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TRAINER60 (trainer60-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: TRAINER60 (trainer60-il)
Reynolds number: 500,000
Max Cl/Cd: 73.13 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-trainer60-il-500000.txt
Download as CSV file: xf-trainer60-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.3016   0.09205   0.08697   0.0186   1.0000   0.0363
 -17.000  -1.3081   0.08759   0.08247   0.0170   1.0000   0.0367
 -16.750  -1.3139   0.08322   0.07804   0.0155   1.0000   0.0372
 -16.500  -1.3191   0.07895   0.07370   0.0141   1.0000   0.0377
 -16.250  -1.3247   0.07467   0.06935   0.0127   1.0000   0.0382
 -16.000  -1.3295   0.07054   0.06513   0.0114   1.0000   0.0388
 -15.750  -1.3336   0.06660   0.06109   0.0102   1.0000   0.0393
 -15.500  -1.3369   0.06284   0.05724   0.0091   1.0000   0.0399
 -15.250  -1.3433   0.05882   0.05313   0.0081   1.0000   0.0405
 -15.000  -1.3543   0.05434   0.04858   0.0070   1.0000   0.0411
 -14.750  -1.3613   0.05037   0.04454   0.0061   1.0000   0.0418
 -14.500  -1.3649   0.04680   0.04090   0.0053   1.0000   0.0425
 -14.250  -1.3652   0.04362   0.03764   0.0046   1.0000   0.0434
 -14.000  -1.3630   0.04071   0.03464   0.0040   1.0000   0.0445
 -13.750  -1.3603   0.03789   0.03173   0.0034   1.0000   0.0455
 -13.500  -1.3620   0.03465   0.02843   0.0028   1.0000   0.0467
 -13.250  -1.3583   0.03211   0.02584   0.0026   1.0000   0.0481
 -13.000  -1.3509   0.03006   0.02372   0.0026   1.0000   0.0500
 -12.750  -1.3463   0.02792   0.02152   0.0029   1.0000   0.0519
 -12.500  -1.3408   0.02606   0.01962   0.0037   1.0000   0.0542
 -12.250  -1.3322   0.02463   0.01814   0.0048   1.0000   0.0571
 -12.000  -1.3276   0.02321   0.01671   0.0069   1.0000   0.0605
 -11.750  -1.3205   0.02207   0.01555   0.0093   1.0000   0.0652
 -11.500  -1.3080   0.02088   0.01440   0.0109   1.0000   0.0726
 -11.250  -1.2944   0.01967   0.01327   0.0123   1.0000   0.0849
 -11.000  -1.2798   0.01852   0.01226   0.0137   1.0000   0.1041
 -10.750  -1.2613   0.01763   0.01152   0.0146   1.0000   0.1241
 -10.500  -1.2381   0.01709   0.01102   0.0150   1.0000   0.1377
 -10.250  -1.2142   0.01659   0.01058   0.0154   1.0000   0.1486
 -10.000  -1.1948   0.01597   0.01000   0.0168   0.9856   0.1559
  -9.750  -1.1473   0.01567   0.00965   0.0125   0.9694   0.1647
  -9.500  -1.0965   0.01511   0.00912   0.0072   0.9638   0.1736
  -9.250  -1.0410   0.01479   0.00872   0.0011   0.9568   0.1806
  -9.000  -0.9874   0.01427   0.00823  -0.0050   0.9490   0.1888
  -8.750  -0.9380   0.01404   0.00792  -0.0098   0.9399   0.1950
  -8.500  -0.9008   0.01372   0.00758  -0.0121   0.9295   0.2013
  -8.250  -0.8722   0.01351   0.00735  -0.0124   0.9182   0.2068
  -8.000  -0.8463   0.01338   0.00716  -0.0119   0.9072   0.2118
  -7.750  -0.8247   0.01312   0.00690  -0.0106   0.8956   0.2172
  -7.500  -0.8044   0.01284   0.00663  -0.0090   0.8827   0.2240
  -7.000  -0.7639   0.01224   0.00606  -0.0056   0.8492   0.2411
