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RAF 32 MOD AIRFOIL (raf32md-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RAF 32 MOD AIRFOIL (raf32md-il)
Reynolds number: 1,000,000
Max Cl/Cd: 144.39 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-raf32md-il-1000000.txt
Download as CSV file: xf-raf32md-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.2954   0.12105   0.11949  -0.0395   0.9995   0.0143
 -12.000  -0.2888   0.11744   0.11588  -0.0416   0.9989   0.0149
 -11.750  -0.7925   0.02710   0.02425  -0.1040   0.9879   0.0103
 -11.500  -0.7664   0.02500   0.02198  -0.1070   0.9858   0.0107
 -11.250  -0.7348   0.02432   0.02125  -0.1091   0.9848   0.0111
 -11.000  -0.7030   0.02354   0.02040  -0.1112   0.9838   0.0114
 -10.750  -0.6792   0.02243   0.01916  -0.1118   0.9801   0.0118
 -10.500  -0.6519   0.02133   0.01791  -0.1131   0.9773   0.0122
 -10.250  -0.6220   0.02029   0.01672  -0.1147   0.9754   0.0127
 -10.000  -0.5904   0.01944   0.01572  -0.1164   0.9740   0.0131
  -9.750  -0.5610   0.01759   0.01364  -0.1186   0.9727   0.0139
  -9.500  -0.5262   0.01744   0.01350  -0.1204   0.9717   0.0144
  -9.250  -0.4946   0.01720   0.01322  -0.1215   0.9696   0.0149
  -9.000  -0.4686   0.01674   0.01269  -0.1215   0.9647   0.0155
  -8.750  -0.4387   0.01615   0.01198  -0.1224   0.9614   0.0163
  -8.500  -0.4074   0.01564   0.01136  -0.1235   0.9587   0.0168
  -8.250  -0.3829   0.01432   0.00986  -0.1236   0.9536   0.0176
  -8.000  -0.3565   0.01395   0.00947  -0.1236   0.9479   0.0183
  -7.750  -0.3260   0.01381   0.00932  -0.1244   0.9440   0.0191
  -7.500  -0.2997   0.01357   0.00901  -0.1243   0.9378   0.0199
  -7.250  -0.2728   0.01321   0.00856  -0.1242   0.9318   0.0208
  -7.000  -0.2449   0.01290   0.00817  -0.1243   0.9263   0.0215
  -6.750  -0.2182   0.01288   0.00808  -0.1240   0.9194   0.0219
  -6.500  -0.1953   0.01136   0.00643  -0.1236   0.9129   0.0235
  -6.250  -0.1699   0.01106   0.00612  -0.1233   0.9057   0.0245
  -6.000  -0.1429   0.01073   0.00571  -0.1232   0.8996   0.0254
  -5.750  -0.1172   0.01038   0.00531  -0.1228   0.8926   0.0263
  -5.500  -0.0904   0.01010   0.00496  -0.1226   0.8862   0.0272
  -5.250  -0.0636   0.00994   0.00475  -0.1224   0.8796   0.0280
  -5.000  -0.0366   0.00977   0.00452  -0.1222   0.8731   0.0284
  -4.750  -0.0128   0.00892   0.00355  -0.1216   0.8665   0.0298
  -4.500   0.0131   0.00856   0.00314  -0.1212   0.8597   0.0310
  -4.250   0.0398   0.00832   0.00284  -0.1210   0.8537   0.0321
  -4.000   0.0664   0.00809   0.00257  -0.1207   0.8471   0.0331
  -3.750   0.0934   0.00792   0.00232  -0.1205   0.8410   0.0340
  -3.500   0.1203   0.00774   0.00211  -0.1203   0.8346   0.0352
  -3.250   0.1474   0.00762   0.00193  -0.1201   0.8283   0.0362
  -3.000   0.1745   0.00748   0.00175  -0.1199   0.8222   0.0373
  -2.750   0.2015   0.00734   0.00156  -0.1196   0.8156   0.0399
