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EPPLER 793 AIRFOIL (e793-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 793 AIRFOIL (e793-il)
Reynolds number: 500,000
Max Cl/Cd: 100.76 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e793-il-500000-n5.txt
Download as CSV file: xf-e793-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6373   0.10465   0.10149  -0.0515   1.0000   0.0132
 -15.750  -0.6707   0.09444   0.09111  -0.0570   1.0000   0.0132
 -15.500  -0.6878   0.08767   0.08423  -0.0607   1.0000   0.0133
 -15.250  -0.7028   0.08155   0.07800  -0.0640   1.0000   0.0133
 -15.000  -0.7182   0.07561   0.07195  -0.0671   1.0000   0.0133
 -14.750  -0.7307   0.07041   0.06666  -0.0698   1.0000   0.0133
 -14.500  -0.7391   0.06604   0.06223  -0.0721   1.0000   0.0135
 -14.250  -0.7506   0.06155   0.05765  -0.0743   1.0000   0.0135
 -14.000  -0.7613   0.05735   0.05335  -0.0761   1.0000   0.0136
 -13.750  -0.7713   0.05341   0.04933  -0.0778   1.0000   0.0136
 -13.500  -0.7791   0.04987   0.04571  -0.0791   1.0000   0.0137
 -13.250  -0.7883   0.04639   0.04215  -0.0802   1.0000   0.0138
 -13.000  -0.7962   0.04324   0.03893  -0.0809   1.0000   0.0139
 -12.750  -0.8044   0.04030   0.03591  -0.0813   1.0000   0.0140
 -12.500  -0.8152   0.03750   0.03303  -0.0810   1.0000   0.0140
 -12.250  -0.8007   0.03442   0.02984  -0.0858   0.9972   0.0142
 -12.000  -0.7811   0.03154   0.02682  -0.0911   0.9930   0.0144
 -11.750  -0.7645   0.02895   0.02410  -0.0955   0.9864   0.0145
 -11.500  -0.7380   0.02687   0.02187  -0.0999   0.9817   0.0148
 -11.250  -0.7178   0.02532   0.02020  -0.1014   0.9742   0.0149
 -11.000  -0.6950   0.02402   0.01880  -0.1027   0.9673   0.0151
 -10.500  -0.6490   0.02190   0.01648  -0.1041   0.9500   0.0154
 -10.250  -0.6215   0.02057   0.01509  -0.1058   0.9435   0.0157
 -10.000  -0.5935   0.01947   0.01393  -0.1072   0.9345   0.0160
  -9.750  -0.5557   0.01849   0.01288  -0.1103   0.9291   0.0163
  -9.500  -0.5184   0.01764   0.01197  -0.1132   0.9198   0.0168
  -9.250  -0.4781   0.01685   0.01110  -0.1165   0.9101   0.0173
  -9.000  -0.4398   0.01615   0.01028  -0.1193   0.8966   0.0178
  -8.750  -0.4071   0.01555   0.00956  -0.1208   0.8794   0.0183
  -8.500  -0.3784   0.01505   0.00893  -0.1213   0.8607   0.0186
  -8.250  -0.3523   0.01459   0.00834  -0.1214   0.8426   0.0189
  -8.000  -0.3275   0.01408   0.00771  -0.1212   0.8252   0.0195
  -7.750  -0.3025   0.01368   0.00722  -0.1209   0.8088   0.0200
  -7.500  -0.2773   0.01335   0.00678  -0.1205   0.7932   0.0206
  -7.250  -0.2520   0.01306   0.00637  -0.1201   0.7779   0.0213
  -7.000  -0.2264   0.01279   0.00600  -0.1198   0.7630   0.0220
  -6.750  -0.2006   0.01251   0.00563  -0.1194   0.7487   0.0229
  -6.500  -0.1748   0.01223   0.00527  -0.1191   0.7347   0.0244
  -6.250  -0.1487   0.01200   0.00496  -0.1188   0.7213   0.0261
  -6.000  -0.1226   0.01176   0.00464  -0.1185   0.7082   0.0289