  -6.750  -0.7421   0.01199   0.00578  -0.0041   0.8267   0.2501
  -6.500  -0.7207   0.01169   0.00546  -0.0026   0.8021   0.2601
  -6.250  -0.6964   0.01147   0.00517  -0.0017   0.7794   0.2707
  -6.000  -0.6711   0.01126   0.00493  -0.0011   0.7615   0.2846
  -5.500  -0.6196   0.01085   0.00454   0.0000   0.7334   0.3181
  -5.250  -0.5930   0.01072   0.00439   0.0004   0.7216   0.3338
  -5.000  -0.5660   0.01060   0.00427   0.0007   0.7107   0.3482
  -4.750  -0.5388   0.01053   0.00415   0.0011   0.7000   0.3613
  -4.500  -0.5118   0.01040   0.00404   0.0014   0.6905   0.3723
  -4.250  -0.4841   0.01035   0.00394   0.0017   0.6811   0.3825
  -4.000  -0.4567   0.01027   0.00385   0.0020   0.6726   0.3917
  -3.750  -0.4291   0.01018   0.00377   0.0023   0.6638   0.4012
  -3.500  -0.4013   0.01014   0.00367   0.0026   0.6550   0.4100
  -3.250  -0.3738   0.01005   0.00361   0.0029   0.6466   0.4191
  -3.000  -0.3456   0.01002   0.00353   0.0031   0.6371   0.4270
  -2.750  -0.3182   0.00997   0.00346   0.0034   0.6279   0.4355
  -2.500  -0.2901   0.00989   0.00341   0.0036   0.6195   0.4439
  -2.250  -0.2620   0.00985   0.00334   0.0038   0.6103   0.4516
  -2.000  -0.2342   0.00981   0.00330   0.0041   0.6016   0.4605
  -1.750  -0.2058   0.00977   0.00326   0.0042   0.5920   0.4694
  -1.500  -0.1782   0.00974   0.00322   0.0045   0.5823   0.4782
  -1.250  -0.1498   0.00970   0.00320   0.0047   0.5723   0.4873
  -1.000  -0.1218   0.00970   0.00315   0.0050   0.5607   0.4956
  -0.750  -0.0936   0.00967   0.00315   0.0052   0.5492   0.5047
  -0.500  -0.0657   0.00972   0.00311   0.0054   0.5371   0.5136
  -0.250  -0.0374   0.00969   0.00313   0.0056   0.5266   0.5226
   0.000  -0.0095   0.00974   0.00313   0.0059   0.5151   0.5317
   0.250   0.0190   0.00975   0.00315   0.0060   0.5050   0.5407
   0.500   0.0468   0.00980   0.00319   0.0063   0.4953   0.5506
   1.000   0.1036   0.00987   0.00328   0.0065   0.4787   0.5692
   1.250   0.1314   0.00997   0.00332   0.0068   0.4702   0.5781
   1.500   0.1605   0.00999   0.00336   0.0068   0.4628   0.5856
   1.750   0.1897   0.01000   0.00340   0.0067   0.4550   0.5933
   2.000   0.2180   0.01011   0.00346   0.0069   0.4473   0.6006
   2.250   0.2472   0.01014   0.00351   0.0068   0.4408   0.6067
   2.500   0.2775   0.01014   0.00355   0.0065   0.4327   0.6141
   2.750   0.3064   0.01023   0.00362   0.0064   0.4248   0.6216
   3.000   0.3359   0.01026   0.00368   0.0063   0.4178   0.6286
   3.250   0.3665   0.01029   0.00374   0.0059   0.4099   0.6364
   3.500   0.3964   0.01036   0.00383   0.0056   0.4021   0.6441
   3.750   0.4265   0.01041   0.00391   0.0054   0.3936   0.6516
   4.000   0.4568   0.01050   0.00399   0.0049   0.3839   0.6595
   4.250   0.4881   0.01052   0.00410   0.0044   0.3746   0.6688
   4.500   0.5179   0.01064   0.00419   0.0041   0.3637   0.6783
   4.750   0.5501   0.01068   0.00432   0.0033   0.3522   0.6897
   5.250   0.6119   0.01097   0.00461   0.0021   0.3216   0.7152