  -2.500   0.2287   0.00722   0.00142  -0.1194   0.8095   0.0441
  -2.250   0.2549   0.00692   0.00129  -0.1192   0.8028   0.0918
  -1.750   0.3074   0.00642   0.00113  -0.1187   0.7895   0.2064
  -1.500   0.3338   0.00624   0.00111  -0.1185   0.7827   0.2707
  -1.250   0.3608   0.00615   0.00109  -0.1183   0.7758   0.3037
  -1.000   0.3876   0.00608   0.00107  -0.1181   0.7685   0.3351
  -0.750   0.4146   0.00601   0.00106  -0.1179   0.7611   0.3621
  -0.500   0.4413   0.00595   0.00105  -0.1176   0.7533   0.3906
  -0.250   0.4679   0.00585   0.00104  -0.1174   0.7454   0.4298
   0.000   0.4933   0.00567   0.00109  -0.1170   0.7373   0.5233
   0.250   0.5196   0.00558   0.00114  -0.1166   0.7285   0.5865
   0.500   0.5456   0.00555   0.00118  -0.1162   0.7200   0.6263
   0.750   0.5718   0.00551   0.00121  -0.1158   0.7106   0.6563
   1.000   0.5977   0.00547   0.00125  -0.1153   0.7013   0.6897
   1.250   0.6228   0.00544   0.00130  -0.1147   0.6918   0.7327
   1.500   0.6462   0.00530   0.00136  -0.1136   0.6816   0.8101
   1.750   0.6968   0.00506   0.00144  -0.1186   0.6680   1.0000
   2.000   0.7220   0.00517   0.00149  -0.1180   0.6556   1.0000
   2.250   0.7468   0.00528   0.00154  -0.1173   0.6413   1.0000
   2.500   0.7712   0.00542   0.00161  -0.1166   0.6242   1.0000
   2.750   0.7956   0.00557   0.00169  -0.1158   0.6075   1.0000
   3.000   0.8202   0.00572   0.00177  -0.1151   0.5917   1.0000
   3.250   0.8448   0.00587   0.00187  -0.1144   0.5759   1.0000
   3.500   0.8693   0.00603   0.00197  -0.1137   0.5588   1.0000
   3.750   0.8938   0.00619   0.00209  -0.1130   0.5415   1.0000
   4.000   0.9175   0.00639   0.00221  -0.1122   0.5193   1.0000
   4.250   0.9410   0.00662   0.00236  -0.1113   0.4963   1.0000
   4.500   0.9634   0.00690   0.00253  -0.1103   0.4669   1.0000
   4.750   0.9833   0.00733   0.00276  -0.1088   0.4209   1.0000
   5.000   1.0011   0.00791   0.00306  -0.1069   0.3623   1.0000
   5.250   1.0160   0.00869   0.00346  -0.1046   0.2881   1.0000
   5.500   1.0301   0.00954   0.00394  -0.1022   0.2140   1.0000
   5.750   1.0462   0.01026   0.00438  -0.1002   0.1612   1.0000
   6.000   1.0628   0.01093   0.00481  -0.0983   0.1155   1.0000
   6.250   1.0787   0.01163   0.00528  -0.0962   0.0750   1.0000
   6.500   1.0981   0.01208   0.00565  -0.0947   0.0604   1.0000
   6.750   1.1191   0.01242   0.00598  -0.0935   0.0537   1.0000
   7.000   1.1395   0.01278   0.00633  -0.0922   0.0470   1.0000
   7.250   1.1592   0.01316   0.00668  -0.0908   0.0405   1.0000
   7.500   1.1782   0.01352   0.00702  -0.0893   0.0340   1.0000
   7.750   1.1947   0.01396   0.00743  -0.0872   0.0272   1.0000
   8.000   1.2101   0.01445   0.00789  -0.0850   0.0221   1.0000
   8.250   1.2261   0.01491   0.00834  -0.0829   0.0194   1.0000
   8.500   1.2407   0.01547   0.00892  -0.0806   0.0173   1.0000
