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EPPLER 793 AIRFOIL (e793-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: EPPLER 793 AIRFOIL (e793-il)
Reynolds number: 1,000,000
Max Cl/Cd: 129.16 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e793-il-1000000.txt
Download as CSV file: xf-e793-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6845   0.09220   0.08979  -0.0576   1.0000   0.0141
 -15.500  -0.7121   0.08350   0.08095  -0.0627   1.0000   0.0141
 -15.250  -0.7354   0.07602   0.07334  -0.0671   1.0000   0.0141
 -15.000  -0.7585   0.06905   0.06623  -0.0712   1.0000   0.0141
 -14.750  -0.7752   0.06350   0.06057  -0.0742   1.0000   0.0140
 -14.500  -0.7856   0.05916   0.05614  -0.0766   1.0000   0.0142
 -14.250  -0.8003   0.05445   0.05133  -0.0789   1.0000   0.0141
 -14.000  -0.8121   0.05031   0.04709  -0.0808   1.0000   0.0142
 -13.750  -0.8239   0.04641   0.04309  -0.0823   1.0000   0.0143
 -13.500  -0.8321   0.04310   0.03969  -0.0834   1.0000   0.0143
 -13.250  -0.8423   0.03984   0.03634  -0.0841   1.0000   0.0144
 -13.000  -0.8517   0.03700   0.03343  -0.0842   1.0000   0.0144
 -12.750  -0.8630   0.03449   0.03083  -0.0837   1.0000   0.0145
 -12.500  -0.8616   0.03177   0.02801  -0.0859   0.9987   0.0146
 -12.250  -0.8388   0.02910   0.02519  -0.0920   0.9948   0.0147
 -12.000  -0.8111   0.02699   0.02294  -0.0967   0.9915   0.0150
 -11.750  -0.7826   0.02547   0.02131  -0.0997   0.9879   0.0152
 -11.500  -0.7513   0.02425   0.01999  -0.1025   0.9855   0.0153
 -11.250  -0.7181   0.02314   0.01878  -0.1054   0.9837   0.0155
 -11.000  -0.6988   0.02095   0.01648  -0.1066   0.9784   0.0159
 -10.750  -0.6704   0.01968   0.01517  -0.1083   0.9746   0.0162
 -10.500  -0.6378   0.01864   0.01410  -0.1105   0.9722   0.0165
 -10.250  -0.6128   0.01779   0.01321  -0.1109   0.9658   0.0167
 -10.000  -0.5832   0.01695   0.01232  -0.1121   0.9609   0.0170
  -9.750  -0.5547   0.01617   0.01149  -0.1129   0.9551   0.0173
  -9.500  -0.5248   0.01543   0.01069  -0.1139   0.9474   0.0176
  -9.250  -0.4868   0.01469   0.00990  -0.1165   0.9423   0.0180
  -9.000  -0.4485   0.01402   0.00916  -0.1191   0.9339   0.0183
  -8.750  -0.4085   0.01345   0.00851  -0.1220   0.9236   0.0187
  -8.500  -0.3731   0.01285   0.00781  -0.1239   0.9079   0.0189
  -8.250  -0.3454   0.01208   0.00691  -0.1245   0.8876   0.0196
  -8.000  -0.3190   0.01168   0.00641  -0.1245   0.8683   0.0202
  -7.750  -0.2933   0.01139   0.00601  -0.1241   0.8500   0.0208
  -7.500  -0.2678   0.01112   0.00564  -0.1237   0.8323   0.0213
  -7.250  -0.2423   0.01087   0.00528  -0.1233   0.8156   0.0218
  -7.000  -0.2164   0.01065   0.00497  -0.1229   0.7997   0.0223
  -6.750  -0.1908   0.01036   0.00458  -0.1225   0.7843   0.0231
  -6.500  -0.1649   0.01008   0.00421  -0.1221   0.7691   0.0242
  -6.250  -0.1385   0.00988   0.00395  -0.1218   0.7546   0.0254
  -6.000  -0.1119   0.00972   0.00370  -0.1214   0.7404   0.0268
  -5.750  -0.0855   0.00949   0.00342  -0.1211   0.7264   0.0303
