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EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 64.01 at α=10.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ea61012-il-1000000.txt
Download as CSV file: xf-ea61012-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER EA 6(-1)-012 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.3506   0.08799   0.08488  -0.0174   1.0000   0.0188
 -19.500  -1.3765   0.07986   0.07659  -0.0221   1.0000   0.0188
 -19.250  -1.3947   0.07320   0.06978  -0.0257   1.0000   0.0190
 -19.000  -1.4140   0.06659   0.06303  -0.0293   1.0000   0.0192
 -18.750  -1.4321   0.06048   0.05680  -0.0324   1.0000   0.0196
 -18.500  -1.4431   0.05576   0.05198  -0.0345   1.0000   0.0199
 -18.250  -1.4486   0.05199   0.04813  -0.0359   1.0000   0.0203
 -18.000  -1.4508   0.04883   0.04490  -0.0368   1.0000   0.0208
 -17.750  -1.4506   0.04612   0.04211  -0.0374   1.0000   0.0213
 -17.500  -1.4500   0.04353   0.03943  -0.0378   1.0000   0.0217
 -17.250  -1.4449   0.04151   0.03731  -0.0379   1.0000   0.0222
 -17.000  -1.4396   0.03955   0.03525  -0.0380   1.0000   0.0226
 -16.750  -1.4421   0.03690   0.03252  -0.0379   1.0000   0.0232
 -16.500  -1.4364   0.03512   0.03072  -0.0377   1.0000   0.0239
 -16.250  -1.4283   0.03361   0.02916  -0.0373   1.0000   0.0245
 -16.000  -1.4166   0.03245   0.02796  -0.0369   1.0000   0.0252
 -15.750  -1.4060   0.03123   0.02667  -0.0364   1.0000   0.0257
 -15.500  -1.3941   0.03014   0.02551  -0.0359   1.0000   0.0263
 -15.250  -1.3811   0.02916   0.02445  -0.0353   1.0000   0.0266
 -15.000  -1.3775   0.02748   0.02271  -0.0342   1.0000   0.0274
 -14.750  -1.3662   0.02646   0.02166  -0.0334   1.0000   0.0281
 -14.500  -1.3526   0.02564   0.02082  -0.0326   1.0000   0.0287
 -14.250  -1.3378   0.02493   0.02008  -0.0318   1.0000   0.0293
 -14.000  -1.3224   0.02430   0.01941  -0.0310   1.0000   0.0300
 -13.750  -1.3082   0.02360   0.01865  -0.0300   1.0000   0.0305
 -13.500  -1.2913   0.02314   0.01812  -0.0291   1.0000   0.0311
 -13.250  -1.2774   0.02250   0.01741  -0.0278   1.0000   0.0314
 -13.000  -1.2714   0.02136   0.01623  -0.0255   1.0000   0.0322
 -12.750  -1.2581   0.02081   0.01567  -0.0238   1.0000   0.0328
 -12.500  -1.2430   0.02041   0.01525  -0.0222   1.0000   0.0334
 -12.250  -1.2267   0.02008   0.01490  -0.0205   1.0000   0.0340
 -12.000  -1.2090   0.01975   0.01454  -0.0191   1.0000   0.0347
 -11.750  -1.1890   0.01943   0.01418  -0.0181   1.0000   0.0354
 -11.500  -1.1689   0.01906   0.01376  -0.0171   1.0000   0.0359
 -11.250  -1.1478   0.01874   0.01339  -0.0162   1.0000   0.0364
 -11.000  -1.1280   0.01822   0.01282  -0.0152   1.0000   0.0369
 -10.750  -1.1113   0.01737   0.01195  -0.0138   1.0000   0.0379
 -10.500  -1.0892   0.01705   0.01164  -0.0131   1.0000   0.0387
 -10.250  -1.0666   0.01673   0.01132  -0.0124   1.0000   0.0394
 -10.000  -1.0437   0.01641   0.01099  -0.0118   1.0000   0.0401
  -9.750  -1.0204   0.01611   0.01067  -0.0112   1.0000   0.0409
  -9.500  -0.9908   0.01576   0.01029  -0.0119   0.9703   0.0417
  -9.250  -0.9468   0.01553   0.00989  -0.0155   0.9016   0.0424
  -9.000  -0.9247   0.01542   0.00962  -0.0144   0.8717   0.0428
  -8.750  -0.9070   0.01455   0.00865  -0.0130   0.8582   0.0438
  -8.500  -0.8852   0.01408   0.00813  -0.0121   0.8496   0.0447
  -8.250  -0.8614   0.01379   0.00781  -0.0115   0.8425   0.0456
  -8.000  -0.8372   0.01352   0.00750  -0.0109   0.8366   0.0463
  -7.750  -0.8126   0.01322   0.00717  -0.0104   0.8314   0.0471
