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TRAINER60 (trainer60-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: TRAINER60 (trainer60-il)
Reynolds number: 500,000
Max Cl/Cd: 65.81 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-trainer60-il-500000-n5.txt
Download as CSV file: xf-trainer60-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TRAINER60                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.3008   0.10035   0.09532   0.0228   1.0000   0.0276
 -17.500  -1.3121   0.09496   0.08984   0.0207   1.0000   0.0278
 -17.250  -1.3241   0.08954   0.08434   0.0186   1.0000   0.0281
 -17.000  -1.3341   0.08443   0.07913   0.0167   1.0000   0.0284
 -16.750  -1.3440   0.07942   0.07403   0.0149   1.0000   0.0287
 -16.500  -1.3526   0.07468   0.06920   0.0133   1.0000   0.0290
 -16.250  -1.3596   0.07022   0.06465   0.0118   1.0000   0.0294
 -16.000  -1.3662   0.06592   0.06025   0.0105   1.0000   0.0298
 -15.750  -1.3721   0.06186   0.05609   0.0093   1.0000   0.0302
 -15.500  -1.3765   0.05806   0.05219   0.0083   1.0000   0.0306
 -15.250  -1.3797   0.05448   0.04851   0.0074   1.0000   0.0310
 -15.000  -1.3827   0.05096   0.04491   0.0066   1.0000   0.0315
 -14.750  -1.3859   0.04742   0.04130   0.0057   1.0000   0.0320
 -14.500  -1.3865   0.04423   0.03803   0.0050   1.0000   0.0325
 -14.250  -1.3846   0.04129   0.03502   0.0044   1.0000   0.0332
 -14.000  -1.3810   0.03858   0.03223   0.0038   1.0000   0.0340
 -13.750  -1.3750   0.03616   0.02974   0.0033   1.0000   0.0348
 -13.250  -1.3613   0.03172   0.02517   0.0028   1.0000   0.0366
 -13.000  -1.3464   0.02971   0.02311   0.0015   0.9992   0.0381
 -12.750  -1.3271   0.02803   0.02136   0.0000   0.9968   0.0398
 -12.500  -1.3255   0.02643   0.01972   0.0025   0.9647   0.0409
 -12.250  -1.3000   0.02487   0.01811  -0.0001   0.9566   0.0431
 -12.000  -1.2704   0.02360   0.01678  -0.0027   0.9508   0.0458
 -11.750  -1.2392   0.02237   0.01550  -0.0056   0.9456   0.0493
 -11.500  -1.2060   0.02127   0.01437  -0.0085   0.9408   0.0539
 -11.250  -1.1721   0.02025   0.01334  -0.0113   0.9365   0.0598
 -11.000  -1.1418   0.01930   0.01239  -0.0132   0.9321   0.0676
 -10.750  -1.1185   0.01834   0.01149  -0.0137   0.9264   0.0797
 -10.500  -1.0931   0.01751   0.01071  -0.0144   0.9209   0.0943
 -10.250  -1.0726   0.01677   0.01006  -0.0138   0.9143   0.1105
 -10.000  -1.0479   0.01624   0.00958  -0.0138   0.9086   0.1236
  -9.750  -1.0272   0.01582   0.00918  -0.0128   0.9011   0.1334
  -9.500  -1.0055   0.01544   0.00882  -0.0118   0.8934   0.1419
  -9.250  -0.9834   0.01514   0.00851  -0.0107   0.8843   0.1487
  -9.000  -0.9626   0.01480   0.00818  -0.0094   0.8735   0.1546
  -8.750  -0.9408   0.01450   0.00787  -0.0082   0.8606   0.1604
  -8.500  -0.9183   0.01427   0.00759  -0.0070   0.8419   0.1649
  -8.250  -0.8978   0.01397   0.00723  -0.0055   0.8137   0.1698
  -8.000  -0.8745   0.01375   0.00690  -0.0045   0.7831   0.1753
  -7.750  -0.8486   0.01360   0.00662  -0.0040   0.7577   0.1795
