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TRAINER60 (trainer60-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: TRAINER60 (trainer60-il)
Reynolds number: 100,000
Max Cl/Cd: 38.76 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-trainer60-il-100000-n5.txt
Download as CSV file: xf-trainer60-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0349   0.09588   0.08855   0.0008   1.0000   0.0726
 -15.500  -1.0414   0.09116   0.08376  -0.0011   1.0000   0.0751
 -15.250  -1.0480   0.08648   0.07899  -0.0030   1.0000   0.0779
 -15.000  -1.0564   0.08170   0.07421  -0.0049   1.0000   0.0803
 -14.750  -1.0658   0.07682   0.06925  -0.0069   1.0000   0.0834
 -14.500  -1.0747   0.07215   0.06453  -0.0086   1.0000   0.0867
 -14.250  -1.0856   0.06739   0.05974  -0.0104   1.0000   0.0902
 -14.000  -1.0943   0.06303   0.05530  -0.0119   1.0000   0.0948
 -13.750  -1.1044   0.05864   0.05090  -0.0133   1.0000   0.0993
 -13.500  -1.1114   0.05469   0.04689  -0.0146   1.0000   0.1052
 -13.250  -1.1180   0.05090   0.04307  -0.0157   1.0000   0.1115
 -13.000  -1.1225   0.04745   0.03959  -0.0166   1.0000   0.1187
 -12.750  -1.1241   0.04441   0.03648  -0.0173   1.0000   0.1270
 -12.500  -1.1244   0.04167   0.03368  -0.0178   1.0000   0.1353
 -12.250  -1.1232   0.03928   0.03124  -0.0179   1.0000   0.1430
 -12.000  -1.1190   0.03727   0.02908  -0.0177   1.0000   0.1514
 -11.750  -1.1155   0.03545   0.02723  -0.0171   1.0000   0.1584
 -11.500  -1.1089   0.03393   0.02558  -0.0163   1.0000   0.1660
 -11.250  -1.1031   0.03260   0.02424  -0.0149   1.0000   0.1726
 -11.000  -1.0949   0.03148   0.02293  -0.0133   1.0000   0.1799
 -10.750  -1.0867   0.03050   0.02202  -0.0114   1.0000   0.1859
 -10.500  -1.0746   0.02961   0.02101  -0.0098   1.0000   0.1929
 -10.250  -1.0606   0.02876   0.02014  -0.0085   1.0000   0.1995
 -10.000  -1.0456   0.02798   0.01934  -0.0071   1.0000   0.2066
  -9.750  -1.0288   0.02724   0.01849  -0.0060   1.0000   0.2138
  -9.500  -1.0118   0.02654   0.01786  -0.0048   1.0000   0.2209
  -9.250  -0.9943   0.02588   0.01709  -0.0036   1.0000   0.2298
  -9.000  -0.9764   0.02525   0.01659  -0.0025   1.0000   0.2381
  -8.750  -0.9579   0.02467   0.01590  -0.0013   1.0000   0.2477
  -8.500  -0.9382   0.02410   0.01546  -0.0003   1.0000   0.2554
  -8.250  -0.9179   0.02355   0.01488   0.0007   1.0000   0.2627
  -8.000  -0.8971   0.02300   0.01434   0.0016   1.0000   0.2692
  -7.750  -0.8769   0.02251   0.01392   0.0027   1.0000   0.2757
  -7.250  -0.8082   0.02140   0.01280  -0.0010   0.9603   0.2934
  -7.000  -0.7607   0.02092   0.01222  -0.0054   0.9445   0.3057
  -6.750  -0.7184   0.02058   0.01188  -0.0086   0.9290   0.3174
  -6.500  -0.6841   0.02035   0.01159  -0.0101   0.9122   0.3288
  -6.250  -0.6581   0.02015   0.01135  -0.0098   0.8935   0.3405
  -6.000  -0.6351   0.01993   0.01116  -0.0088   0.8738   0.3513
  -5.750  -0.6121   0.01970   0.01084  -0.0078   0.8548   0.3639
  -5.500  -0.5885   0.01948   0.01067  -0.0068   0.8369   0.3745
  -5.250  -0.5645   0.01926   0.01036  -0.0059   0.8203   0.3863
  -5.000  -0.5401   0.01907   0.01017  -0.0050   0.8050   0.3968
  -4.750  -0.5153   0.01889   0.00988  -0.0041   0.7913   0.4085
  -4.500  -0.4904   0.01874   0.00974  -0.0032   0.7766   0.4192
  -4.250  -0.4649   0.01859   0.00950  -0.0025   0.7640   0.4302
  -4.000  -0.4391   0.01848   0.00936  -0.0018   0.7512   0.4400
  -3.750  -0.4126   0.01836   0.00915  -0.0013   0.7392   0.4506
  -3.500  -0.3860   0.01830   0.00908  -0.0008   0.7271   0.4603
  -3.250  -0.3596   0.01821   0.00890  -0.0003   0.7157   0.4711
  -3.000  -0.3329   0.01818   0.00888   0.0003   0.7045   0.4797
  -2.750  -0.3065   0.01814   0.00874   0.0008   0.6945   0.4903
  -2.500  -0.2799   0.01811   0.00873   0.0013   0.6835   0.4987
  -2.250  -0.2535   0.01810   0.00863   0.0020   0.6740   0.5085
  -2.000  -0.2275   0.01807   0.00860   0.0025   0.6627   0.5178
  -1.750  -0.2009   0.01808   0.00856   0.0031   0.6534   0.5272
  -1.500  -0.1748   0.01809   0.00854   0.0037   0.6435   0.5383
  -1.250  -0.1485   0.01812   0.00860   0.0043   0.6340   0.5490
  -1.000  -0.1225   0.01815   0.00855   0.0050   0.6254   0.5611
  -0.750  -0.0959   0.01815   0.00863   0.0055   0.6149   0.5706
