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EPPLER 793 AIRFOIL (e793-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 793 AIRFOIL (e793-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.98 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e793-il-1000000-n5.txt
Download as CSV file: xf-e793-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 793 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
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.6241   0.15313   0.15097  -0.0276   1.0000   0.0101
 -18.500  -0.6719   0.13829   0.13595  -0.0350   1.0000   0.0103
 -18.250  -0.6973   0.12913   0.12668  -0.0395   1.0000   0.0103
 -18.000  -0.7149   0.12181   0.11928  -0.0432   1.0000   0.0104
 -17.750  -0.7314   0.11493   0.11231  -0.0466   1.0000   0.0104
 -17.500  -0.7448   0.10876   0.10607  -0.0497   1.0000   0.0104
 -17.250  -0.7603   0.10236   0.09959  -0.0529   1.0000   0.0105
 -17.000  -0.7736   0.09649   0.09365  -0.0559   1.0000   0.0105
 -16.750  -0.7888   0.09048   0.08756  -0.0589   1.0000   0.0105
 -16.500  -0.8034   0.08472   0.08171  -0.0618   1.0000   0.0105
 -16.250  -0.8142   0.07959   0.07652  -0.0643   1.0000   0.0106
 -16.000  -0.8263   0.07446   0.07131  -0.0669   1.0000   0.0106
 -15.750  -0.8404   0.06921   0.06598  -0.0695   1.0000   0.0107
 -15.500  -0.8528   0.06439   0.06109  -0.0718   1.0000   0.0107
 -15.250  -0.8653   0.05982   0.05644  -0.0740   1.0000   0.0108
 -15.000  -0.8810   0.05507   0.05161  -0.0761   1.0000   0.0108
 -14.750  -0.8958   0.05061   0.04706  -0.0779   1.0000   0.0108
 -14.500  -0.9051   0.04690   0.04329  -0.0793   1.0000   0.0108
 -14.250  -0.9198   0.04279   0.03909  -0.0806   1.0000   0.0108
 -14.000  -0.9305   0.03927   0.03550  -0.0814   1.0000   0.0109
 -13.750  -0.9282   0.03545   0.03158  -0.0853   0.9990   0.0110
 -13.500  -0.9134   0.03215   0.02818  -0.0903   0.9968   0.0111
 -13.250  -0.8961   0.02893   0.02486  -0.0958   0.9941   0.0112
 -13.000  -0.8824   0.02620   0.02203  -0.1000   0.9898   0.0113
 -12.750  -0.8601   0.02401   0.01974  -0.1046   0.9854   0.0115
 -12.250  -0.8142   0.02147   0.01703  -0.1080   0.9768   0.0118
 -11.750  -0.7689   0.01959   0.01501  -0.1092   0.9641   0.0121
 -11.250  -0.7169   0.01797   0.01326  -0.1107   0.9487   0.0123
 -11.000  -0.6800   0.01718   0.01240  -0.1135   0.9427   0.0124
 -10.750  -0.6376   0.01635   0.01150  -0.1174   0.9350   0.0125
 -10.500  -0.5949   0.01530   0.01035  -0.1217   0.9226   0.0129
 -10.250  -0.5582   0.01465   0.00958  -0.1242   0.9015   0.0132
 -10.000  -0.5308   0.01421   0.00901  -0.1246   0.8777   0.0134
  -9.750  -0.5067   0.01385   0.00852  -0.1242   0.8554   0.0136
  -9.500  -0.4832   0.01352   0.00808  -0.1236   0.8345   0.0138
  -9.250  -0.4596   0.01322   0.00766  -0.1230   0.8158   0.0141
  -9.000  -0.4355   0.01292   0.00726  -0.1225   0.7986   0.0143
  -8.750  -0.4108   0.01265   0.00690  -0.1220   0.7826   0.0147
  -8.500  -0.3858   0.01239   0.00655  -0.1216   0.7675   0.0150
  -8.250  -0.3606   0.01215   0.00621  -0.1212   0.7520   0.0152
  -8.000  -0.3349   0.01192   0.00589  -0.1208   0.7381   0.0154
  -7.750  -0.3095   0.01161   0.00551  -0.1205   0.7247   0.0158
  -7.500  -0.2839   0.01134   0.00515  -0.1201   0.7107   0.0162
  -7.250  -0.2575   0.01111   0.00485  -0.1199   0.6974   0.0167
