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TRAINER60 (trainer60-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: TRAINER60 (trainer60-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.44 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-trainer60-il-1000000.txt
Download as CSV file: xf-trainer60-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -1.3935   0.10378   0.09963   0.0270   1.0000   0.0257
 -18.500  -1.4052   0.09841   0.09417   0.0250   1.0000   0.0259
 -18.250  -1.4190   0.09281   0.08847   0.0229   1.0000   0.0261
 -18.000  -1.4292   0.08783   0.08340   0.0212   1.0000   0.0264
 -17.750  -1.4397   0.08283   0.07831   0.0195   1.0000   0.0266
 -17.500  -1.4500   0.07790   0.07328   0.0178   1.0000   0.0267
 -17.250  -1.4588   0.07327   0.06856   0.0164   1.0000   0.0270
 -17.000  -1.4662   0.06887   0.06406   0.0151   1.0000   0.0271
 -16.750  -1.4729   0.06465   0.05974   0.0139   1.0000   0.0273
 -16.500  -1.4865   0.05971   0.05471   0.0126   1.0000   0.0276
 -16.250  -1.4990   0.05507   0.04997   0.0115   1.0000   0.0279
 -16.000  -1.5092   0.05082   0.04563   0.0106   1.0000   0.0283
 -15.750  -1.5144   0.04715   0.04188   0.0100   1.0000   0.0287
 -15.500  -1.5173   0.04377   0.03843   0.0094   1.0000   0.0291
 -15.250  -1.5159   0.04087   0.03547   0.0089   1.0000   0.0297
 -15.000  -1.5129   0.03814   0.03267   0.0084   1.0000   0.0302
 -14.750  -1.5074   0.03572   0.03018   0.0080   1.0000   0.0307
 -14.500  -1.5002   0.03354   0.02792   0.0078   1.0000   0.0311
 -14.250  -1.4961   0.03110   0.02541   0.0077   1.0000   0.0317
 -14.000  -1.4923   0.02879   0.02304   0.0078   1.0000   0.0326
 -13.750  -1.4845   0.02698   0.02119   0.0082   1.0000   0.0334
 -13.500  -1.4686   0.02548   0.01964   0.0076   0.9994   0.0343
 -13.250  -1.4476   0.02427   0.01837   0.0066   0.9982   0.0353
 -13.000  -1.4301   0.02295   0.01702   0.0062   0.9962   0.0367
 -12.750  -1.4361   0.02184   0.01587   0.0114   0.9679   0.0375
 -12.500  -1.4086   0.02096   0.01494   0.0101   0.9620   0.0392
 -12.250  -1.3799   0.02011   0.01405   0.0088   0.9565   0.0411
 -12.000  -1.3433   0.01913   0.01307   0.0058   0.9546   0.0441
 -11.750  -1.3043   0.01818   0.01212   0.0024   0.9529   0.0480
 -11.500  -1.2649   0.01728   0.01123  -0.0011   0.9500   0.0534
 -11.250  -1.2278   0.01642   0.01040  -0.0041   0.9457   0.0613
 -11.000  -1.1949   0.01550   0.00955  -0.0063   0.9410   0.0743
 -10.750  -1.1626   0.01454   0.00872  -0.0084   0.9358   0.0944
 -10.500  -1.1341   0.01382   0.00810  -0.0094   0.9302   0.1143
 -10.250  -1.1069   0.01332   0.00768  -0.0098   0.9240   0.1288
 -10.000  -1.0802   0.01303   0.00740  -0.0097   0.9179   0.1383
  -9.750  -1.0546   0.01272   0.00713  -0.0095   0.9117   0.1466
  -9.500  -1.0305   0.01251   0.00691  -0.0087   0.9052   0.1521
  -9.250  -1.0069   0.01224   0.00665  -0.0079   0.8985   0.1587
  -9.000  -0.9847   0.01205   0.00646  -0.0066   0.8911   0.1634
  -8.750  -0.9618   0.01183   0.00622  -0.0055   0.8837   0.1677
  -8.500  -0.9415   0.01156   0.00598  -0.0038   0.8732   0.1726
  -8.250  -0.9195   0.01136   0.00576  -0.0024   0.8611   0.1768
  -8.000  -0.8975   0.01122   0.00557  -0.0009   0.8419   0.1798
  -7.750  -0.8763   0.01100   0.00527   0.0006   0.8109   0.1848
  -7.500  -0.8494   0.01084   0.00501   0.0010   0.7761   0.1897
