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PSU 94-097 (AIAA 2001-2478) (psu94097-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: PSU 94-097 (AIAA 2001-2478) (psu94097-il)
Reynolds number: 100,000
Max Cl/Cd: 63.95 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-psu94097-il-100000.txt
Download as CSV file: xf-psu94097-il-100000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -7.750  -0.3216   0.09598   0.09156  -0.0364   1.0000   0.0774
  -7.500  -0.3358   0.09497   0.09067  -0.0336   1.0000   0.0788
  -7.250  -0.3574   0.09467   0.09050  -0.0294   1.0000   0.0793
  -7.000  -0.3806   0.09445   0.09039  -0.0251   1.0000   0.0796
  -6.750  -0.3991   0.09359   0.08962  -0.0228   1.0000   0.0806
  -6.500  -0.4143   0.09222   0.08834  -0.0228   1.0000   0.0819
  -6.250  -0.4263   0.09021   0.08640  -0.0281   1.0000   0.0832
  -6.000  -0.4171   0.08495   0.08114  -0.0348   0.9974   0.0849
  -5.750  -0.4011   0.08186   0.07806  -0.0304   0.9946   0.0886
  -5.500  -0.3602   0.07446   0.07038  -0.0520   0.9861   0.0985
  -5.250  -0.3435   0.07112   0.06718  -0.0482   0.9833   0.1019
  -5.000  -0.3097   0.06535   0.06116  -0.0603   0.9760   0.1133
  -4.750  -0.2790   0.06175   0.05749  -0.0642   0.9715   0.1244
  -4.500  -0.2539   0.05763   0.05335  -0.0671   0.9668   0.1318
  -4.250  -0.2231   0.05374   0.04931  -0.0721   0.9609   0.1462
  -4.000  -0.1815   0.04960   0.04489  -0.0795   0.9569   0.1710
  -3.750  -0.0989   0.03645   0.03009  -0.0928   0.9559   0.0664
  -3.500  -0.0583   0.03212   0.02487  -0.0953   0.9514   0.0540
  -3.250  -0.0169   0.02912   0.02130  -0.0979   0.9476   0.0513
  -3.000   0.0270   0.02727   0.01890  -0.1007   0.9442   0.0552
  -2.750   0.0731   0.02510   0.01641  -0.1038   0.9419   0.0594
  -2.500   0.1035   0.02407   0.01529  -0.1043   0.9360   0.0694
  -2.250   0.1443   0.02255   0.01395  -0.1069   0.9321   0.1104
  -2.000   0.1906   0.01948   0.01314  -0.1112   0.9308   0.5719
  -1.750   0.2050   0.01896   0.01332  -0.1063   0.9259   0.8403
  -1.500   0.2260   0.01893   0.01315  -0.1045   0.9175   1.0000
  -1.250   0.2711   0.01910   0.01290  -0.1082   0.9136   1.0000
  -1.000   0.2956   0.01951   0.01305  -0.1082   0.9051   1.0000
  -0.750   0.3379   0.01968   0.01295  -0.1112   0.9006   1.0000
  -0.500   0.3637   0.02010   0.01318  -0.1114   0.8924   1.0000
  -0.250   0.4036   0.02026   0.01314  -0.1138   0.8873   1.0000
   0.000   0.4310   0.02065   0.01339  -0.1142   0.8794   1.0000
   0.250   0.4676   0.02080   0.01340  -0.1159   0.8735   1.0000
   0.500   0.4947   0.02118   0.01367  -0.1160   0.8653   1.0000
   0.750   0.5309   0.02125   0.01365  -0.1174   0.8592   1.0000
   1.000   0.5567   0.02164   0.01398  -0.1173   0.8503   1.0000
   1.250   0.5935   0.02159   0.01386  -0.1185   0.8445   1.0000
   1.500   0.6180   0.02196   0.01420  -0.1181   0.8346   1.0000
   1.750   0.6565   0.02167   0.01387  -0.1191   0.8294   1.0000
   2.000   0.6802   0.02199   0.01418  -0.1184   0.8183   1.0000
   2.250   0.7078   0.02211   0.01431  -0.1180   0.8088   1.0000
   2.500   0.7424   0.02177   0.01396  -0.1182   0.8021   1.0000