  -5.750  -0.0963   0.01151   0.00435  -0.1183   0.6951   0.0345
  -5.500  -0.0700   0.01122   0.00406  -0.1181   0.6822   0.0467
  -5.250  -0.0435   0.01097   0.00381  -0.1179   0.6701   0.0618
  -5.000  -0.0169   0.01073   0.00357  -0.1177   0.6581   0.0796
  -4.750   0.0097   0.01047   0.00335  -0.1176   0.6457   0.1025
  -4.500   0.0367   0.01023   0.00315  -0.1175   0.6343   0.1274
  -4.250   0.0635   0.01000   0.00298  -0.1174   0.6231   0.1570
  -4.000   0.0906   0.00981   0.00284  -0.1173   0.6117   0.1867
  -3.750   0.1181   0.00968   0.00273  -0.1172   0.6013   0.2118
  -3.500   0.1453   0.00958   0.00264  -0.1171   0.5908   0.2361
  -3.250   0.1730   0.00950   0.00258  -0.1170   0.5802   0.2596
  -3.000   0.2006   0.00945   0.00253  -0.1169   0.5705   0.2793
  -2.750   0.2282   0.00942   0.00249  -0.1168   0.5608   0.2980
  -2.500   0.2561   0.00940   0.00246  -0.1166   0.5514   0.3128
  -2.000   0.3116   0.00941   0.00241  -0.1164   0.5333   0.3350
  -1.750   0.3391   0.00945   0.00239  -0.1162   0.5247   0.3451
  -1.500   0.3672   0.00945   0.00238  -0.1161   0.5161   0.3555
  -1.250   0.3946   0.00950   0.00238  -0.1160   0.5078   0.3649
  -1.000   0.4227   0.00952   0.00239  -0.1159   0.5002   0.3750
  -0.750   0.4502   0.00956   0.00240  -0.1157   0.4923   0.3845
  -0.500   0.4781   0.00960   0.00242  -0.1156   0.4848   0.3945
  -0.250   0.5056   0.00964   0.00245  -0.1155   0.4773   0.4045
   0.000   0.5334   0.00969   0.00248  -0.1154   0.4708   0.4146
   0.250   0.5611   0.00973   0.00252  -0.1153   0.4635   0.4254
   0.500   0.5883   0.00980   0.00257  -0.1151   0.4567   0.4358
   0.750   0.6162   0.00985   0.00262  -0.1150   0.4503   0.4473
   1.000   0.6434   0.00992   0.00269  -0.1148   0.4437   0.4586
   1.250   0.6709   0.00998   0.00276  -0.1147   0.4377   0.4706
   1.750   0.7252   0.01014   0.00293  -0.1143   0.4252   0.4966
   2.000   0.7528   0.01020   0.00302  -0.1142   0.4196   0.5101
   2.250   0.7799   0.01028   0.00311  -0.1140   0.4134   0.5238
   2.500   0.8066   0.01039   0.00322  -0.1137   0.4076   0.5386
   3.000   0.8608   0.01055   0.00345  -0.1133   0.3965   0.5690
   3.250   0.8871   0.01066   0.00359  -0.1130   0.3910   0.5858
   3.500   0.9141   0.01074   0.00371  -0.1128   0.3853   0.6026
   3.750   0.9405   0.01085   0.00386  -0.1125   0.3797   0.6195
   4.000   0.9665   0.01097   0.00402  -0.1121   0.3749   0.6383
   4.250   0.9931   0.01106   0.00417  -0.1119   0.3696   0.6587
   4.500   1.0188   0.01117   0.00434  -0.1114   0.3637   0.6796
   4.750   1.0441   0.01131   0.00452  -0.1110   0.3587   0.7018
   5.000   1.0701   0.01139   0.00469  -0.1106   0.3539   0.7276
   5.250   1.0949   0.01151   0.00489  -0.1100   0.3485   0.7558
   5.500   1.1185   0.01164   0.00509  -0.1091   0.3432   0.7885
   5.750   1.1419   0.01169   0.00528  -0.1082   0.3385   0.8303
   6.000   1.1597   0.01169   0.00545  -0.1060   0.3335   0.8996
   6.500   1.2105   0.01202   0.00581  -0.1051   0.3225   1.0000
