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RAF 32 MOD AIRFOIL (raf32md-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RAF 32 MOD AIRFOIL (raf32md-il)
Reynolds number: 500,000
Max Cl/Cd: 110.54 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-raf32md-il-500000-n5.txt
Download as CSV file: xf-raf32md-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAF 32 MOD AIRFOIL                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.3962   0.13885   0.13635  -0.0362   1.0000   0.0077
 -13.000  -0.3947   0.13502   0.13253  -0.0371   1.0000   0.0078
 -11.500  -0.7243   0.03325   0.03030  -0.1033   0.9832   0.0083
 -11.250  -0.7089   0.02887   0.02551  -0.1084   0.9784   0.0086
 -11.000  -0.6901   0.02602   0.02231  -0.1108   0.9740   0.0089
 -10.750  -0.6676   0.02377   0.01978  -0.1128   0.9702   0.0092
 -10.500  -0.6395   0.02237   0.01822  -0.1147   0.9683   0.0098
 -10.250  -0.6122   0.02160   0.01737  -0.1157   0.9651   0.0103
 -10.000  -0.5857   0.02065   0.01626  -0.1165   0.9613   0.0109
  -9.750  -0.5570   0.01958   0.01500  -0.1178   0.9586   0.0117
  -9.500  -0.5300   0.01846   0.01365  -0.1186   0.9551   0.0123
  -9.250  -0.5040   0.01771   0.01282  -0.1190   0.9502   0.0131
  -9.000  -0.4729   0.01739   0.01246  -0.1201   0.9472   0.0138
  -8.750  -0.4446   0.01697   0.01196  -0.1206   0.9428   0.0147
  -8.500  -0.4171   0.01645   0.01132  -0.1209   0.9376   0.0157
  -8.250  -0.3867   0.01589   0.01058  -0.1218   0.9340   0.0168
  -8.000  -0.3614   0.01541   0.01006  -0.1217   0.9275   0.0177
  -7.750  -0.3319   0.01518   0.00978  -0.1223   0.9227   0.0186
  -7.500  -0.3046   0.01481   0.00934  -0.1225   0.9170   0.0197
  -7.250  -0.2772   0.01447   0.00890  -0.1226   0.9110   0.0210
  -7.000  -0.2486   0.01416   0.00846  -0.1229   0.9058   0.0222
  -6.750  -0.2221   0.01391   0.00811  -0.1227   0.8990   0.0229
  -6.500  -0.1963   0.01306   0.00713  -0.1227   0.8930   0.0242
  -6.250  -0.1708   0.01256   0.00658  -0.1225   0.8864   0.0254
  -6.000  -0.1440   0.01219   0.00614  -0.1224   0.8800   0.0265
  -5.750  -0.1173   0.01184   0.00570  -0.1223   0.8740   0.0276
  -5.500  -0.0908   0.01151   0.00530  -0.1221   0.8673   0.0288
  -5.250  -0.0638   0.01117   0.00487  -0.1220   0.8615   0.0297
  -5.000  -0.0377   0.01086   0.00449  -0.1217   0.8547   0.0304
  -4.750  -0.0105   0.01063   0.00417  -0.1216   0.8487   0.0312
  -4.500   0.0161   0.01040   0.00388  -0.1214   0.8423   0.0317
  -4.250   0.0427   0.01012   0.00352  -0.1212   0.8359   0.0321
  -4.000   0.0694   0.00982   0.00313  -0.1210   0.8300   0.0329
  -3.750   0.0960   0.00958   0.00283  -0.1208   0.8233   0.0338
  -3.250   0.1500   0.00924   0.00237  -0.1204   0.8108   0.0360
  -3.000   0.1771   0.00910   0.00218  -0.1202   0.8045   0.0379
  -2.750   0.2042   0.00898   0.00202  -0.1200   0.7982   0.0401