  -7.250  -0.8202   0.01074   0.00481   0.0008   0.7510   0.1944
  -7.000  -0.7918   0.01060   0.00461   0.0007   0.7333   0.1991
  -6.750  -0.7646   0.01040   0.00439   0.0009   0.7189   0.2066
  -6.500  -0.7364   0.01028   0.00424   0.0010   0.7067   0.2127
  -6.250  -0.7102   0.01004   0.00402   0.0014   0.6960   0.2239
  -6.000  -0.6829   0.00988   0.00385   0.0016   0.6863   0.2327
  -5.750  -0.6564   0.00968   0.00366   0.0020   0.6760   0.2442
  -5.500  -0.6298   0.00946   0.00349   0.0024   0.6685   0.2571
  -5.250  -0.6032   0.00925   0.00333   0.0028   0.6606   0.2732
  -5.000  -0.5764   0.00908   0.00318   0.0032   0.6521   0.2911
  -4.750  -0.5491   0.00890   0.00306   0.0034   0.6461   0.3082
  -4.500  -0.5213   0.00876   0.00296   0.0037   0.6389   0.3234
  -4.250  -0.4937   0.00864   0.00286   0.0039   0.6305   0.3382
  -4.000  -0.4653   0.00855   0.00278   0.0040   0.6237   0.3488
  -3.750  -0.4370   0.00846   0.00271   0.0041   0.6160   0.3594
  -3.500  -0.4083   0.00842   0.00263   0.0042   0.6077   0.3674
  -3.250  -0.3799   0.00833   0.00256   0.0043   0.6006   0.3765
  -3.000  -0.3508   0.00828   0.00251   0.0043   0.5925   0.3837
  -2.750  -0.3224   0.00823   0.00244   0.0045   0.5833   0.3918
  -2.500  -0.2935   0.00816   0.00239   0.0045   0.5754   0.4002
  -2.250  -0.2644   0.00814   0.00234   0.0045   0.5652   0.4062
  -2.000  -0.2358   0.00808   0.00228   0.0046   0.5546   0.4148
  -1.750  -0.2069   0.00806   0.00224   0.0046   0.5419   0.4224
  -1.500  -0.1778   0.00806   0.00220   0.0046   0.5291   0.4289
  -1.250  -0.1493   0.00803   0.00216   0.0047   0.5152   0.4379
  -1.000  -0.1199   0.00802   0.00214   0.0046   0.5048   0.4461
  -0.750  -0.0911   0.00803   0.00213   0.0046   0.4923   0.4554
  -0.500  -0.0617   0.00801   0.00212   0.0045   0.4821   0.4656
  -0.250  -0.0326   0.00804   0.00212   0.0045   0.4709   0.4743
   0.000  -0.0030   0.00802   0.00213   0.0044   0.4633   0.4845
   0.250   0.0266   0.00805   0.00214   0.0042   0.4551   0.4930
   0.500   0.0559   0.00807   0.00217   0.0041   0.4458   0.5040
   0.750   0.0858   0.00809   0.00220   0.0040   0.4393   0.5140
   1.000   0.1156   0.00810   0.00224   0.0038   0.4319   0.5246
   1.250   0.1449   0.00816   0.00228   0.0037   0.4244   0.5340
   1.500   0.1752   0.00817   0.00232   0.0034   0.4183   0.5428
   1.750   0.2049   0.00821   0.00237   0.0032   0.4108   0.5524
   2.000   0.2340   0.00831   0.00243   0.0032   0.4033   0.5587
   2.250   0.2651   0.00830   0.00247   0.0027   0.3979   0.5671
   2.500   0.2955   0.00834   0.00252   0.0024   0.3910   0.5736
   2.750   0.3249   0.00845   0.00259   0.0023   0.3827   0.5791
   3.000   0.3552   0.00849   0.00263   0.0020   0.3766   0.5835
   3.250   0.3869   0.00853   0.00269   0.0013   0.3677   0.5904
   3.500   0.4179   0.00860   0.00277   0.0008   0.3595   0.5967
   3.750   0.4486   0.00866   0.00283   0.0004   0.3505   0.6023
   4.000   0.4785   0.00879   0.00291   0.0002   0.3400   0.6069
   4.250   0.5116   0.00885   0.00299  -0.0009   0.3275   0.6142
   4.500   0.5434   0.00897   0.00309  -0.0016   0.3118   0.6205
   4.750   0.5741   0.00916   0.00321  -0.0022   0.2916   0.6264
   5.000   0.6052   0.00942   0.00337  -0.0029   0.2678   0.6326
   5.250   0.6395   0.00969   0.00357  -0.0044   0.2435   0.6415
