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RAF 32 MOD AIRFOIL (raf32md-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAF 32 MOD AIRFOIL (raf32md-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.34 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-raf32md-il-1000000-n5.txt
Download as CSV file: xf-raf32md-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.4387   0.15191   0.15011  -0.0310   1.0000   0.0044
 -14.500  -0.4386   0.14735   0.14556  -0.0323   1.0000   0.0046
 -13.500  -0.9078   0.03364   0.03110  -0.1028   0.9929   0.0049
 -13.250  -0.8959   0.02914   0.02632  -0.1091   0.9883   0.0050
 -13.000  -0.8753   0.02651   0.02349  -0.1126   0.9862   0.0052
 -12.750  -0.8572   0.02466   0.02149  -0.1138   0.9819   0.0054
 -12.500  -0.8338   0.02302   0.01969  -0.1155   0.9795   0.0055
 -12.250  -0.8074   0.02172   0.01825  -0.1172   0.9779   0.0058
 -12.000  -0.7828   0.02046   0.01684  -0.1183   0.9752   0.0060
 -11.750  -0.7577   0.01938   0.01562  -0.1192   0.9718   0.0062
 -11.500  -0.7302   0.01839   0.01449  -0.1203   0.9694   0.0064
 -11.250  -0.7010   0.01748   0.01343  -0.1217   0.9675   0.0065
 -11.000  -0.6781   0.01645   0.01228  -0.1218   0.9622   0.0070
 -10.750  -0.6500   0.01565   0.01139  -0.1227   0.9588   0.0073
 -10.500  -0.6228   0.01498   0.01063  -0.1232   0.9549   0.0078
 -10.250  -0.5966   0.01437   0.00993  -0.1235   0.9496   0.0082
 -10.000  -0.5682   0.01380   0.00925  -0.1241   0.9455   0.0086
  -9.750  -0.5430   0.01331   0.00865  -0.1239   0.9389   0.0090
  -9.500  -0.5157   0.01277   0.00803  -0.1242   0.9333   0.0098
  -9.250  -0.4903   0.01236   0.00757  -0.1241   0.9260   0.0106
  -9.000  -0.4633   0.01200   0.00714  -0.1241   0.9196   0.0117
  -8.750  -0.4375   0.01165   0.00672  -0.1239   0.9122   0.0124
  -8.500  -0.4107   0.01138   0.00641  -0.1239   0.9056   0.0137
  -8.250  -0.3840   0.01119   0.00621  -0.1238   0.8982   0.0148
  -8.000  -0.3572   0.01100   0.00595  -0.1237   0.8913   0.0159
  -7.750  -0.3308   0.01078   0.00567  -0.1235   0.8840   0.0166
  -7.500  -0.3043   0.01055   0.00538  -0.1233   0.8770   0.0176
  -7.250  -0.2774   0.01043   0.00526  -0.1232   0.8700   0.0186
  -7.000  -0.2504   0.01032   0.00510  -0.1231   0.8630   0.0195
  -6.750  -0.2237   0.01015   0.00488  -0.1229   0.8565   0.0204
  -6.500  -0.1969   0.01002   0.00469  -0.1228   0.8497   0.0214
  -6.250  -0.1699   0.00988   0.00450  -0.1226   0.8435   0.0222
  -6.000  -0.1431   0.00975   0.00432  -0.1225   0.8367   0.0226
  -5.750  -0.1160   0.00967   0.00417  -0.1223   0.8309   0.0230
  -5.500  -0.0899   0.00934   0.00377  -0.1221   0.8245   0.0236
  -5.250  -0.0642   0.00894   0.00329  -0.1218   0.8183   0.0249
  -5.000  -0.0375   0.00871   0.00302  -0.1216   0.8124   0.0259
  -4.750  -0.0108   0.00852   0.00277  -0.1214   0.8060   0.0266
  -4.500   0.0161   0.00837   0.00257  -0.1212   0.8003   0.0274
  -4.250   0.0432   0.00821   0.00237  -0.1210   0.7940   0.0280
  -4.000   0.0700   0.00808   0.00218  -0.1208   0.7879   0.0284