  -2.500   0.2312   0.00887   0.00188  -0.1198   0.7915   0.0428
  -2.250   0.2577   0.00862   0.00174  -0.1196   0.7852   0.0787
  -2.000   0.2844   0.00846   0.00166  -0.1194   0.7780   0.1079
  -1.750   0.3111   0.00832   0.00157  -0.1192   0.7715   0.1361
  -1.500   0.3376   0.00814   0.00150  -0.1190   0.7640   0.1740
  -1.250   0.3640   0.00796   0.00147  -0.1188   0.7572   0.2320
  -1.000   0.3906   0.00786   0.00145  -0.1186   0.7494   0.2699
  -0.750   0.4173   0.00781   0.00144  -0.1184   0.7421   0.2980
  -0.500   0.4440   0.00773   0.00144  -0.1182   0.7338   0.3289
  -0.250   0.4702   0.00762   0.00144  -0.1179   0.7260   0.3751
   0.000   0.4960   0.00745   0.00146  -0.1175   0.7173   0.4358
   0.250   0.5209   0.00725   0.00156  -0.1170   0.7090   0.5488
   0.500   0.5469   0.00723   0.00160  -0.1166   0.6999   0.5887
   0.750   0.5730   0.00722   0.00164  -0.1162   0.6909   0.6184
   1.000   0.5986   0.00720   0.00168  -0.1157   0.6819   0.6489
   1.250   0.6241   0.00717   0.00174  -0.1151   0.6723   0.6807
   1.500   0.6495   0.00717   0.00181  -0.1146   0.6631   0.7111
   1.750   0.6739   0.00714   0.00188  -0.1138   0.6537   0.7556
   2.000   0.6968   0.00701   0.00196  -0.1126   0.6442   0.8288
   2.250   0.7441   0.00691   0.00205  -0.1168   0.6326   1.0000
   2.500   0.7690   0.00705   0.00213  -0.1162   0.6196   1.0000
   2.750   0.7934   0.00720   0.00222  -0.1154   0.6038   1.0000
   3.000   0.8169   0.00739   0.00233  -0.1145   0.5827   1.0000
   3.250   0.8397   0.00761   0.00245  -0.1135   0.5594   1.0000
   3.500   0.8626   0.00784   0.00258  -0.1125   0.5357   1.0000
   3.750   0.8859   0.00806   0.00273  -0.1116   0.5167   1.0000
   4.000   0.9085   0.00831   0.00290  -0.1105   0.4917   1.0000
   4.250   0.9302   0.00862   0.00310  -0.1094   0.4631   1.0000
   4.500   0.9502   0.00901   0.00333  -0.1079   0.4265   1.0000
   4.750   0.9692   0.00949   0.00362  -0.1063   0.3838   1.0000
   5.000   0.9875   0.01003   0.00395  -0.1046   0.3384   1.0000
   5.250   1.0052   0.01062   0.00433  -0.1028   0.2914   1.0000
   5.500   1.0209   0.01135   0.00478  -0.1008   0.2355   1.0000
   6.000   1.0503   0.01292   0.00582  -0.0964   0.1334   1.0000
   6.250   1.0648   0.01369   0.00635  -0.0942   0.0889   1.0000
   6.500   1.0820   0.01426   0.00681  -0.0925   0.0689   1.0000
   6.750   1.1002   0.01469   0.00722  -0.0908   0.0593   1.0000
   7.000   1.1175   0.01513   0.00764  -0.0890   0.0526   1.0000
   7.250   1.1358   0.01551   0.00804  -0.0873   0.0477   1.0000
   7.500   1.1527   0.01597   0.00850  -0.0855   0.0418   1.0000
   7.750   1.1698   0.01642   0.00896  -0.0837   0.0365   1.0000
   8.000   1.1855   0.01695   0.00946  -0.0818   0.0296   1.0000
   8.250   1.2005   0.01753   0.01001  -0.0798   0.0224   1.0000