  -5.500  -0.0591   0.00919   0.00313  -0.1209   0.7126   0.0439
  -5.250  -0.0328   0.00878   0.00284  -0.1208   0.6993   0.0758
  -5.000  -0.0059   0.00849   0.00262  -0.1207   0.6866   0.1042
  -4.750   0.0209   0.00826   0.00244  -0.1205   0.6742   0.1330
  -4.500   0.0481   0.00805   0.00229  -0.1204   0.6615   0.1617
  -4.250   0.0756   0.00787   0.00217  -0.1204   0.6492   0.1892
  -4.000   0.1032   0.00774   0.00207  -0.1203   0.6379   0.2163
  -3.500   0.1587   0.00757   0.00194  -0.1201   0.6146   0.2622
  -3.250   0.1867   0.00755   0.00189  -0.1200   0.6037   0.2780
  -2.750   0.2428   0.00751   0.00183  -0.1199   0.5824   0.3069
  -2.500   0.2707   0.00751   0.00181  -0.1198   0.5721   0.3197
  -2.250   0.2988   0.00751   0.00180  -0.1197   0.5617   0.3357
  -2.000   0.3270   0.00752   0.00179  -0.1197   0.5525   0.3484
  -1.500   0.3832   0.00756   0.00178  -0.1195   0.5334   0.3685
  -1.000   0.4394   0.00762   0.00180  -0.1194   0.5160   0.3887
  -0.750   0.4672   0.00767   0.00181  -0.1192   0.5073   0.3986
  -0.500   0.4956   0.00769   0.00183  -0.1192   0.4993   0.4094
  -0.250   0.5232   0.00775   0.00186  -0.1191   0.4912   0.4199
   0.250   0.5793   0.00783   0.00193  -0.1190   0.4763   0.4429
   0.500   0.6076   0.00786   0.00197  -0.1190   0.4695   0.4545
   0.750   0.6354   0.00791   0.00202  -0.1189   0.4624   0.4669
   1.000   0.6632   0.00797   0.00208  -0.1188   0.4558   0.4800
   1.250   0.6913   0.00800   0.00213  -0.1187   0.4491   0.4936
   1.500   0.7186   0.00809   0.00220  -0.1186   0.4420   0.5073
   1.750   0.7468   0.00813   0.00227  -0.1185   0.4365   0.5218
   2.000   0.7744   0.00819   0.00234  -0.1184   0.4302   0.5369
   2.250   0.8017   0.00828   0.00243  -0.1183   0.4238   0.5527
   2.500   0.8297   0.00832   0.00251  -0.1182   0.4180   0.5694
   2.750   0.8569   0.00840   0.00261  -0.1180   0.4119   0.5865
   3.000   0.8842   0.00848   0.00271  -0.1179   0.4064   0.6039
   3.250   0.9118   0.00853   0.00281  -0.1178   0.4007   0.6228
   3.500   0.9386   0.00863   0.00293  -0.1175   0.3945   0.6421
   3.750   0.9658   0.00870   0.00304  -0.1174   0.3892   0.6626
   4.000   0.9930   0.00876   0.00316  -0.1172   0.3839   0.6851
   4.250   1.0193   0.00887   0.00330  -0.1169   0.3779   0.7087
   4.500   1.0461   0.00894   0.00343  -0.1166   0.3727   0.7332
   5.250   1.1230   0.00914   0.00388  -0.1152   0.3564   0.8349
   5.500   1.1450   0.00914   0.00402  -0.1139   0.3509   0.8933
   5.750   1.1679   0.00919   0.00414  -0.1128   0.3446   1.0000
   6.000   1.1948   0.00932   0.00427  -0.1126   0.3396   1.0000
   6.250   1.2209   0.00949   0.00442  -0.1123   0.3337   1.0000
   6.500   1.2458   0.00972   0.00461  -0.1118   0.3274   1.0000
   6.750   1.2722   0.00985   0.00476  -0.1116   0.3225   1.0000
   7.000   1.2973   0.01005   0.00494  -0.1112   0.3165   1.0000
   7.250   1.3219   0.01027   0.00514  -0.1106   0.3103   1.0000
   7.500   1.3473   0.01044   0.00531  -0.1102   0.3047   1.0000