   8.750   1.2574   0.01591   0.00940  -0.0788   0.0161   1.0000
   9.000   1.2726   0.01644   0.00995  -0.0767   0.0149   1.0000
   9.250   1.2855   0.01711   0.01066  -0.0743   0.0139   1.0000
   9.500   1.2973   0.01786   0.01147  -0.0718   0.0132   1.0000
   9.750   1.3127   0.01840   0.01207  -0.0700   0.0126   1.0000
  10.000   1.3261   0.01906   0.01279  -0.0679   0.0122   1.0000
  10.250   1.3394   0.01975   0.01351  -0.0659   0.0116   1.0000
  10.500   1.3520   0.02050   0.01432  -0.0638   0.0112   1.0000
  10.750   1.3620   0.02143   0.01530  -0.0615   0.0107   1.0000
  11.000   1.3646   0.02287   0.01684  -0.0583   0.0101   1.0000
  11.250   1.3732   0.02397   0.01802  -0.0561   0.0099   1.0000
  11.500   1.3861   0.02480   0.01890  -0.0545   0.0096   1.0000
  11.750   1.3966   0.02581   0.01999  -0.0526   0.0094   1.0000
  12.000   1.4070   0.02687   0.02112  -0.0509   0.0091   1.0000
  12.250   1.4153   0.02811   0.02244  -0.0490   0.0089   1.0000
  12.500   1.4239   0.02936   0.02376  -0.0473   0.0086   1.0000
  12.750   1.4325   0.03065   0.02511  -0.0457   0.0083   1.0000
  13.000   1.4393   0.03212   0.02665  -0.0441   0.0081   1.0000
  13.250   1.4446   0.03376   0.02836  -0.0425   0.0079   1.0000
  13.500   1.4482   0.03562   0.03029  -0.0409   0.0078   1.0000
  13.750   1.4403   0.03866   0.03347  -0.0388   0.0074   1.0000
  14.000   1.4350   0.04162   0.03657  -0.0370   0.0073   1.0000
  14.250   1.4373   0.04385   0.03892  -0.0359   0.0073   1.0000
  14.500   1.4435   0.04572   0.04088  -0.0352   0.0072   1.0000
  14.750   1.4468   0.04798   0.04326  -0.0344   0.0071   1.0000
  15.000   1.4481   0.05054   0.04593  -0.0338   0.0070   1.0000
  15.250   1.4479   0.05335   0.04886  -0.0334   0.0069   1.0000
  15.500   1.4469   0.05636   0.05199  -0.0331   0.0068   1.0000
  15.750   1.4456   0.05953   0.05528  -0.0331   0.0067   1.0000
  16.000   1.4436   0.06290   0.05876  -0.0333   0.0066   1.0000
  16.250   1.4423   0.06627   0.06224  -0.0337   0.0065   1.0000
  16.500   1.4373   0.07028   0.06638  -0.0344   0.0064   1.0000
  16.750   1.4343   0.07417   0.07037  -0.0353   0.0062   1.0000
  17.000   1.4248   0.07918   0.07553  -0.0366   0.0062   1.0000
  17.250   1.4185   0.08384   0.08032  -0.0382   0.0061   1.0000
  17.500   1.4110   0.08888   0.08547  -0.0401   0.0060   1.0000
  17.750   1.4052   0.09380   0.09049  -0.0421   0.0059   1.0000
  18.000   1.3917   0.10022   0.09707  -0.0449   0.0059   1.0000
  18.250   1.3796   0.10662   0.10360  -0.0480   0.0059   1.0000
  18.500   1.3679   0.11315   0.11025  -0.0513   0.0058   1.0000
  18.750   1.3556   0.12001   0.11723  -0.0550   0.0058   1.0000
  19.000   1.3384   0.12810   0.12548  -0.0595   0.0058   1.0000
  19.250   1.3214   0.13638   0.13392  -0.0644   0.0058   1.0000
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