  -7.500  -0.7879   0.01294   0.00684  -0.0098   0.8264   0.0479
  -7.250  -0.7630   0.01269   0.00654  -0.0093   0.8215   0.0487
  -7.000  -0.7372   0.01246   0.00630  -0.0090   0.8173   0.0494
  -6.750  -0.7111   0.01228   0.00608  -0.0087   0.8129   0.0499
  -6.500  -0.6880   0.01178   0.00552  -0.0079   0.8085   0.0510
  -6.250  -0.6637   0.01139   0.00511  -0.0073   0.8044   0.0524
  -6.000  -0.6380   0.01110   0.00482  -0.0070   0.8007   0.0536
  -5.750  -0.6118   0.01087   0.00457  -0.0066   0.7968   0.0547
  -5.500  -0.5855   0.01066   0.00434  -0.0063   0.7930   0.0559
  -5.250  -0.5590   0.01050   0.00414  -0.0060   0.7890   0.0571
  -5.000  -0.5320   0.01032   0.00395  -0.0058   0.7856   0.0580
  -4.750  -0.5053   0.01009   0.00371  -0.0056   0.7817   0.0591
  -4.500  -0.4793   0.00980   0.00341  -0.0052   0.7779   0.0616
  -4.250  -0.4527   0.00961   0.00321  -0.0049   0.7739   0.0638
  -4.000  -0.4255   0.00943   0.00303  -0.0047   0.7697   0.0659
  -3.750  -0.3980   0.00928   0.00287  -0.0045   0.7649   0.0679
  -3.500  -0.3713   0.00906   0.00267  -0.0043   0.7602   0.0732
  -3.250  -0.3442   0.00890   0.00251  -0.0040   0.7559   0.0791
  -3.000  -0.3179   0.00856   0.00232  -0.0037   0.7516   0.1041
  -2.750  -0.2937   0.00799   0.00208  -0.0032   0.7470   0.1800
  -2.500  -0.2693   0.00748   0.00186  -0.0027   0.7427   0.2560
  -2.250  -0.2452   0.00693   0.00168  -0.0022   0.7386   0.3535
  -2.000  -0.2192   0.00655   0.00154  -0.0019   0.7341   0.4136
  -1.750  -0.1954   0.00599   0.00138  -0.0012   0.7292   0.5190
  -1.500  -0.1686   0.00581   0.00134  -0.0009   0.7246   0.5744
  -1.250  -0.1406   0.00572   0.00132  -0.0008   0.7204   0.5988
  -1.000  -0.1124   0.00564   0.00130  -0.0007   0.7141   0.6178
  -0.500  -0.0564   0.00554   0.00125  -0.0003   0.6966   0.6520
  -0.250  -0.0283   0.00552   0.00122  -0.0001   0.6857   0.6632
   0.000   0.0000   0.00552   0.00121   0.0000   0.6750   0.6751
   0.250   0.0282   0.00552   0.00122   0.0002   0.6630   0.6858
   0.500   0.0563   0.00554   0.00125   0.0003   0.6520   0.6966
   0.750   0.0845   0.00561   0.00127   0.0005   0.6369   0.7066
   1.000   0.1123   0.00565   0.00130   0.0007   0.6177   0.7143
   1.250   0.1405   0.00572   0.00132   0.0008   0.5987   0.7204
   1.500   0.1685   0.00581   0.00134   0.0009   0.5743   0.7247
   1.750   0.1953   0.00599   0.00138   0.0013   0.5186   0.7292
   2.000   0.2192   0.00655   0.00154   0.0019   0.4135   0.7340
   2.250   0.2452   0.00693   0.00168   0.0022   0.3543   0.7386
   2.500   0.2693   0.00747   0.00186   0.0027   0.2570   0.7427
   2.750   0.2937   0.00799   0.00208   0.0032   0.1807   0.7470
   3.000   0.3179   0.00856   0.00232   0.0037   0.1041   0.7517
   3.250   0.3442   0.00890   0.00251   0.0040   0.0790   0.7559
   3.500   0.3712   0.00906   0.00267   0.0043   0.0731   0.7602
   3.750   0.3980   0.00928   0.00287   0.0046   0.0679   0.7649
   4.000   0.4254   0.00943   0.00303   0.0047   0.0659   0.7698
   4.250   0.4526   0.00961   0.00321   0.0049   0.0638   0.7739
   4.500   0.4792   0.00980   0.00341   0.0052   0.0616   0.7779
   4.750   0.5053   0.01009   0.00371   0.0056   0.0591   0.7817
   5.000   0.5319   0.01032   0.00395   0.0059   0.0580   0.7856
   5.250   0.5589   0.01050   0.00414   0.0061   0.0571   0.7890
   5.500   0.5855   0.01066   0.00434   0.0063   0.0558   0.7930
   5.750   0.6118   0.01087   0.00457   0.0067   0.0547   0.7968
   6.000   0.6379   0.01110   0.00482   0.0070   0.0536   0.8007