  -3.750   0.0973   0.00794   0.00200  -0.1207   0.7818   0.0289
  -3.500   0.1243   0.00783   0.00184  -0.1205   0.7752   0.0293
  -3.250   0.1515   0.00773   0.00169  -0.1204   0.7692   0.0297
  -3.000   0.1787   0.00763   0.00156  -0.1202   0.7622   0.0301
  -2.750   0.2058   0.00756   0.00144  -0.1200   0.7557   0.0306
  -2.500   0.2331   0.00749   0.00134  -0.1199   0.7483   0.0312
  -2.250   0.2601   0.00744   0.00125  -0.1197   0.7414   0.0317
  -2.000   0.2874   0.00737   0.00116  -0.1195   0.7336   0.0342
  -1.750   0.3143   0.00731   0.00109  -0.1193   0.7261   0.0395
  -1.500   0.3407   0.00708   0.00101  -0.1191   0.7176   0.0888
  -1.250   0.3674   0.00701   0.00097  -0.1189   0.7092   0.1088
  -1.000   0.3941   0.00694   0.00093  -0.1186   0.7003   0.1308
  -0.750   0.4206   0.00681   0.00090  -0.1184   0.6916   0.1712
  -0.500   0.4466   0.00668   0.00090  -0.1181   0.6825   0.2269
  -0.250   0.4732   0.00662   0.00091  -0.1179   0.6731   0.2630
   0.000   0.4997   0.00658   0.00093  -0.1177   0.6639   0.2936
   0.250   0.5261   0.00657   0.00096  -0.1174   0.6544   0.3230
   0.500   0.5527   0.00653   0.00099  -0.1172   0.6453   0.3531
   0.750   0.5787   0.00647   0.00102  -0.1169   0.6359   0.4003
   1.000   0.6037   0.00625   0.00111  -0.1164   0.6266   0.5157
   1.250   0.6298   0.00624   0.00118  -0.1161   0.6174   0.5647
   1.500   0.6557   0.00628   0.00125  -0.1157   0.6070   0.5934
   1.750   0.6813   0.00633   0.00133  -0.1152   0.5937   0.6168
   2.000   0.7069   0.00642   0.00140  -0.1148   0.5790   0.6311
   2.250   0.7323   0.00650   0.00148  -0.1143   0.5641   0.6474
   2.500   0.7564   0.00663   0.00158  -0.1135   0.5396   0.6710
   2.750   0.7794   0.00675   0.00171  -0.1125   0.5135   0.7090
   3.000   0.8016   0.00687   0.00185  -0.1114   0.4868   0.7597
   3.250   0.8236   0.00685   0.00198  -0.1102   0.4695   0.8304
   3.500   0.8629   0.00694   0.00219  -0.1129   0.4324   1.0000
   3.750   0.8841   0.00733   0.00239  -0.1117   0.3914   1.0000
   4.000   0.9061   0.00769   0.00260  -0.1106   0.3576   1.0000
   4.250   0.9263   0.00816   0.00286  -0.1092   0.3125   1.0000
   4.500   0.9448   0.00875   0.00319  -0.1076   0.2578   1.0000
   4.750   0.9641   0.00928   0.00351  -0.1061   0.2130   1.0000
   5.000   0.9833   0.00981   0.00384  -0.1046   0.1729   1.0000
   5.250   1.0023   0.01036   0.00420  -0.1031   0.1346   1.0000
   5.500   1.0192   0.01103   0.00461  -0.1012   0.0867   1.0000
   5.750   1.0389   0.01149   0.00496  -0.0998   0.0639   1.0000
   6.000   1.0610   0.01179   0.00523  -0.0988   0.0569   1.0000
   6.250   1.0826   0.01211   0.00553  -0.0977   0.0496   1.0000
   6.500   1.1045   0.01240   0.00581  -0.0967   0.0452   1.0000
   6.750   1.1252   0.01274   0.00613  -0.0955   0.0397   1.0000
   7.000   1.1463   0.01305   0.00643  -0.0943   0.0353   1.0000
   7.250   1.1654   0.01342   0.00676  -0.0928   0.0294   1.0000
   7.500   1.1824   0.01384   0.00714  -0.0909   0.0217   1.0000
   7.750   1.1988   0.01428   0.00755  -0.0889   0.0161   1.0000
