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E591 (e591-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E591 (e591-il)
Reynolds number: 1,000,000
Max Cl/Cd: 118.72 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e591-il-1000000-n5.txt
Download as CSV file: xf-e591-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E591                                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4445   0.06857   0.06594  -0.1090   0.9843   0.0096
 -13.250  -0.4669   0.06125   0.05849  -0.1141   0.9805   0.0095
 -13.000  -0.4889   0.05338   0.05049  -0.1213   0.9760   0.0095
 -12.750  -0.5014   0.04615   0.04311  -0.1295   0.9725   0.0095
 -12.250  -0.5359   0.03627   0.03304  -0.1356   0.9507   0.0095
 -12.000  -0.5387   0.03124   0.02787  -0.1411   0.9389   0.0096
 -11.750  -0.5181   0.02642   0.02288  -0.1504   0.9308   0.0097
 -11.500  -0.4781   0.02243   0.01871  -0.1617   0.9249   0.0098
 -11.250  -0.4340   0.02007   0.01618  -0.1700   0.9197   0.0100
 -11.000  -0.3909   0.01873   0.01471  -0.1755   0.9128   0.0101
 -10.750  -0.3399   0.01751   0.01336  -0.1822   0.9068   0.0103
 -10.500  -0.2955   0.01659   0.01230  -0.1870   0.8960   0.0105
 -10.250  -0.2567   0.01586   0.01144  -0.1903   0.8825   0.0105
 -10.000  -0.2248   0.01498   0.01040  -0.1925   0.8657   0.0108
  -9.750  -0.1966   0.01432   0.00961  -0.1935   0.8492   0.0110
  -9.500  -0.1699   0.01384   0.00900  -0.1939   0.8327   0.0112
  -9.250  -0.1440   0.01342   0.00845  -0.1940   0.8166   0.0114
  -9.000  -0.1178   0.01304   0.00798  -0.1940   0.8014   0.0115
  -8.750  -0.0915   0.01272   0.00757  -0.1940   0.7868   0.0118
  -8.500  -0.0652   0.01241   0.00715  -0.1939   0.7728   0.0120
  -8.250  -0.0389   0.01214   0.00677  -0.1938   0.7589   0.0122
  -8.000  -0.0116   0.01184   0.00639  -0.1938   0.7456   0.0125
  -7.750   0.0156   0.01159   0.00605  -0.1938   0.7331   0.0127
  -7.500   0.0425   0.01138   0.00573  -0.1936   0.7197   0.0130
  -7.250   0.0705   0.01115   0.00542  -0.1937   0.7077   0.0132
  -7.000   0.0984   0.01089   0.00508  -0.1938   0.6962   0.0136
  -6.750   0.1262   0.01069   0.00480  -0.1938   0.6833   0.0140
  -6.500   0.1545   0.01051   0.00456  -0.1939   0.6718   0.0146
  -6.250   0.1823   0.01038   0.00435  -0.1938   0.6603   0.0151
  -6.000   0.2108   0.01023   0.00414  -0.1939   0.6484   0.0157
  -5.750   0.2391   0.01011   0.00394  -0.1939   0.6373   0.0163
  -5.500   0.2673   0.00999   0.00377  -0.1939   0.6254   0.0173
  -5.250   0.2959   0.00989   0.00361  -0.1940   0.6147   0.0184
  -5.000   0.3240   0.00982   0.00347  -0.1939   0.6031   0.0195
  -4.750   0.3529   0.00972   0.00333  -0.1940   0.5926   0.0210
  -4.500   0.3811   0.00967   0.00322  -0.1940   0.5818   0.0224
  -4.250   0.4098   0.00960   0.00310  -0.1940   0.5708   0.0242
  -4.000   0.4382   0.00956   0.00300  -0.1940   0.5612   0.0261