   6.250   0.6637   0.01139   0.00510   0.0073   0.0524   0.8044
   6.500   0.6880   0.01178   0.00551   0.0079   0.0511   0.8085
   6.750   0.7110   0.01228   0.00608   0.0087   0.0499   0.8129
   7.000   0.7371   0.01246   0.00629   0.0090   0.0494   0.8173
   7.250   0.7629   0.01270   0.00655   0.0094   0.0487   0.8215
   7.500   0.7878   0.01294   0.00685   0.0099   0.0479   0.8264
   7.750   0.8125   0.01322   0.00717   0.0104   0.0472   0.8314
   8.000   0.8372   0.01351   0.00749   0.0109   0.0463   0.8366
   8.250   0.8613   0.01380   0.00781   0.0115   0.0456   0.8425
   8.500   0.8851   0.01408   0.00813   0.0121   0.0447   0.8496
   8.750   0.9068   0.01456   0.00865   0.0130   0.0438   0.8583
   9.000   0.9245   0.01542   0.00962   0.0145   0.0428   0.8719
   9.250   0.9468   0.01551   0.00987   0.0155   0.0424   0.9022
   9.500   0.9912   0.01576   0.01029   0.0118   0.0417   0.9713
   9.750   1.0203   0.01612   0.01068   0.0112   0.0409   1.0000
  10.000   1.0438   0.01641   0.01098   0.0118   0.0401   1.0000
  10.250   1.0667   0.01671   0.01130   0.0124   0.0394   1.0000
  10.500   1.0895   0.01702   0.01161   0.0131   0.0387   1.0000
  10.750   1.1113   0.01738   0.01197   0.0139   0.0379   1.0000
  11.000   1.1278   0.01826   0.01286   0.0152   0.0369   1.0000
  11.250   1.1473   0.01881   0.01346   0.0163   0.0364   1.0000
  11.500   1.1691   0.01905   0.01375   0.0171   0.0359   1.0000
  11.750   1.1893   0.01941   0.01416   0.0181   0.0353   1.0000
  12.000   1.2094   0.01973   0.01452   0.0191   0.0347   1.0000
  12.250   1.2279   0.02001   0.01482   0.0204   0.0339   1.0000
  12.500   1.2435   0.02039   0.01523   0.0221   0.0334   1.0000
  12.750   1.2587   0.02079   0.01565   0.0237   0.0328   1.0000
  13.000   1.2717   0.02137   0.01624   0.0255   0.0322   1.0000
  13.250   1.2777   0.02250   0.01741   0.0277   0.0314   1.0000
  13.500   1.2920   0.02312   0.01810   0.0290   0.0310   1.0000
  13.750   1.3080   0.02365   0.01869   0.0300   0.0305   1.0000
  14.000   1.3222   0.02435   0.01945   0.0310   0.0300   1.0000
  14.250   1.3383   0.02493   0.02007   0.0318   0.0293   1.0000
  14.500   1.3514   0.02576   0.02096   0.0327   0.0288   1.0000
  14.750   1.3670   0.02642   0.02163   0.0333   0.0281   1.0000
  15.000   1.3780   0.02748   0.02271   0.0342   0.0274   1.0000
  15.250   1.3812   0.02920   0.02448   0.0352   0.0267   1.0000
  15.500   1.3949   0.03013   0.02549   0.0358   0.0263   1.0000
  15.750   1.4065   0.03125   0.02669   0.0363   0.0258   1.0000
  16.000   1.4175   0.03243   0.02794   0.0368   0.0252   1.0000
  16.250   1.4284   0.03366   0.02922   0.0372   0.0245   1.0000
  16.500   1.4371   0.03513   0.03073   0.0375   0.0239   1.0000
  16.750   1.4422   0.03697   0.03261   0.0378   0.0233   1.0000
  17.000   1.4420   0.03940   0.03510   0.0378   0.0225   1.0000
  17.250   1.4475   0.04134   0.03713   0.0378   0.0222   1.0000
  17.500   1.4507   0.04357   0.03946   0.0376   0.0218   1.0000
  17.750   1.4530   0.04598   0.04196   0.0372   0.0213   1.0000
  18.000   1.4530   0.04873   0.04479   0.0366   0.0207   1.0000
  18.250   1.4504   0.05193   0.04806   0.0357   0.0203   1.0000
  18.500   1.4445   0.05577   0.05199   0.0342   0.0199   1.0000
  18.750   1.4319   0.06074   0.05705   0.0320   0.0194   1.0000
  19.000   1.4159   0.06653   0.06297   0.0291   0.0192   1.0000
  19.250   1.3969   0.07312   0.06970   0.0255   0.0190   1.0000
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