  -7.000  -0.2309   0.01090   0.00458  -0.1197   0.6850   0.0172
  -6.750  -0.2042   0.01072   0.00433  -0.1194   0.6728   0.0177
  -6.500  -0.1775   0.01057   0.00410  -0.1192   0.6598   0.0182
  -6.250  -0.1502   0.01042   0.00388  -0.1191   0.6475   0.0187
  -6.000  -0.1231   0.01024   0.00365  -0.1189   0.6359   0.0198
  -5.750  -0.0959   0.01009   0.00344  -0.1187   0.6242   0.0211
  -5.500  -0.0684   0.00995   0.00326  -0.1186   0.6127   0.0230
  -5.250  -0.0410   0.00978   0.00306  -0.1185   0.6016   0.0271
  -5.000  -0.0139   0.00956   0.00285  -0.1184   0.5909   0.0400
  -4.750   0.0137   0.00935   0.00267  -0.1184   0.5805   0.0547
  -4.500   0.0413   0.00920   0.00252  -0.1183   0.5707   0.0685
  -4.250   0.0689   0.00903   0.00237  -0.1183   0.5598   0.0861
  -4.000   0.0967   0.00881   0.00223  -0.1183   0.5508   0.1112
  -3.750   0.1242   0.00864   0.00210  -0.1183   0.5414   0.1384
  -3.500   0.1522   0.00844   0.00199  -0.1184   0.5322   0.1704
  -3.250   0.1801   0.00834   0.00192  -0.1184   0.5231   0.1927
  -3.000   0.2083   0.00825   0.00185  -0.1184   0.5149   0.2130
  -2.750   0.2363   0.00818   0.00181  -0.1184   0.5067   0.2343
  -2.500   0.2646   0.00812   0.00177  -0.1184   0.4984   0.2531
  -2.250   0.2926   0.00808   0.00176  -0.1184   0.4904   0.2777
  -2.000   0.3210   0.00804   0.00174  -0.1184   0.4832   0.2959
  -1.750   0.3491   0.00806   0.00174  -0.1183   0.4754   0.3070
  -1.500   0.3775   0.00806   0.00173  -0.1183   0.4685   0.3165
  -1.250   0.4056   0.00809   0.00174  -0.1183   0.4610   0.3260
  -1.000   0.4339   0.00811   0.00175  -0.1183   0.4550   0.3354
  -0.500   0.4901   0.00818   0.00178  -0.1181   0.4410   0.3537
  -0.250   0.5185   0.00820   0.00180  -0.1181   0.4354   0.3620
   0.000   0.5466   0.00824   0.00184  -0.1181   0.4291   0.3718
   0.250   0.5746   0.00829   0.00187  -0.1180   0.4231   0.3805
   0.500   0.6028   0.00832   0.00191  -0.1180   0.4170   0.3903
   0.750   0.6306   0.00838   0.00196  -0.1179   0.4110   0.3997
   1.000   0.6586   0.00844   0.00201  -0.1178   0.4059   0.4096
   1.250   0.6866   0.00848   0.00206  -0.1178   0.4000   0.4198
   1.500   0.7141   0.00856   0.00213  -0.1177   0.3938   0.4300
   1.750   0.7420   0.00861   0.00220  -0.1176   0.3890   0.4412
   2.000   0.7699   0.00866   0.00227  -0.1175   0.3838   0.4521
   2.250   0.7973   0.00875   0.00235  -0.1174   0.3777   0.4640
   2.500   0.8249   0.00881   0.00243  -0.1173   0.3726   0.4766
   2.750   0.8525   0.00888   0.00252  -0.1172   0.3673   0.4890
   3.000   0.8797   0.00897   0.00262  -0.1170   0.3620   0.5016
   3.250   0.9070   0.00905   0.00272  -0.1169   0.3572   0.5159
   3.500   0.9344   0.00913   0.00283  -0.1168   0.3518   0.5298
   3.750   0.9612   0.00923   0.00294  -0.1165   0.3461   0.5436
   4.000   0.9882   0.00932   0.00306  -0.1164   0.3418   0.5588
   4.250   1.0153   0.00941   0.00318  -0.1162   0.3370   0.5743
   4.500   1.0418   0.00953   0.00332  -0.1159   0.3313   0.5892
   4.750   1.0683   0.00964   0.00346  -0.1157   0.3264   0.6057
   5.000   1.0951   0.00973   0.00360  -0.1155   0.3220   0.6244
   5.250   1.1212   0.00985   0.00376  -0.1151   0.3163   0.6431
   5.500   1.1470   0.00999   0.00392  -0.1148   0.3108   0.6616
   5.750   1.1731   0.01010   0.00409  -0.1145   0.3051   0.6829