  -7.500  -0.8236   0.01334   0.00631  -0.0035   0.7382   0.1861
  -7.250  -0.7976   0.01314   0.00606  -0.0031   0.7219   0.1937
  -7.000  -0.7723   0.01288   0.00578  -0.0026   0.7084   0.2023
  -6.750  -0.7463   0.01267   0.00554  -0.0022   0.6969   0.2105
  -6.500  -0.7202   0.01246   0.00531  -0.0018   0.6861   0.2162
  -6.000  -0.6677   0.01208   0.00487  -0.0010   0.6674   0.2290
  -5.750  -0.6417   0.01187   0.00466  -0.0005   0.6591   0.2365
  -5.500  -0.6153   0.01170   0.00446  -0.0001   0.6514   0.2452
  -5.250  -0.5892   0.01148   0.00428   0.0004   0.6443   0.2556
  -5.000  -0.5629   0.01129   0.00410   0.0008   0.6362   0.2687
  -4.500  -0.5103   0.01092   0.00380   0.0017   0.6206   0.2980
  -4.250  -0.4835   0.01077   0.00367   0.0021   0.6127   0.3112
  -4.000  -0.4562   0.01068   0.00355   0.0024   0.6052   0.3237
  -3.750  -0.4290   0.01054   0.00345   0.0027   0.5982   0.3360
  -3.500  -0.4013   0.01044   0.00336   0.0030   0.5899   0.3469
  -3.250  -0.3741   0.01036   0.00326   0.0033   0.5813   0.3575
  -3.000  -0.3458   0.01029   0.00319   0.0035   0.5722   0.3657
  -2.750  -0.3184   0.01021   0.00310   0.0038   0.5624   0.3742
  -2.500  -0.2902   0.01016   0.00303   0.0039   0.5538   0.3821
  -2.250  -0.2621   0.01010   0.00297   0.0041   0.5443   0.3890
  -2.000  -0.2344   0.01006   0.00290   0.0044   0.5352   0.3972
  -1.750  -0.2059   0.01002   0.00286   0.0045   0.5263   0.4055
  -1.500  -0.1781   0.00997   0.00281   0.0047   0.5166   0.4135
  -1.250  -0.1499   0.00995   0.00278   0.0049   0.5071   0.4215
  -1.000  -0.1218   0.00996   0.00274   0.0051   0.4947   0.4285
  -0.750  -0.0938   0.00993   0.00272   0.0052   0.4833   0.4369
  -0.500  -0.0658   0.00996   0.00270   0.0054   0.4710   0.4460
  -0.250  -0.0374   0.00994   0.00270   0.0055   0.4618   0.4550
   0.000  -0.0092   0.00996   0.00271   0.0057   0.4510   0.4650
   0.250   0.0191   0.00997   0.00273   0.0058   0.4416   0.4761
   0.500   0.0476   0.00998   0.00276   0.0059   0.4329   0.4895
   0.750   0.0758   0.01001   0.00280   0.0060   0.4256   0.5011
   1.000   0.1048   0.01003   0.00284   0.0060   0.4192   0.5132
   1.250   0.1335   0.01005   0.00290   0.0061   0.4114   0.5236
   1.500   0.1619   0.01013   0.00295   0.0062   0.4038   0.5324
   1.750   0.1913   0.01016   0.00300   0.0061   0.3977   0.5393
   2.000   0.2204   0.01020   0.00306   0.0060   0.3906   0.5463
   2.250   0.2490   0.01029   0.00312   0.0061   0.3832   0.5529
   2.500   0.2784   0.01035   0.00318   0.0060   0.3759   0.5586
   2.750   0.3076   0.01040   0.00325   0.0059   0.3670   0.5650
   3.000   0.3367   0.01048   0.00334   0.0058   0.3592   0.5718
   3.250   0.3660   0.01056   0.00342   0.0056   0.3505   0.5780
   3.500   0.3947   0.01069   0.00350   0.0056   0.3409   0.5830
   3.750   0.4245   0.01075   0.00360   0.0054   0.3295   0.5888
   4.000   0.4536   0.01088   0.00371   0.0052   0.3168   0.5948
   4.250   0.4823   0.01104   0.00384   0.0051   0.3013   0.6010
