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EPPLER 560 AIRFOIL (e560-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 560 AIRFOIL (e560-il)
Reynolds number: 200,000
Max Cl/Cd: 75.26 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e560-il-200000-n5.txt
Download as CSV file: xf-e560-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 560 AIRFOIL                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.5489   0.12058   0.11615  -0.0507   1.0000   0.0210
 -15.500  -0.5729   0.11193   0.10737  -0.0548   1.0000   0.0210
 -15.250  -0.5888   0.10524   0.10056  -0.0579   1.0000   0.0210
 -15.000  -0.6038   0.09894   0.09413  -0.0608   1.0000   0.0211
 -14.750  -0.6095   0.09474   0.08989  -0.0624   1.0000   0.0213
 -14.500  -0.6122   0.09124   0.08638  -0.0636   1.0000   0.0216
 -14.250  -0.6162   0.08755   0.08267  -0.0649   1.0000   0.0219
 -14.000  -0.6207   0.08386   0.07895  -0.0662   1.0000   0.0221
 -13.750  -0.6260   0.08014   0.07520  -0.0674   1.0000   0.0223
 -13.500  -0.6311   0.07662   0.07163  -0.0685   1.0000   0.0225
 -13.250  -0.6365   0.07322   0.06819  -0.0694   1.0000   0.0226
 -13.000  -0.6430   0.06985   0.06479  -0.0702   1.0000   0.0229
 -12.750  -0.6501   0.06665   0.06155  -0.0707   1.0000   0.0230
 -12.500  -0.6595   0.06345   0.05832  -0.0712   1.0000   0.0232
 -12.250  -0.6701   0.06037   0.05520  -0.0713   1.0000   0.0234
 -12.000  -0.6824   0.05738   0.05218  -0.0711   1.0000   0.0235
 -11.750  -0.6981   0.05438   0.04917  -0.0705   1.0000   0.0236
 -11.500  -0.7038   0.05099   0.04573  -0.0725   0.9981   0.0238
 -11.250  -0.6943   0.04699   0.04162  -0.0784   0.9926   0.0243
 -11.000  -0.6874   0.04305   0.03757  -0.0839   0.9850   0.0246
 -10.750  -0.6784   0.03881   0.03321  -0.0900   0.9758   0.0249
 -10.500  -0.6620   0.03411   0.02835  -0.0981   0.9664   0.0255
 -10.250  -0.6338   0.02980   0.02385  -0.1076   0.9596   0.0262
 -10.000  -0.6118   0.02754   0.02145  -0.1109   0.9505   0.0272
  -9.750  -0.5835   0.02575   0.01951  -0.1141   0.9442   0.0287
  -9.500  -0.5551   0.02423   0.01786  -0.1166   0.9372   0.0306
  -9.250  -0.5206   0.02273   0.01628  -0.1200   0.9334   0.0336
  -9.000  -0.4955   0.02152   0.01499  -0.1211   0.9242   0.0373
  -8.500  -0.4327   0.01923   0.01260  -0.1250   0.9115   0.0536
  -8.250  -0.3981   0.01828   0.01162  -0.1271   0.9059   0.0662
  -8.000  -0.3647   0.01748   0.01080  -0.1289   0.8990   0.0789
  -7.750  -0.3301   0.01677   0.01008  -0.1308   0.8918   0.0923
  -7.500  -0.2908   0.01612   0.00940  -0.1335   0.8864   0.1066
  -7.250  -0.2561   0.01560   0.00885  -0.1352   0.8773   0.1203
  -7.000  -0.2123   0.01508   0.00830  -0.1386   0.8712   0.1368
  -6.750  -0.1746   0.01470   0.00789  -0.1408   0.8608   0.1521
  -6.500  -0.1316   0.01436   0.00748  -0.1440   0.8516   0.1673
  -6.250  -0.0910   0.01407   0.00712  -0.1466   0.8403   0.1799
  -6.000  -0.0535   0.01385   0.00678  -0.1486   0.8274   0.1903
