1.4478   0.02093   0.01388  -0.0930   0.0233   1.0000
  10.000   1.4584   0.02187   0.01483  -0.0906   0.0185   1.0000
  10.250   1.4705   0.02275   0.01575  -0.0885   0.0149   1.0000
  10.500   1.4803   0.02384   0.01691  -0.0863   0.0108   1.0000
  10.750   1.4811   0.02571   0.01879  -0.0831   0.0054   1.0000
  11.000   1.4870   0.02725   0.02041  -0.0807   0.0036   1.0000
  11.250   1.4899   0.02913   0.02243  -0.0782   0.0030   1.0000
  11.500   1.4957   0.03078   0.02421  -0.0762   0.0026   1.0000
  11.750   1.5002   0.03261   0.02617  -0.0744   0.0023   1.0000
  12.000   1.5033   0.03462   0.02831  -0.0726   0.0022   1.0000
  12.250   1.5036   0.03698   0.03080  -0.0708   0.0020   1.0000
  12.500   1.5001   0.03978   0.03375  -0.0690   0.0019   1.0000
  12.750   1.4933   0.04305   0.03719  -0.0674   0.0019   1.0000
  13.000   1.4849   0.04660   0.04090  -0.0660   0.0018   1.0000
  13.250   1.4733   0.05066   0.04514  -0.0648   0.0018   1.0000
  13.500   1.4646   0.05452   0.04915  -0.0640   0.0018   1.0000
  13.750   1.4584   0.05822   0.05301  -0.0635   0.0018   1.0000
  14.000   1.4510   0.06224   0.05719  -0.0633   0.0017   1.0000
  14.250   1.4427   0.06655   0.06166  -0.0634   0.0017   1.0000
  14.500   1.4336   0.07117   0.06646  -0.0638   0.0017   1.0000
  14.750   1.4237   0.07613   0.07158  -0.0646   0.0017   1.0000
  15.000   1.4128   0.08140   0.07702  -0.0656   0.0017   1.0000
  15.250   1.4010   0.08702   0.08280  -0.0671   0.0017   1.0000
  15.500   1.3888   0.09295   0.08891  -0.0689   0.0017   1.0000
  15.750   1.3762   0.09915   0.09527  -0.0710   0.0017   1.0000
  16.000   1.3626   0.10570   0.10197  -0.0735   0.0017   1.0000
  16.250   1.3488   0.11253   0.10897  -0.0764   0.0017   1.0000
  16.500   1.3353   0.11949   0.11609  -0.0795   0.0017   1.0000
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