   5.500   0.6431   0.01115   0.00479   0.0014   0.3015   0.7303
   5.750   0.6738   0.01139   0.00502   0.0007   0.2807   0.7485
   6.000   0.7050   0.01167   0.00529  -0.0001   0.2613   0.7693
   6.250   0.7362   0.01199   0.00560  -0.0009   0.2454   0.7914
   6.500   0.7647   0.01225   0.00592  -0.0011   0.2345   0.8140
   6.750   0.7862   0.01255   0.00626   0.0004   0.2261   0.8360
   7.000   0.8018   0.01282   0.00658   0.0032   0.2194   0.8564
   7.250   0.8149   0.01318   0.00692   0.0064   0.2134   0.8737
   7.500   0.8291   0.01345   0.00720   0.0095   0.2086   0.8885
   7.750   0.8435   0.01368   0.00745   0.0125   0.2037   0.9015
   8.000   0.8595   0.01396   0.00771   0.0150   0.1980   0.9139
   8.250   0.8830   0.01420   0.00796   0.0158   0.1928   0.9254
   8.500   0.9182   0.01435   0.00816   0.0141   0.1875   0.9347
   8.750   0.9603   0.01467   0.00847   0.0106   0.1811   0.9419
   9.000   1.0099   0.01495   0.00880   0.0055   0.1748   0.9475
   9.250   1.0617   0.01530   0.00916   0.0000   0.1674   0.9522
   9.500   1.1108   0.01569   0.00959  -0.0050   0.1602   0.9570
   9.750   1.1579   0.01610   0.01000  -0.0096   0.1515   0.9620
  10.000   1.2044   0.01647   0.01039  -0.0139   0.1410   0.9699
  10.250   1.2249   0.01719   0.01106  -0.0128   0.1307   0.9993
  10.500   1.2519   0.01793   0.01166  -0.0134   0.1102   1.0000
  10.750   1.2678   0.01922   0.01271  -0.0125   0.0819   1.0000
  11.000   1.2827   0.02055   0.01392  -0.0114   0.0678   1.0000
  11.250   1.2985   0.02174   0.01507  -0.0104   0.0613   1.0000
  11.500   1.3139   0.02285   0.01619  -0.0094   0.0575   1.0000
  11.750   1.3243   0.02407   0.01743  -0.0077   0.0548   1.0000
  12.000   1.3316   0.02525   0.01868  -0.0058   0.0530   1.0000
  12.250   1.3363   0.02691   0.02037  -0.0045   0.0513   1.0000
  12.500   1.3377   0.02912   0.02263  -0.0037   0.0498   1.0000
  12.750   1.3473   0.03085   0.02444  -0.0035   0.0486   1.0000
  13.000   1.3539   0.03301   0.02667  -0.0036   0.0474   1.0000
  13.250   1.3584   0.03550   0.02923  -0.0039   0.0465   1.0000
  13.500   1.3593   0.03847   0.03226  -0.0044   0.0456   1.0000
  13.750   1.3558   0.04194   0.03579  -0.0051   0.0449   1.0000
  14.000   1.3549   0.04517   0.03911  -0.0057   0.0442   1.0000
  14.250   1.3565   0.04814   0.04217  -0.0063   0.0436   1.0000
  14.500   1.3560   0.05137   0.04549  -0.0070   0.0430   1.0000
  14.750   1.3540   0.05482   0.04902  -0.0078   0.0424   1.0000
  15.000   1.3507   0.05843   0.05272  -0.0087   0.0419   1.0000
  15.250   1.3463   0.06223   0.05659  -0.0097   0.0414   1.0000
  15.500   1.3416   0.06614   0.06057  -0.0108   0.0410   1.0000
  15.750   1.3356   0.07031   0.06480  -0.0121   0.0405   1.0000
  16.000   1.3284   0.07466   0.06920  -0.0133   0.0401   1.0000
  16.500   1.3212   0.08250   0.07718  -0.0157   0.0392   1.0000
  16.750   1.3199   0.08627   0.08102  -0.0169   0.0389   1.0000
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