  -5.750  -0.0171   0.01366   0.00649  -0.1503   0.8143   0.2006
  -5.500   0.0175   0.01351   0.00624  -0.1516   0.8006   0.2098
  -5.250   0.0506   0.01341   0.00597  -0.1525   0.7870   0.2193
  -5.000   0.0811   0.01331   0.00581  -0.1530   0.7728   0.2272
  -4.750   0.1107   0.01324   0.00560  -0.1532   0.7589   0.2356
  -4.500   0.1397   0.01317   0.00548  -0.1534   0.7456   0.2430
  -4.250   0.1687   0.01314   0.00529  -0.1535   0.7328   0.2510
  -3.750   0.2249   0.01308   0.00506  -0.1534   0.7077   0.2658
  -3.500   0.2525   0.01305   0.00498  -0.1532   0.6956   0.2726
  -3.250   0.2803   0.01306   0.00488  -0.1531   0.6841   0.2801
  -3.000   0.3078   0.01305   0.00479  -0.1529   0.6725   0.2870
  -2.750   0.3350   0.01306   0.00474  -0.1526   0.6613   0.2942
  -2.500   0.3625   0.01309   0.00465  -0.1524   0.6506   0.3015
  -2.250   0.3895   0.01309   0.00464  -0.1522   0.6398   0.3081
  -2.000   0.4168   0.01313   0.00459  -0.1519   0.6297   0.3158
  -1.750   0.4438   0.01316   0.00456  -0.1517   0.6197   0.3221
  -1.500   0.4708   0.01319   0.00456  -0.1514   0.6095   0.3296
  -1.250   0.4979   0.01325   0.00454  -0.1511   0.6003   0.3368
  -1.000   0.5248   0.01329   0.00456  -0.1508   0.5907   0.3437
  -0.750   0.5518   0.01336   0.00455  -0.1506   0.5817   0.3515
  -0.500   0.5785   0.01341   0.00460  -0.1503   0.5726   0.3584
  -0.250   0.6054   0.01349   0.00462  -0.1500   0.5642   0.3663
   0.000   0.6321   0.01355   0.00467  -0.1497   0.5558   0.3735
   0.250   0.6588   0.01364   0.00473  -0.1494   0.5478   0.3817
   0.500   0.6854   0.01372   0.00479  -0.1490   0.5394   0.3895
   0.750   0.7120   0.01381   0.00487  -0.1487   0.5319   0.3974
   1.000   0.7386   0.01390   0.00495  -0.1484   0.5242   0.4060
   1.250   0.7650   0.01402   0.00505  -0.1481   0.5172   0.4146
   1.500   0.7914   0.01411   0.00515  -0.1477   0.5095   0.4235
   1.750   0.8175   0.01423   0.00526  -0.1473   0.5027   0.4328
   2.000   0.8440   0.01433   0.00540  -0.1470   0.4960   0.4426
   2.250   0.8701   0.01446   0.00553  -0.1466   0.4893   0.4530
   2.500   0.8961   0.01459   0.00568  -0.1463   0.4830   0.4635
   2.750   0.9221   0.01471   0.00585  -0.1459   0.4762   0.4754
   3.000   0.9479   0.01486   0.00601  -0.1454   0.4704   0.4883
   3.250   0.9738   0.01500   0.00620  -0.1451   0.4646   0.5017
   3.500   0.9992   0.01513   0.00640  -0.1446   0.4583   0.5169
   3.750   1.0244   0.01530   0.00659  -0.1440   0.4528   0.5340
   4.000   1.0499   0.01544   0.00683  -0.1436   0.4471   0.5531
   4.250   1.0750   0.01559   0.00706  -0.1430   0.4414   0.5754
   4.500   1.0996   0.01576   0.00730  -0.1424   0.4363   0.6009
   4.750   1.1242   0.01590   0.00757  -0.1418   0.4308   0.6316
   5.000   1.1480   0.01603   0.00784  -0.1410   0.4253   0.6690
   5.250   1.1708   0.01618   0.00810  -0.1400   0.4205   0.7165
   5.500   1.1914   0.01626   0.00837  -0.1384   0.4155   0.7811
   5.750   1.2042   0.01610   0.00847  -0.1350   0.4106   0.9837