   2.750   0.7673   0.02196   0.01417  -0.1175   0.7910   1.0000
   3.000   0.7953   0.02192   0.01414  -0.1169   0.7813   1.0000
   3.250   0.8283   0.02146   0.01373  -0.1166   0.7737   1.0000
   3.500   0.8539   0.02148   0.01380  -0.1157   0.7619   1.0000
   3.750   0.8808   0.02138   0.01375  -0.1148   0.7506   1.0000
   4.000   0.9095   0.02111   0.01353  -0.1140   0.7400   1.0000
   4.250   0.9410   0.02057   0.01304  -0.1133   0.7307   1.0000
   4.500   0.9676   0.02039   0.01293  -0.1123   0.7176   1.0000
   4.750   0.9945   0.02014   0.01276  -0.1113   0.7039   1.0000
   5.000   1.0220   0.01983   0.01255  -0.1102   0.6896   1.0000
   5.250   1.0498   0.01947   0.01225  -0.1092   0.6744   1.0000
   5.500   1.0738   0.01936   0.01225  -0.1079   0.6547   1.0000
   5.750   1.1006   0.01901   0.01197  -0.1067   0.6350   1.0000
   6.000   1.1253   0.01879   0.01186  -0.1054   0.6113   1.0000
   6.250   1.1499   0.01860   0.01172  -0.1040   0.5838   1.0000
   6.500   1.1736   0.01852   0.01163  -0.1025   0.5514   1.0000
   6.750   1.1953   0.01869   0.01174  -0.1008   0.5130   1.0000
   7.000   1.2154   0.01912   0.01203  -0.0991   0.4708   1.0000
   7.250   1.2338   0.01983   0.01258  -0.0972   0.4283   1.0000
   7.500   1.2509   0.02074   0.01330  -0.0954   0.3881   1.0000
   7.750   1.2671   0.02179   0.01413  -0.0936   0.3522   1.0000
   8.000   1.2826   0.02287   0.01513  -0.0918   0.3182   1.0000
   8.250   1.2971   0.02401   0.01617  -0.0899   0.2874   1.0000
   8.500   1.3107   0.02520   0.01727  -0.0879   0.2587   1.0000
   8.750   1.3226   0.02643   0.01844  -0.0858   0.2314   1.0000
   9.000   1.3329   0.02773   0.01974  -0.0835   0.2052   1.0000
   9.250   1.3411   0.02915   0.02111  -0.0810   0.1804   1.0000
   9.500   1.3466   0.03070   0.02253  -0.0782   0.1574   1.0000
   9.750   1.3490   0.03225   0.02412  -0.0749   0.1360   1.0000
  10.000   1.3513   0.03415   0.02589  -0.0720   0.1175   1.0000
  10.250   1.3553   0.03618   0.02797  -0.0693   0.1006   1.0000
  10.500   1.3599   0.03834   0.03013  -0.0668   0.0869   1.0000
  10.750   1.3656   0.04062   0.03244  -0.0646   0.0756   1.0000
  11.000   1.3748   0.04315   0.03496  -0.0626   0.0662   1.0000
  11.250   1.3849   0.04587   0.03757  -0.0610   0.0571   1.0000
  11.500   1.3864   0.04824   0.04035  -0.0585   0.0517   1.0000
  11.750   1.3948   0.05144   0.04357  -0.0570   0.0453   1.0000
  12.000   1.3951   0.05447   0.04702  -0.0547   0.0416   1.0000
  12.250   1.3935   0.05712   0.04974  -0.0530   0.0378   1.0000
  12.500   1.3920   0.06152   0.05437  -0.0512   0.0349   1.0000
  12.750   1.3830   0.06551   0.05878  -0.0494   0.0339   1.0000
  13.000   1.3716   0.06982   0.06346  -0.0480   0.0330   1.0000
  13.250   1.3571   0.07436   0.06832  -0.0471   0.0322   1.0000
  13.500   1.3413   0.07916   0.07342  -0.0468   0.0315   1.0000
  13.750   1.3236   0.08443   0.07898  -0.0472   0.0313   1.0000
  14.000   1.3041   0.09016   0.08497  -0.0483   0.0311   1.0000
  14.250   1.2815   0.09673   0.09182  -0.0503   0.0315   1.0000
  14.500   1.2577   0.10401   0.09936  -0.0533   0.0322   1.0000
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