   5.500   0.6718   0.00994   0.00377  -0.0054   0.2276   0.6498
   5.750   0.7058   0.01013   0.00396  -0.0067   0.2173   0.6601
   6.000   0.7398   0.01032   0.00416  -0.0081   0.2088   0.6719
   6.250   0.7745   0.01048   0.00436  -0.0095   0.2018   0.6860
   6.500   0.8088   0.01070   0.00460  -0.0110   0.1936   0.7038
   6.750   0.8447   0.01083   0.00480  -0.0127   0.1885   0.7255
   7.000   0.8802   0.01105   0.00506  -0.0144   0.1818   0.7495
   7.250   0.9175   0.01123   0.00532  -0.0165   0.1762   0.7725
   7.500   0.9503   0.01140   0.00556  -0.0175   0.1712   0.7945
   7.750   0.9792   0.01162   0.00585  -0.0177   0.1659   0.8185
   8.000   1.0048   0.01183   0.00612  -0.0171   0.1617   0.8396
   8.250   1.0278   0.01203   0.00637  -0.0160   0.1578   0.8572
   8.500   1.0479   0.01231   0.00665  -0.0142   0.1529   0.8720
   8.750   1.0648   0.01259   0.00692  -0.0118   0.1482   0.8841
   9.000   1.0777   0.01279   0.00714  -0.0084   0.1441   0.8925
   9.250   1.0918   0.01310   0.00742  -0.0054   0.1377   0.9001
   9.500   1.1096   0.01337   0.00769  -0.0033   0.1317   0.9061
   9.750   1.1265   0.01374   0.00801  -0.0011   0.1220   0.9119
  10.000   1.1477   0.01422   0.00841  -0.0001   0.1076   0.9171
  10.250   1.1633   0.01507   0.00908   0.0017   0.0840   0.9224
  10.750   1.2077   0.01687   0.01068   0.0021   0.0548   0.9307
  11.000   1.2425   0.01766   0.01145  -0.0004   0.0492   0.9330
  11.250   1.2741   0.01838   0.01217  -0.0021   0.0457   0.9362
  11.500   1.2979   0.01902   0.01282  -0.0020   0.0436   0.9406
  11.750   1.3275   0.01969   0.01352  -0.0033   0.0417   0.9439
  12.000   1.3502   0.02048   0.01433  -0.0034   0.0402   0.9478
  12.250   1.3741   0.02123   0.01512  -0.0038   0.0390   0.9513
  12.500   1.3953   0.02196   0.01591  -0.0038   0.0380   0.9554
  12.750   1.4162   0.02291   0.01694  -0.0043   0.0370   0.9603
  13.000   1.4408   0.02427   0.01836  -0.0064   0.0360   0.9649
  13.250   1.4268   0.02598   0.02010  -0.0007   0.0357   0.9961
  13.500   1.4429   0.02782   0.02201  -0.0021   0.0348   0.9978
  13.750   1.4645   0.02926   0.02352  -0.0039   0.0343   0.9992
  14.000   1.4828   0.03104   0.02536  -0.0056   0.0337   1.0000
  14.250   1.4908   0.03310   0.02749  -0.0058   0.0332   1.0000
  14.500   1.4971   0.03541   0.02986  -0.0061   0.0328   1.0000
  14.750   1.5018   0.03790   0.03240  -0.0065   0.0322   1.0000
  15.000   1.5028   0.04084   0.03541  -0.0070   0.0319   1.0000
  15.250   1.5000   0.04424   0.03889  -0.0077   0.0315   1.0000
  15.500   1.4941   0.04802   0.04275  -0.0085   0.0311   1.0000
  15.750   1.4813   0.05268   0.04752  -0.0095   0.0306   1.0000
  16.000   1.4785   0.05620   0.05113  -0.0103   0.0305   1.0000
  16.250   1.4748   0.05990   0.05492  -0.0113   0.0303   1.0000
  16.500   1.4696   0.06387   0.05898  -0.0124   0.0301   1.0000
  16.750   1.4632   0.06810   0.06330  -0.0137   0.0299   1.0000
  17.000   1.4546   0.07274   0.06803  -0.0152   0.0298   1.0000
  17.250   1.4463   0.07738   0.07276  -0.0167   0.0296   1.0000
  17.500   1.4381   0.08204   0.07752  -0.0183   0.0292   1.0000
  17.750   1.4278   0.08707   0.08263  -0.0201   0.0291   1.0000
  18.000   1.4173   0.09219   0.08784  -0.0219   0.0289   1.0000
  18.250   1.4067   0.09737   0.09311  -0.0239   0.0287   1.0000
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