   6.000   1.2292   0.01639   0.00874  -0.1345   0.4056   1.0000
   6.250   1.2534   0.01670   0.00902  -0.1340   0.4008   1.0000
   6.500   1.2772   0.01697   0.00934  -0.1333   0.3952   1.0000
   6.750   1.3003   0.01728   0.00964  -0.1325   0.3901   1.0000
   7.000   1.3232   0.01762   0.00995  -0.1317   0.3855   1.0000
   7.250   1.3455   0.01791   0.01031  -0.1308   0.3799   1.0000
   7.500   1.3665   0.01823   0.01066  -0.1296   0.3746   1.0000
   7.750   1.3872   0.01860   0.01099  -0.1284   0.3699   1.0000
   8.000   1.4073   0.01891   0.01140  -0.1271   0.3642   1.0000
   8.250   1.4265   0.01927   0.01179  -0.1257   0.3586   1.0000
   8.500   1.4453   0.01968   0.01218  -0.1243   0.3535   1.0000
   8.750   1.4639   0.02004   0.01265  -0.1228   0.3474   1.0000
   9.000   1.4810   0.02046   0.01309  -0.1211   0.3415   1.0000
   9.250   1.4980   0.02091   0.01357  -0.1194   0.3358   1.0000
   9.500   1.5144   0.02135   0.01410  -0.1176   0.3292   1.0000
   9.750   1.5291   0.02188   0.01463  -0.1157   0.3232   1.0000
  10.000   1.5446   0.02239   0.01523  -0.1139   0.3166   1.0000
  10.250   1.5583   0.02296   0.01585  -0.1119   0.3100   1.0000
  10.500   1.5714   0.02359   0.01654  -0.1099   0.3035   1.0000
  10.750   1.5838   0.02426   0.01728  -0.1079   0.2962   1.0000
  11.000   1.5942   0.02504   0.01809  -0.1057   0.2892   1.0000
  11.250   1.6048   0.02585   0.01898  -0.1036   0.2810   1.0000
  11.500   1.6129   0.02681   0.01997  -0.1013   0.2732   1.0000
  11.750   1.6211   0.02783   0.02106  -0.0992   0.2644   1.0000
  12.000   1.6278   0.02899   0.02228  -0.0971   0.2561   1.0000
  12.250   1.6326   0.03033   0.02366  -0.0949   0.2470   1.0000
  12.500   1.6378   0.03174   0.02513  -0.0930   0.2378   1.0000
  12.750   1.6393   0.03347   0.02688  -0.0910   0.2288   1.0000
  13.000   1.6414   0.03527   0.02874  -0.0892   0.2187   1.0000
  13.250   1.6418   0.03731   0.03083  -0.0876   0.2091   1.0000
  13.500   1.6386   0.03976   0.03329  -0.0860   0.1994   1.0000
  13.750   1.6364   0.04229   0.03588  -0.0847   0.1893   1.0000
  14.000   1.6324   0.04513   0.03875  -0.0836   0.1794   1.0000
  14.250   1.6252   0.04843   0.04208  -0.0826   0.1699   1.0000
  14.500   1.6185   0.05185   0.04554  -0.0820   0.1603   1.0000
  14.750   1.6116   0.05546   0.04919  -0.0816   0.1513   1.0000
  15.000   1.6012   0.05963   0.05338  -0.0815   0.1428   1.0000
  15.250   1.5931   0.06369   0.05750  -0.0816   0.1342   1.0000
  15.500   1.5836   0.06810   0.06195  -0.0819   0.1264   1.0000
  15.750   1.5725   0.07284   0.06673  -0.0825   0.1187   1.0000
  16.000   1.5639   0.07738   0.07134  -0.0833   0.1115   1.0000
  16.250   1.5514   0.08263   0.07662  -0.0843   0.1049   1.0000
  16.500   1.5437   0.08728   0.08134  -0.0854   0.0979   1.0000
  16.750   1.5318   0.09265   0.08676  -0.0868   0.0921   1.0000
  17.000   1.5252   0.09732   0.09150  -0.0881   0.0860   1.0000
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