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RAE 104 AIRFOIL (rae104-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE 104 AIRFOIL (rae104-il)
Reynolds number: 1,000,000
Max Cl/Cd: 61.92 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae104-il-1000000-n5.txt
Download as CSV file: xf-rae104-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 104 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.0635   0.05398   0.05165  -0.0414   1.0000   0.0034
 -14.500  -1.0754   0.04929   0.04682  -0.0434   1.0000   0.0035
 -14.250  -1.0999   0.04367   0.04097  -0.0446   1.0000   0.0035
 -14.000  -1.0993   0.04138   0.03859  -0.0446   1.0000   0.0036
 -13.750  -1.1078   0.03833   0.03538  -0.0439   1.0000   0.0036
 -13.500  -1.1152   0.03560   0.03248  -0.0426   1.0000   0.0036
 -13.250  -1.1206   0.03323   0.02993  -0.0408   1.0000   0.0036
 -13.000  -1.1245   0.03113   0.02766  -0.0384   1.0000   0.0037
 -12.750  -1.1153   0.03023   0.02669  -0.0369   1.0000   0.0039
 -12.500  -1.1145   0.02867   0.02496  -0.0342   1.0000   0.0039
 -12.250  -1.1139   0.02714   0.02327  -0.0311   1.0000   0.0040
 -12.000  -1.1056   0.02632   0.02234  -0.0286   1.0000   0.0041
 -11.750  -1.1043   0.02492   0.02077  -0.0249   1.0000   0.0041
 -11.500  -1.0934   0.02401   0.01974  -0.0227   1.0000   0.0042
 -11.250  -1.0843   0.02274   0.01831  -0.0201   1.0000   0.0043
 -11.000  -1.0710   0.02185   0.01729  -0.0182   1.0000   0.0044
 -10.750  -1.0581   0.02085   0.01616  -0.0161   1.0000   0.0044
 -10.500  -1.0427   0.02009   0.01530  -0.0143   1.0000   0.0045
 -10.250  -1.0273   0.01930   0.01439  -0.0125   1.0000   0.0046
 -10.000  -1.0109   0.01860   0.01360  -0.0108   1.0000   0.0046
  -9.750  -0.9947   0.01787   0.01277  -0.0090   1.0000   0.0047
  -9.500  -0.9821   0.01678   0.01153  -0.0065   1.0000   0.0049
  -9.250  -0.9660   0.01610   0.01077  -0.0046   1.0000   0.0051
  -9.000  -0.9423   0.01543   0.01004  -0.0044   0.9987   0.0054
  -8.500  -0.8874   0.01434   0.00884  -0.0053   0.9896   0.0059
  -8.250  -0.8579   0.01386   0.00832  -0.0061   0.9852   0.0063
  -8.000  -0.8280   0.01339   0.00778  -0.0070   0.9805   0.0067
  -7.750  -0.7965   0.01292   0.00725  -0.0082   0.9751   0.0070
  -7.500  -0.7630   0.01246   0.00673  -0.0099   0.9700   0.0072
  -7.250  -0.7319   0.01182   0.00602  -0.0111   0.9613   0.0081
  -7.000  -0.6990   0.01139   0.00556  -0.0126   0.9523   0.0089
  -6.750  -0.6679   0.01103   0.00514  -0.0137   0.9404   0.0095
  -6.500  -0.6400   0.01074   0.00478  -0.0139   0.9260   0.0103
  -6.250  -0.6143   0.01050   0.00447  -0.0136   0.9113   0.0108
  -6.000  -0.5905   0.01021   0.00411  -0.0130   0.8974   0.0123
  -5.500  -0.5419   0.00979   0.00359  -0.0118   0.8737   0.0155
  -5.250  -0.5174   0.00958   0.00332  -0.0112   0.8635   0.0175
  -5.000  -0.4931   0.00937   0.00309  -0.0106   0.8540   0.0207
  -4.750  -0.4681   0.00919   0.00288  -0.0101   0.8452   0.0240
  -4.500  -0.4434   0.00898   0.00268  -0.0096   0.8378   0.0302
  -4.250  -0.4183   0.00880   0.00248  -0.0092   0.8306   0.0372
  -4.000  -0.3931   0.00862   0.00231  -0.0088   0.8244   0.0466
  -3.750  -0.3683   0.00839   0.00213  -0.0083   0.8181   0.0640
  -3.500  -0.3434   0.00818   0.00197  -0.0078   0.8126   0.0844
  -3.250  -0.3190   0.00789   0.00180  -0.0073   0.8071   0.1185
  -3.000  -0.2950   0.00760   0.00164  -0.0067   0.8017   0.1618
  -2.750  -0.2715   0.00725   0.00149  -0.0061   0.7968   0.2181
  -2.500  -0.2485   0.00685   0.00133  -0.0053   0.7916   0.2897
  -2.250  -0.2263   0.00641   0.00117  -0.0045   0.7868   0.3729
  -2.000  -0.2045   0.00595   0.00102  -0.0035   0.7825   0.4645
  -1.750  -0.1839   0.00543   0.00088  -0.0022   0.7776   0.5708
  -1.500  -0.1608   0.00518   0.00086  -0.0013   0.7729   0.6437
  -1.250  -0.1346   0.00511   0.00084  -0.0010   0.7684   0.6710
  -1.000  -0.1079   0.00506   0.00083  -0.0007   0.7630   0.6895
  -0.750  -0.0812   0.00504   0.00082  -0.0005   0.7571   0.7035