   4.750   0.5401   0.01142   0.00414   0.0048   0.2675   0.6140
   5.000   0.5690   0.01163   0.00432   0.0045   0.2527   0.6210
   5.250   0.5978   0.01186   0.00452   0.0043   0.2405   0.6275
   5.750   0.6574   0.01229   0.00497   0.0035   0.2211   0.6435
   6.250   0.7182   0.01275   0.00546   0.0022   0.2034   0.6650
   6.750   0.7811   0.01321   0.00601   0.0005   0.1888   0.6932
   7.000   0.8144   0.01346   0.00630  -0.0008   0.1815   0.7124
   7.250   0.8480   0.01368   0.00660  -0.0021   0.1762   0.7328
   7.500   0.8810   0.01389   0.00689  -0.0033   0.1698   0.7553
   7.750   0.9120   0.01419   0.00725  -0.0042   0.1631   0.7798
   8.000   0.9413   0.01439   0.00757  -0.0045   0.1574   0.8069
   8.250   0.9646   0.01468   0.00793  -0.0036   0.1521   0.8316
   8.500   0.9854   0.01499   0.00828  -0.0021   0.1474   0.8502
   8.750   1.0062   0.01529   0.00861  -0.0007   0.1416   0.8644
   9.000   1.0263   0.01567   0.00898   0.0007   0.1352   0.8759
   9.250   1.0463   0.01604   0.00934   0.0022   0.1279   0.8859
   9.500   1.0660   0.01646   0.00974   0.0036   0.1196   0.8942
   9.750   1.0858   0.01698   0.01020   0.0048   0.1082   0.9006
  10.000   1.1040   0.01766   0.01079   0.0061   0.0925   0.9068
  10.250   1.1204   0.01853   0.01155   0.0074   0.0756   0.9126
  10.500   1.1382   0.01941   0.01237   0.0083   0.0638   0.9182
  10.750   1.1578   0.02025   0.01319   0.0089   0.0568   0.9230
  11.000   1.1827   0.02114   0.01407   0.0081   0.0515   0.9271
  11.250   1.2017   0.02198   0.01493   0.0086   0.0484   0.9314
  11.500   1.2268   0.02294   0.01593   0.0075   0.0458   0.9344
  11.750   1.2469   0.02401   0.01705   0.0069   0.0438   0.9380
  12.000   1.2679   0.02519   0.01829   0.0059   0.0422   0.9413
  12.250   1.2901   0.02660   0.01976   0.0042   0.0406   0.9447
  12.500   1.3089   0.02824   0.02146   0.0026   0.0393   0.9497
  12.750   1.3331   0.02984   0.02316   0.0000   0.0381   0.9547
  13.000   1.3543   0.03177   0.02518  -0.0026   0.0370   0.9607
  13.500   1.3577   0.03632   0.02983  -0.0005   0.0356   0.9968
  13.750   1.3658   0.03900   0.03257  -0.0019   0.0351   0.9979
  14.000   1.3749   0.04164   0.03529  -0.0034   0.0345   0.9988
  14.250   1.3841   0.04440   0.03815  -0.0051   0.0339   0.9996
  14.500   1.3894   0.04745   0.04128  -0.0066   0.0334   1.0000
  14.750   1.3892   0.05065   0.04457  -0.0074   0.0330   1.0000
  15.000   1.3868   0.05416   0.04816  -0.0082   0.0326   1.0000
  15.250   1.3824   0.05794   0.05204  -0.0092   0.0322   1.0000
  15.500   1.3772   0.06190   0.05608  -0.0104   0.0319   1.0000
  15.750   1.3701   0.06619   0.06046  -0.0117   0.0316   1.0000
  16.000   1.3616   0.07079   0.06516  -0.0131   0.0313   1.0000
  16.250   1.3531   0.07551   0.06996  -0.0148   0.0310   1.0000
  16.500   1.3426   0.08056   0.07510  -0.0165   0.0308   1.0000
  16.750   1.3340   0.08543   0.08006  -0.0183   0.0305   1.0000
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