  -0.500  -0.0694   0.01814   0.00852   0.0060   0.6064   0.5803
  -0.250  -0.0423   0.01812   0.00855   0.0064   0.5974   0.5878
   0.000  -0.0154   0.01811   0.00856   0.0068   0.5883   0.5963
   0.250   0.0115   0.01811   0.00844   0.0073   0.5809   0.6056
   0.500   0.0388   0.01809   0.00854   0.0076   0.5710   0.6128
   0.750   0.0660   0.01808   0.00853   0.0080   0.5626   0.6217
   1.000   0.0929   0.01809   0.00850   0.0083   0.5536   0.6309
   1.250   0.1201   0.01804   0.00852   0.0088   0.5417   0.6388
   1.500   0.1471   0.01802   0.00846   0.0092   0.5303   0.6477
   1.750   0.1746   0.01800   0.00845   0.0095   0.5185   0.6567
   2.000   0.2024   0.01802   0.00850   0.0098   0.5090   0.6657
   2.250   0.2302   0.01807   0.00857   0.0100   0.4991   0.6762
   2.500   0.2591   0.01811   0.00860   0.0101   0.4909   0.6849
   2.750   0.2871   0.01819   0.00878   0.0101   0.4804   0.6952
   3.000   0.3155   0.01826   0.00884   0.0103   0.4715   0.7053
   3.250   0.3436   0.01837   0.00902   0.0104   0.4620   0.7165
   3.500   0.3719   0.01846   0.00915   0.0104   0.4520   0.7281
   3.750   0.4002   0.01858   0.00931   0.0105   0.4427   0.7401
   4.000   0.4282   0.01870   0.00951   0.0106   0.4319   0.7524
   4.250   0.4559   0.01884   0.00966   0.0108   0.4222   0.7662
   4.500   0.4829   0.01898   0.00992   0.0112   0.4108   0.7795
   4.750   0.5094   0.01915   0.01010   0.0116   0.4008   0.7948
   5.000   0.5352   0.01932   0.01038   0.0122   0.3890   0.8105
   5.250   0.5607   0.01950   0.01061   0.0128   0.3777   0.8267
   5.500   0.5856   0.01970   0.01085   0.0135   0.3654   0.8449
   5.750   0.6100   0.01993   0.01112   0.0143   0.3533   0.8650
   6.000   0.6336   0.02015   0.01131   0.0152   0.3422   0.8859
   6.250   0.6585   0.02038   0.01160   0.0156   0.3292   0.9070
   6.500   0.6887   0.02057   0.01179   0.0149   0.3169   0.9262
   6.750   0.7297   0.02082   0.01205   0.0118   0.3035   0.9418
   7.000   0.7821   0.02124   0.01256   0.0062   0.2899   0.9531
   7.250   0.8358   0.02177   0.01313   0.0003   0.2780   0.9627
   7.500   0.8703   0.02250   0.01383  -0.0016   0.2687   1.0000
   7.750   0.8929   0.02305   0.01433  -0.0010   0.2621   1.0000
   8.000   0.9159   0.02363   0.01494  -0.0006   0.2551   1.0000
   8.250   0.9381   0.02422   0.01545  -0.0001   0.2480   1.0000
   8.500   0.9599   0.02485   0.01612   0.0004   0.2390   1.0000
   8.750   0.9804   0.02551   0.01667   0.0011   0.2298   1.0000
   9.000   1.0005   0.02620   0.01743   0.0016   0.2195   1.0000
   9.250   1.0196   0.02696   0.01806   0.0023   0.2110   1.0000
   9.500   1.0396   0.02771   0.01894   0.0029   0.2029   1.0000
   9.750   1.0582   0.02852   0.01974   0.0036   0.1962   1.0000
  10.000   1.0767   0.02936   0.02066   0.0042   0.1896   1.0000
  10.250   1.0934   0.03027   0.02163   0.0050   0.1826   1.0000
  10.500   1.1088   0.03127   0.02265   0.0058   0.1762   1.0000
  10.750   1.1226   0.03233   0.02384   0.0067   0.1689   1.0000
  11.000   1.1306   0.03354   0.02503   0.0082   0.1630   1.0000
  11.250   1.1396   0.03490   0.02657   0.0091   0.1554   1.0000
  11.500   1.1449   0.03659   0.02826   0.0098   0.1489   1.0000
  11.750   1.1519   0.03843   0.03027   0.0100   0.1405   1.0000
  12.000   1.1560   0.04064   0.03254   0.0099   0.1327   1.0000
  12.250   1.1576   0.04327   0.03523   0.0093   0.1245   1.0000
  12.500   1.1583   0.04620   0.03824   0.0086   0.1154   1.0000
  12.750   1.1567   0.04948   0.04158   0.0076   0.1076   1.0000
  13.000   1.1521   0.05321   0.04533   0.0064   0.1010   1.0000
  13.250   1.1462   0.05720   0.04937   0.0050   0.0951   1.0000
  13.500   1.1392   0.06142   0.05363   0.0036   0.0904   1.0000
  13.750   1.1309   0.06590   0.05817   0.0019   0.0866   1.0000
  14.000   1.1218   0.07055   0.06285   0.0002   0.0835   1.0000
  14.250   1.1136   0.07522   0.06761  -0.0016   0.0803   1.0000
  14.500   1.1039   0.08020   0.07263  -0.0036   0.0778   1.0000
  14.750   1.0961   0.08502   0.07749  -0.0055   0.0756   1.0000
  15.000   1.0896   0.08981   0.08238  -0.0074   0.0732   1.0000
  15.250   1.0833   0.09457   0.08719  -0.0094   0.0712   1.0000
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