  -0.500  -0.0540   0.00502   0.00081  -0.0004   0.7503   0.7154
  -0.250  -0.0271   0.00502   0.00080  -0.0001   0.7428   0.7257
   0.000   0.0000   0.00501   0.00080   0.0000   0.7344   0.7344
   0.250   0.0271   0.00502   0.00080   0.0001   0.7256   0.7428
   0.500   0.0540   0.00502   0.00081   0.0004   0.7154   0.7503
   0.750   0.0812   0.00504   0.00082   0.0005   0.7036   0.7571
   1.000   0.1079   0.00506   0.00083   0.0007   0.6892   0.7630
   1.250   0.1346   0.00511   0.00084   0.0009   0.6710   0.7684
   1.500   0.1608   0.00518   0.00086   0.0013   0.6443   0.7729
   1.750   0.1839   0.00543   0.00088   0.0022   0.5709   0.7777
   2.000   0.2044   0.00595   0.00102   0.0035   0.4630   0.7825
   2.250   0.2265   0.00640   0.00117   0.0044   0.3761   0.7868
   2.500   0.2484   0.00686   0.00133   0.0054   0.2866   0.7916
   2.750   0.2715   0.00725   0.00148   0.0061   0.2190   0.7968
   3.000   0.2949   0.00760   0.00164   0.0067   0.1609   0.8017
   3.250   0.3190   0.00790   0.00180   0.0073   0.1179   0.8070
   3.500   0.3435   0.00818   0.00197   0.0078   0.0848   0.8125
   3.750   0.3683   0.00839   0.00213   0.0083   0.0641   0.8180
   4.000   0.3931   0.00862   0.00231   0.0088   0.0469   0.8244
   4.250   0.4183   0.00880   0.00248   0.0092   0.0373   0.8306
   4.500   0.4434   0.00899   0.00268   0.0096   0.0301   0.8378
   4.750   0.4681   0.00919   0.00288   0.0101   0.0241   0.8452
   5.000   0.4931   0.00936   0.00309   0.0106   0.0208   0.8540
   5.250   0.5175   0.00957   0.00332   0.0112   0.0179   0.8634
   5.500   0.5419   0.00978   0.00358   0.0118   0.0155   0.8737
   6.000   0.5905   0.01020   0.00410   0.0130   0.0123   0.8975
   6.250   0.6143   0.01051   0.00447   0.0137   0.0108   0.9115
   6.500   0.6400   0.01074   0.00478   0.0139   0.0103   0.9262
   6.750   0.6679   0.01102   0.00515   0.0137   0.0095   0.9405
   7.000   0.6990   0.01139   0.00556   0.0126   0.0088   0.9524
   7.250   0.7319   0.01182   0.00602   0.0111   0.0080   0.9614
   7.500   0.7629   0.01246   0.00673   0.0099   0.0073   0.9700
   7.750   0.7966   0.01290   0.00723   0.0083   0.0070   0.9751
   8.000   0.8277   0.01340   0.00780   0.0071   0.0067   0.9806
   8.250   0.8578   0.01388   0.00833   0.0061   0.0062   0.9852
   8.500   0.8872   0.01436   0.00887   0.0053   0.0059   0.9897
   9.000   0.9422   0.01544   0.01005   0.0044   0.0053   0.9987
   9.250   0.9660   0.01610   0.01078   0.0046   0.0051   1.0000
   9.500   0.9822   0.01677   0.01152   0.0065   0.0050   1.0000
   9.750   0.9955   0.01779   0.01268   0.0088   0.0047   1.0000
  10.000   1.0107   0.01862   0.01362   0.0108   0.0046   1.0000
  10.250   1.0256   0.01949   0.01460   0.0127   0.0046   1.0000
  10.500   1.0423   0.02013   0.01534   0.0144   0.0045   1.0000
  10.750   1.0571   0.02096   0.01629   0.0162   0.0045   1.0000
  11.000   1.0699   0.02197   0.01743   0.0183   0.0044   1.0000
  11.250   1.0835   0.02283   0.01841   0.0203   0.0043   1.0000
  11.500   1.0955   0.02380   0.01950   0.0224   0.0042   1.0000
  11.750   1.1049   0.02487   0.02071   0.0248   0.0041   1.0000
  12.000   1.1090   0.02605   0.02203   0.0281   0.0041   1.0000
  12.250   1.1150   0.02707   0.02319   0.0309   0.0039   1.0000
  12.500   1.1150   0.02864   0.02494   0.0341   0.0039   1.0000
  12.750   1.1153   0.03026   0.02672   0.0368   0.0038   1.0000
  13.000   1.1120   0.03227   0.02891   0.0394   0.0038   1.0000
  13.250   1.1168   0.03361   0.03035   0.0410   0.0037   1.0000
  13.500   1.1142   0.03573   0.03262   0.0426   0.0036   1.0000
  13.750   1.1156   0.03759   0.03459   0.0436   0.0036   1.0000
  14.000   1.1098   0.04031   0.03746   0.0444   0.0035   1.0000
  14.250   1.0993   0.04382   0.04113   0.0445   0.0035   1.0000
  14.500   1.0602   0.05147   0.04909   0.0424   0.0035   1.0000
  14.750   1.0519   0.05589   0.05363   0.0401   0.0035   1.0000
  15.000   1.0338   0.06293   0.06082   0.0354   0.0034   1.0000
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