  -3.750   0.4669   0.00950   0.00291  -0.1941   0.5508   0.0284
  -3.500   0.4954   0.00947   0.00283  -0.1941   0.5411   0.0313
  -3.250   0.5240   0.00943   0.00275  -0.1941   0.5311   0.0351
  -3.000   0.5527   0.00939   0.00269  -0.1942   0.5223   0.0412
  -2.750   0.5816   0.00934   0.00263  -0.1943   0.5123   0.0524
  -2.500   0.6106   0.00927   0.00257  -0.1945   0.5038   0.0717
  -2.250   0.6401   0.00915   0.00252  -0.1949   0.4948   0.1016
  -2.000   0.6698   0.00902   0.00248  -0.1953   0.4861   0.1487
  -1.750   0.6991   0.00896   0.00248  -0.1956   0.4778   0.1820
  -1.500   0.7274   0.00897   0.00250  -0.1956   0.4695   0.2074
  -1.250   0.7563   0.00896   0.00252  -0.1957   0.4621   0.2310
  -1.000   0.7843   0.00901   0.00257  -0.1957   0.4536   0.2534
  -0.750   0.8126   0.00904   0.00262  -0.1956   0.4469   0.2725
  -0.500   0.8407   0.00909   0.00267  -0.1956   0.4394   0.2901
  -0.250   0.8682   0.00918   0.00275  -0.1954   0.4316   0.3091
   0.000   0.8961   0.00924   0.00280  -0.1953   0.4255   0.3189
   0.250   0.9236   0.00933   0.00287  -0.1951   0.4183   0.3289
   0.500   0.9507   0.00944   0.00294  -0.1948   0.4117   0.3362
   0.750   0.9783   0.00952   0.00301  -0.1946   0.4052   0.3456
   1.000   1.0052   0.00964   0.00311  -0.1943   0.3984   0.3546
   1.250   1.0323   0.00975   0.00319  -0.1941   0.3926   0.3622
   1.500   1.0594   0.00985   0.00329  -0.1938   0.3859   0.3727
   1.750   1.0857   0.00999   0.00340  -0.1934   0.3793   0.3813
   2.000   1.1127   0.01009   0.00350  -0.1932   0.3739   0.3916
   2.500   1.1651   0.01037   0.00375  -0.1924   0.3606   0.4131
   2.750   1.1916   0.01048   0.00386  -0.1921   0.3558   0.4234
   3.000   1.2178   0.01061   0.00400  -0.1917   0.3494   0.4368
   3.250   1.2429   0.01079   0.00416  -0.1911   0.3424   0.4483
   3.500   1.2688   0.01091   0.00429  -0.1907   0.3375   0.4615
   3.750   1.2938   0.01106   0.00445  -0.1901   0.3312   0.4762
   4.000   1.3177   0.01125   0.00462  -0.1893   0.3247   0.4898
   4.250   1.3424   0.01138   0.00478  -0.1886   0.3198   0.5042
   4.500   1.3664   0.01155   0.00496  -0.1879   0.3139   0.5216
   4.750   1.3897   0.01176   0.00517  -0.1870   0.3077   0.5384
   5.000   1.4139   0.01191   0.00536  -0.1863   0.3027   0.5548
   5.250   1.4372   0.01211   0.00557  -0.1854   0.2970   0.5735
   5.500   1.4598   0.01235   0.00581  -0.1845   0.2911   0.5950
   5.750   1.4835   0.01252   0.00603  -0.1837   0.2862   0.6164
   6.000   1.5064   0.01274   0.00628  -0.1828   0.2808   0.6378
   6.250   1.5283   0.01300   0.00656  -0.1818   0.2750   0.6643
   6.500   1.5517   0.01319   0.00681  -0.1810   0.2704   0.6942
   7.000   1.5947   0.01369   0.00742  -0.1788   0.2600   0.7627
   7.250   1.6163   0.01388   0.00772  -0.1777   0.2558   0.8184
   7.500   1.6294   0.01390   0.00796  -0.1748   0.2511   1.0000
   7.750   1.6495   0.01426   0.00829  -0.1735   0.2460   1.0000