   7.750   1.3710   0.01069   0.00553  -0.1095   0.2984   1.0000
   8.000   1.3955   0.01089   0.00574  -0.1090   0.2933   1.0000
   8.250   1.4196   0.01110   0.00595  -0.1084   0.2873   1.0000
   8.500   1.4416   0.01140   0.00621  -0.1074   0.2807   1.0000
   8.750   1.4658   0.01158   0.00642  -0.1068   0.2755   1.0000
   9.000   1.4875   0.01185   0.00668  -0.1058   0.2691   1.0000
   9.250   1.5082   0.01211   0.00694  -0.1046   0.2632   1.0000
   9.500   1.5288   0.01237   0.00719  -0.1034   0.2567   1.0000
   9.750   1.5468   0.01272   0.00752  -0.1018   0.2497   1.0000
  10.000   1.5671   0.01298   0.00780  -0.1005   0.2433   1.0000
  10.250   1.5838   0.01339   0.00818  -0.0987   0.2352   1.0000
  10.500   1.6028   0.01371   0.00850  -0.0973   0.2278   1.0000
  10.750   1.6184   0.01417   0.00893  -0.0954   0.2187   1.0000
  11.000   1.6346   0.01461   0.00936  -0.0937   0.2098   1.0000
  11.250   1.6498   0.01509   0.00983  -0.0918   0.2015   1.0000
  11.500   1.6619   0.01572   0.01041  -0.0896   0.1910   1.0000
  11.750   1.6728   0.01642   0.01106  -0.0872   0.1785   1.0000
  12.000   1.6841   0.01710   0.01173  -0.0850   0.1683   1.0000
  12.250   1.6931   0.01793   0.01252  -0.0825   0.1580   1.0000
  12.500   1.6999   0.01889   0.01345  -0.0800   0.1478   1.0000
  12.750   1.7052   0.01999   0.01450  -0.0774   0.1374   1.0000
  13.000   1.7128   0.02100   0.01552  -0.0752   0.1297   1.0000
  13.250   1.7158   0.02236   0.01685  -0.0728   0.1202   1.0000
  13.500   1.7201   0.02371   0.01820  -0.0706   0.1133   1.0000
  13.750   1.7241   0.02516   0.01966  -0.0687   0.1064   1.0000
  14.000   1.7244   0.02697   0.02146  -0.0667   0.0990   1.0000
  14.250   1.7282   0.02862   0.02313  -0.0651   0.0936   1.0000
  14.500   1.7278   0.03070   0.02522  -0.0635   0.0881   1.0000
  14.750   1.7303   0.03264   0.02720  -0.0623   0.0836   1.0000
  15.000   1.7288   0.03504   0.02962  -0.0611   0.0786   1.0000
  15.250   1.7275   0.03754   0.03216  -0.0602   0.0742   1.0000
  15.500   1.7264   0.04014   0.03480  -0.0594   0.0703   1.0000
  15.750   1.7206   0.04332   0.03801  -0.0588   0.0661   1.0000
  16.000   1.7201   0.04608   0.04085  -0.0585   0.0633   1.0000
  16.250   1.7160   0.04934   0.04416  -0.0583   0.0603   1.0000
  16.500   1.7086   0.05309   0.04795  -0.0584   0.0570   1.0000
  16.750   1.7052   0.05650   0.05143  -0.0586   0.0546   1.0000
  17.000   1.6988   0.06039   0.05539  -0.0590   0.0521   1.0000
  17.250   1.6889   0.06483   0.05988  -0.0597   0.0493   1.0000
  17.500   1.6833   0.06884   0.06397  -0.0604   0.0474   1.0000
  17.750   1.6766   0.07309   0.06830  -0.0613   0.0454   1.0000
  18.000   1.6660   0.07798   0.07325  -0.0625   0.0431   1.0000
  18.250   1.6561   0.08287   0.07821  -0.0638   0.0411   1.0000
  18.500   1.6492   0.08743   0.08285  -0.0652   0.0393   1.0000
  18.750   1.6404   0.09235   0.08784  -0.0667   0.0377   1.0000
  19.000   1.6291   0.09772   0.09328  -0.0686   0.0359   1.0000
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