   8.000   1.2154   0.01471   0.00798  -0.0869   0.0135   1.0000
   8.250   1.2324   0.01512   0.00841  -0.0851   0.0118   1.0000
   8.500   1.2498   0.01552   0.00884  -0.0833   0.0108   1.0000
   8.750   1.2661   0.01599   0.00932  -0.0815   0.0098   1.0000
   9.000   1.2813   0.01652   0.00989  -0.0795   0.0088   1.0000
   9.250   1.2974   0.01701   0.01042  -0.0776   0.0083   1.0000
   9.500   1.3134   0.01751   0.01096  -0.0758   0.0079   1.0000
   9.750   1.3288   0.01805   0.01154  -0.0740   0.0075   1.0000
  10.000   1.3436   0.01863   0.01215  -0.0722   0.0070   1.0000
  10.250   1.3576   0.01928   0.01283  -0.0702   0.0067   1.0000
  10.500   1.3700   0.02003   0.01362  -0.0681   0.0061   1.0000
  10.750   1.3832   0.02075   0.01441  -0.0662   0.0059   1.0000
  11.000   1.3969   0.02145   0.01516  -0.0645   0.0056   1.0000
  11.250   1.4095   0.02224   0.01601  -0.0627   0.0054   1.0000
  11.500   1.4217   0.02308   0.01690  -0.0608   0.0053   1.0000
  11.750   1.4334   0.02396   0.01784  -0.0591   0.0051   1.0000
  12.000   1.4444   0.02492   0.01887  -0.0573   0.0049   1.0000
  12.250   1.4556   0.02589   0.01989  -0.0556   0.0047   1.0000
  12.500   1.4651   0.02701   0.02107  -0.0538   0.0045   1.0000
  12.750   1.4735   0.02825   0.02237  -0.0521   0.0044   1.0000
  13.000   1.4801   0.02968   0.02389  -0.0502   0.0042   1.0000
  13.250   1.4852   0.03127   0.02557  -0.0484   0.0041   1.0000
  13.500   1.4935   0.03262   0.02700  -0.0470   0.0040   1.0000
  13.750   1.5012   0.03407   0.02853  -0.0456   0.0039   1.0000
  14.000   1.5069   0.03572   0.03026  -0.0442   0.0039   1.0000
  14.250   1.5122   0.03746   0.03209  -0.0429   0.0038   1.0000
  14.500   1.5177   0.03924   0.03396  -0.0418   0.0037   1.0000
  14.750   1.5218   0.04120   0.03601  -0.0407   0.0036   1.0000
  15.000   1.5240   0.04342   0.03834  -0.0397   0.0036   1.0000
  15.250   1.5287   0.04545   0.04044  -0.0390   0.0034   1.0000
  15.500   1.5311   0.04780   0.04289  -0.0383   0.0034   1.0000
  15.750   1.5312   0.05050   0.04571  -0.0377   0.0033   1.0000
  16.000   1.5357   0.05275   0.04803  -0.0374   0.0032   1.0000
  16.250   1.5344   0.05580   0.05118  -0.0372   0.0032   1.0000
  16.500   1.5316   0.05915   0.05465  -0.0372   0.0031   1.0000
  16.750   1.5321   0.06216   0.05774  -0.0374   0.0031   1.0000
  17.000   1.5295   0.06567   0.06135  -0.0378   0.0030   1.0000
  17.250   1.5235   0.06981   0.06561  -0.0384   0.0029   1.0000
  17.500   1.5171   0.07415   0.07007  -0.0394   0.0029   1.0000
  17.750   1.5094   0.07883   0.07487  -0.0407   0.0029   1.0000
  18.000   1.4989   0.08411   0.08028  -0.0423   0.0029   1.0000
  18.250   1.4883   0.08963   0.08593  -0.0443   0.0028   1.0000
  18.500   1.4758   0.09566   0.09209  -0.0467   0.0028   1.0000
  18.750   1.4586   0.10276   0.09935  -0.0499   0.0027   1.0000
  19.000   1.4432   0.10975   0.10648  -0.0532   0.0027   1.0000
  19.250   1.4286   0.11684   0.11370  -0.0568   0.0027   1.0000
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