   8.500   1.2150   0.01815   0.01062  -0.0777   0.0180   1.0000
   8.750   1.2297   0.01877   0.01127  -0.0757   0.0157   1.0000
   9.000   1.2439   0.01943   0.01197  -0.0737   0.0140   1.0000
   9.250   1.2567   0.02019   0.01278  -0.0715   0.0126   1.0000
   9.500   1.2694   0.02097   0.01362  -0.0695   0.0117   1.0000
   9.750   1.2831   0.02169   0.01441  -0.0676   0.0109   1.0000
  10.000   1.2959   0.02249   0.01529  -0.0657   0.0103   1.0000
  10.250   1.3079   0.02336   0.01622  -0.0637   0.0097   1.0000
  10.500   1.3185   0.02435   0.01727  -0.0617   0.0092   1.0000
  10.750   1.3263   0.02558   0.01857  -0.0594   0.0086   1.0000
  11.000   1.3353   0.02675   0.01982  -0.0574   0.0083   1.0000
  11.250   1.3452   0.02787   0.02106  -0.0556   0.0081   1.0000
  11.500   1.3541   0.02911   0.02239  -0.0538   0.0078   1.0000
  11.750   1.3627   0.03041   0.02378  -0.0521   0.0075   1.0000
  12.000   1.3707   0.03179   0.02524  -0.0504   0.0072   1.0000
  12.250   1.3798   0.03310   0.02663  -0.0490   0.0069   1.0000
  12.500   1.3869   0.03463   0.02824  -0.0475   0.0066   1.0000
  12.750   1.3932   0.03626   0.02995  -0.0461   0.0064   1.0000
  13.000   1.3966   0.03821   0.03199  -0.0446   0.0062   1.0000
  13.250   1.3954   0.04069   0.03457  -0.0430   0.0060   1.0000
  13.500   1.4001   0.04265   0.03664  -0.0419   0.0059   1.0000
  13.750   1.4035   0.04480   0.03894  -0.0409   0.0058   1.0000
  14.000   1.4056   0.04717   0.04144  -0.0400   0.0057   1.0000
  14.250   1.4073   0.04967   0.04407  -0.0392   0.0056   1.0000
  14.500   1.4077   0.05240   0.04693  -0.0386   0.0055   1.0000
  14.750   1.4078   0.05525   0.04991  -0.0382   0.0053   1.0000
  15.000   1.4060   0.05844   0.05324  -0.0380   0.0052   1.0000
  15.250   1.4050   0.06165   0.05658  -0.0380   0.0051   1.0000
  15.500   1.4021   0.06520   0.06027  -0.0382   0.0050   1.0000
  15.750   1.3975   0.06913   0.06434  -0.0387   0.0050   1.0000
  16.000   1.3942   0.07303   0.06837  -0.0395   0.0049   1.0000
  16.250   1.3877   0.07752   0.07301  -0.0405   0.0048   1.0000
  16.500   1.3823   0.08199   0.07762  -0.0418   0.0047   1.0000
  16.750   1.3740   0.08708   0.08286  -0.0434   0.0047   1.0000
  17.000   1.3663   0.09228   0.08820  -0.0454   0.0046   1.0000
  17.250   1.3561   0.09807   0.09414  -0.0477   0.0046   1.0000
  17.500   1.3445   0.10428   0.10051  -0.0505   0.0046   1.0000
  17.750   1.3342   0.11051   0.10688  -0.0535   0.0045   1.0000
  18.000   1.3208   0.11755   0.11407  -0.0571   0.0045   1.0000
  18.250   1.3096   0.12436   0.12102  -0.0608   0.0045   1.0000
  18.500   1.2943   0.13220   0.12902  -0.0652   0.0045   1.0000
  18.750   1.2809   0.13992   0.13688  -0.0698   0.0045   1.0000
  19.000   1.2655   0.14838   0.14550  -0.0749   0.0045   1.0000
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