   6.750   1.2347   0.01226   0.00603  -0.1045   0.3161   1.0000
   7.000   1.2583   0.01252   0.00627  -0.1039   0.3106   1.0000
   7.250   1.2827   0.01273   0.00650  -0.1033   0.3048   1.0000
   7.500   1.3053   0.01301   0.00676  -0.1025   0.2986   1.0000
   7.750   1.3284   0.01327   0.00702  -0.1017   0.2931   1.0000
   8.000   1.3507   0.01353   0.00729  -0.1008   0.2865   1.0000
   8.250   1.3704   0.01385   0.00759  -0.0995   0.2804   1.0000
   8.500   1.3918   0.01410   0.00787  -0.0984   0.2741   1.0000
   8.750   1.4107   0.01444   0.00820  -0.0970   0.2677   1.0000
   9.000   1.4304   0.01476   0.00853  -0.0957   0.2620   1.0000
   9.250   1.4495   0.01511   0.00889  -0.0943   0.2552   1.0000
   9.500   1.4668   0.01552   0.00930  -0.0927   0.2489   1.0000
   9.750   1.4854   0.01589   0.00969  -0.0913   0.2418   1.0000
  10.000   1.5010   0.01638   0.01017  -0.0895   0.2350   1.0000
  10.250   1.5187   0.01680   0.01061  -0.0880   0.2280   1.0000
  10.500   1.5325   0.01738   0.01118  -0.0860   0.2204   1.0000
  10.750   1.5483   0.01789   0.01171  -0.0844   0.2124   1.0000
  11.000   1.5605   0.01858   0.01238  -0.0824   0.2040   1.0000
  11.250   1.5729   0.01927   0.01309  -0.0805   0.1948   1.0000
  11.500   1.5839   0.02007   0.01388  -0.0785   0.1862   1.0000
  11.750   1.5920   0.02105   0.01484  -0.0762   0.1764   1.0000
  12.000   1.5998   0.02209   0.01588  -0.0741   0.1657   1.0000
  12.250   1.6062   0.02328   0.01705  -0.0720   0.1558   1.0000
  12.500   1.6115   0.02459   0.01837  -0.0700   0.1477   1.0000
  12.750   1.6162   0.02603   0.01981  -0.0681   0.1390   1.0000
  13.000   1.6207   0.02756   0.02136  -0.0664   0.1322   1.0000
  13.250   1.6233   0.02932   0.02313  -0.0648   0.1250   1.0000
  13.500   1.6258   0.03117   0.02502  -0.0633   0.1182   1.0000
  13.750   1.6247   0.03344   0.02729  -0.0620   0.1111   1.0000
  14.000   1.6263   0.03557   0.02947  -0.0609   0.1051   1.0000
  14.250   1.6233   0.03825   0.03217  -0.0599   0.0989   1.0000
  14.500   1.6233   0.04076   0.03474  -0.0592   0.0937   1.0000
  14.750   1.6206   0.04363   0.03766  -0.0587   0.0891   1.0000
  15.000   1.6171   0.04673   0.04080  -0.0583   0.0843   1.0000
  15.250   1.6125   0.05007   0.04419  -0.0582   0.0793   1.0000
  15.500   1.6063   0.05371   0.04788  -0.0582   0.0756   1.0000
  15.750   1.6035   0.05706   0.05131  -0.0584   0.0720   1.0000
  16.000   1.5969   0.06101   0.05532  -0.0588   0.0683   1.0000
  16.250   1.5894   0.06517   0.05955  -0.0595   0.0654   1.0000
  16.500   1.5849   0.06906   0.06352  -0.0601   0.0623   1.0000
  16.750   1.5772   0.07347   0.06800  -0.0611   0.0590   1.0000
  17.000   1.5681   0.07818   0.07277  -0.0622   0.0563   1.0000
  17.250   1.5625   0.08247   0.07715  -0.0633   0.0537   1.0000
  17.500   1.5539   0.08731   0.08205  -0.0647   0.0506   1.0000
  17.750   1.5444   0.09237   0.08718  -0.0663   0.0481   1.0000
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