   6.000   1.1984   0.01025   0.00427  -0.1140   0.2988   0.7076
   6.250   1.2238   0.01037   0.00446  -0.1136   0.2936   0.7327
   6.500   1.2489   0.01049   0.00465  -0.1131   0.2876   0.7622
   6.750   1.2727   0.01065   0.00487  -0.1124   0.2812   0.7988
   7.000   1.2961   0.01072   0.00507  -0.1115   0.2760   0.8471
   7.250   1.3146   0.01069   0.00524  -0.1095   0.2691   1.0000
   7.500   1.3387   0.01093   0.00546  -0.1089   0.2628   1.0000
   7.750   1.3628   0.01116   0.00567  -0.1083   0.2563   1.0000
   8.000   1.3857   0.01144   0.00592  -0.1075   0.2498   1.0000
   8.250   1.4093   0.01166   0.00615  -0.1068   0.2438   1.0000
   8.500   1.4310   0.01197   0.00643  -0.1058   0.2364   1.0000
   8.750   1.4529   0.01223   0.00668  -0.1049   0.2300   1.0000
   9.000   1.4724   0.01255   0.00697  -0.1034   0.2224   1.0000
   9.250   1.4920   0.01284   0.00726  -0.1021   0.2158   1.0000
   9.500   1.5097   0.01322   0.00761  -0.1004   0.2074   1.0000
   9.750   1.5279   0.01357   0.00795  -0.0988   0.1998   1.0000
  10.000   1.5438   0.01403   0.00837  -0.0969   0.1905   1.0000
  10.250   1.5598   0.01448   0.00879  -0.0951   0.1809   1.0000
  10.500   1.5744   0.01500   0.00927  -0.0931   0.1706   1.0000
  10.750   1.5864   0.01564   0.00985  -0.0907   0.1589   1.0000
  11.000   1.5974   0.01633   0.01050  -0.0883   0.1477   1.0000
  11.250   1.6083   0.01704   0.01117  -0.0860   0.1379   1.0000
  11.500   1.6194   0.01775   0.01186  -0.0838   0.1295   1.0000
  11.750   1.6261   0.01870   0.01277  -0.0811   0.1183   1.0000
  12.000   1.6334   0.01967   0.01371  -0.0786   0.1101   1.0000
  12.250   1.6421   0.02060   0.01465  -0.0765   0.1031   1.0000
  12.500   1.6480   0.02174   0.01577  -0.0742   0.0958   1.0000
  12.750   1.6535   0.02297   0.01700  -0.0720   0.0891   1.0000
  13.000   1.6605   0.02418   0.01822  -0.0702   0.0846   1.0000
  13.250   1.6616   0.02586   0.01988  -0.0680   0.0767   1.0000
  13.500   1.6695   0.02715   0.02121  -0.0666   0.0743   1.0000
  13.750   1.6725   0.02887   0.02296  -0.0650   0.0692   1.0000
  14.000   1.6744   0.03079   0.02489  -0.0636   0.0648   1.0000
  14.250   1.6758   0.03284   0.02697  -0.0623   0.0601   1.0000
  14.500   1.6755   0.03515   0.02930  -0.0612   0.0563   1.0000
  14.750   1.6780   0.03730   0.03152  -0.0604   0.0536   1.0000
  15.000   1.6769   0.03991   0.03416  -0.0596   0.0504   1.0000
  15.250   1.6750   0.04270   0.03699  -0.0591   0.0473   1.0000
  15.500   1.6728   0.04565   0.03999  -0.0587   0.0443   1.0000
  16.000   1.6646   0.05230   0.04675  -0.0586   0.0390   1.0000
  16.250   1.6600   0.05585   0.05037  -0.0588   0.0367   1.0000
  16.500   1.6536   0.05975   0.05434  -0.0592   0.0349   1.0000
  16.750   1.6499   0.06343   0.05808  -0.0597   0.0333   1.0000
  17.000   1.6442   0.06744   0.06217  -0.0604   0.0317   1.0000
  17.250   1.6359   0.07191   0.06671  -0.0613   0.0300   1.0000
  17.500   1.6300   0.07617   0.07105  -0.0623   0.0287   1.0000
  17.750   1.6239   0.08051   0.07547  -0.0635   0.0274   1.0000
  18.000   1.6155   0.08529   0.08031  -0.0648   0.0259   1.0000
  18.500   1.6007   0.09479   0.08997  -0.0678   0.0233   1.0000
  18.750   1.5937   0.09955   0.09480  -0.0695   0.0224   1.0000
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