   8.000   1.6695   0.01460   0.00863  -0.1722   0.2417   1.0000
   8.250   1.6898   0.01493   0.00895  -0.1710   0.2372   1.0000
   8.500   1.7089   0.01533   0.00934  -0.1696   0.2321   1.0000
   8.750   1.7272   0.01576   0.00975  -0.1681   0.2274   1.0000
   9.000   1.7466   0.01613   0.01013  -0.1668   0.2237   1.0000
   9.250   1.7649   0.01656   0.01057  -0.1654   0.2190   1.0000
   9.500   1.7814   0.01710   0.01108  -0.1637   0.2139   1.0000
   9.750   1.7991   0.01755   0.01155  -0.1623   0.2103   1.0000
  10.000   1.8166   0.01804   0.01205  -0.1608   0.2061   1.0000
  10.250   1.8317   0.01865   0.01266  -0.1590   0.2013   1.0000
  10.500   1.8470   0.01927   0.01328  -0.1573   0.1971   1.0000
  10.750   1.8629   0.01985   0.01388  -0.1557   0.1934   1.0000
  11.000   1.8775   0.02053   0.01457  -0.1540   0.1890   1.0000
  11.250   1.8899   0.02135   0.01538  -0.1521   0.1846   1.0000
  11.500   1.9047   0.02205   0.01611  -0.1506   0.1814   1.0000
  11.750   1.9180   0.02284   0.01693  -0.1489   0.1776   1.0000
  12.000   1.9296   0.02378   0.01787  -0.1471   0.1734   1.0000
  12.250   1.9403   0.02479   0.01890  -0.1452   0.1697   1.0000
  12.500   1.9531   0.02570   0.01985  -0.1437   0.1666   1.0000
  12.750   1.9639   0.02677   0.02094  -0.1420   0.1628   1.0000
  13.000   1.9720   0.02806   0.02225  -0.1402   0.1589   1.0000
  13.250   1.9817   0.02929   0.02351  -0.1386   0.1556   1.0000
  13.500   1.9916   0.03054   0.02480  -0.1371   0.1524   1.0000
  13.750   1.9993   0.03200   0.02630  -0.1356   0.1490   1.0000
  14.000   2.0049   0.03370   0.02802  -0.1339   0.1453   1.0000
  14.250   2.0130   0.03523   0.02960  -0.1326   0.1425   1.0000
  14.500   2.0199   0.03692   0.03133  -0.1313   0.1395   1.0000
  14.750   2.0245   0.03888   0.03333  -0.1300   0.1361   1.0000
  15.000   2.0268   0.04113   0.03561  -0.1287   0.1326   1.0000
  15.250   2.0328   0.04307   0.03761  -0.1277   0.1301   1.0000
  15.500   2.0364   0.04532   0.03991  -0.1268   0.1270   1.0000
  15.750   2.0371   0.04796   0.04259  -0.1258   0.1238   1.0000
  16.000   2.0366   0.05081   0.04550  -0.1250   0.1206   1.0000
  16.250   2.0398   0.05332   0.04807  -0.1244   0.1182   1.0000
  16.500   2.0401   0.05620   0.05102  -0.1239   0.1153   1.0000
  16.750   2.0367   0.05964   0.05450  -0.1235   0.1122   1.0000
  17.000   2.0335   0.06316   0.05809  -0.1232   0.1094   1.0000
  17.250   2.0322   0.06651   0.06151  -0.1231   0.1068   1.0000
  17.500   2.0279   0.07030   0.06537  -0.1231   0.1039   1.0000
  17.750   2.0202   0.07466   0.06978  -0.1233   0.1010   1.0000
  18.000   2.0159   0.07861   0.07381  -0.1236   0.0987   1.0000
  18.250   2.0119   0.08260   0.07788  -0.1240   0.0964   1.0000
  18.500   2.0042   0.08716   0.08251  -0.1247   0.0938   1.0000
  18.750   1.9936   0.09225   0.08767  -0.1256   0.0913   1.0000
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