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TRAINER60 (trainer60-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: TRAINER60 (trainer60-il)
Reynolds number: 100,000
Max Cl/Cd: 36.69 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-trainer60-il-100000.txt
Download as CSV file: xf-trainer60-il-100000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.4561   0.18031   0.17515   0.0234   1.0000   0.1418
 -17.250  -0.4507   0.17811   0.17293   0.0224   1.0000   0.1466
 -17.000  -1.1463   0.09755   0.09080  -0.0116   1.0000   0.0857
 -16.500  -1.1051   0.09646   0.08994  -0.0097   1.0000   0.0907
 -16.250  -1.1424   0.08729   0.08046  -0.0144   1.0000   0.0911
 -16.000  -0.9026   0.09317   0.08718  -0.0214   1.0000   0.1034
 -15.750  -0.9636   0.08188   0.07555  -0.0259   1.0000   0.1031
 -15.500  -1.2066   0.06918   0.06151  -0.0215   1.0000   0.0948
 -15.250  -1.1774   0.06933   0.06197  -0.0202   1.0000   0.0987
 -15.000  -1.1832   0.06548   0.05797  -0.0211   1.0000   0.1013
 -14.750  -1.1964   0.06091   0.05310  -0.0223   1.0000   0.1037
 -14.500  -1.1802   0.05965   0.05205  -0.0217   1.0000   0.1078
 -14.250  -1.1823   0.05651   0.04881  -0.0222   1.0000   0.1118
 -14.000  -1.1838   0.05347   0.04569  -0.0225   1.0000   0.1162
 -13.750  -1.1801   0.05121   0.04350  -0.0225   1.0000   0.1215
 -13.500  -1.1842   0.04816   0.04031  -0.0226   1.0000   0.1271
 -13.250  -1.1816   0.04607   0.03830  -0.0223   1.0000   0.1336
 -13.000  -1.1845   0.04361   0.03580  -0.0218   1.0000   0.1409
 -12.750  -1.1906   0.04128   0.03337  -0.0208   1.0000   0.1492
 -12.500  -1.1888   0.03973   0.03192  -0.0195   1.0000   0.1580
 -12.250  -1.1956   0.03789   0.02998  -0.0170   1.0000   0.1675
 -12.000  -1.1989   0.03670   0.02876  -0.0139   1.0000   0.1774
 -11.750  -1.1917   0.03574   0.02789  -0.0119   1.0000   0.1881
 -11.500  -1.1886   0.03455   0.02657  -0.0094   1.0000   0.1987
 -11.250  -1.1770   0.03385   0.02587  -0.0076   1.0000   0.2095
 -11.000  -1.1606   0.03310   0.02519  -0.0063   1.0000   0.2195
 -10.750  -1.1517   0.03224   0.02411  -0.0042   1.0000   0.2293
 -10.500  -1.1275   0.03173   0.02380  -0.0037   1.0000   0.2386
 -10.250  -1.1166   0.03088   0.02269  -0.0018   1.0000   0.2478
 -10.000  -1.0900   0.03047   0.02251  -0.0016   1.0000   0.2565
  -9.750  -1.0757   0.02971   0.02155   0.0001   1.0000   0.2654
  -9.500  -1.0499   0.02927   0.02128   0.0004   1.0000   0.2737
  -9.250  -1.0321   0.02870   0.02059   0.0017   1.0000   0.2828
  -9.000  -1.0083   0.02827   0.02027   0.0023   1.0000   0.2914
  -8.750  -0.9888   0.02789   0.01984   0.0035   1.0000   0.3012
  -8.500  -0.9656   0.02749   0.01952   0.0043   1.0000   0.3101
  -8.250  -0.9445   0.02711   0.01915   0.0053   1.0000   0.3192
  -8.000  -0.9252   0.02635   0.01833   0.0064   1.0000   0.3269
  -7.750  -0.9008   0.02595   0.01804   0.0070   1.0000   0.3340
  -7.500  -0.8852   0.02524   0.01716   0.0087   1.0000   0.3422
  -7.250  -0.8642   0.02470   0.01675   0.0097   1.0000   0.3492
  -7.000  -0.8486   0.02433   0.01643   0.0114   1.0000   0.3569
  -6.750  -0.8460   0.02386   0.01580   0.0148   1.0000   0.3649
  -6.500  -0.8358   0.02370   0.01583   0.0170   1.0000   0.3712
  -6.250  -0.7920   0.02303   0.01502   0.0130   0.9839   0.3858
  -6.000  -0.7378   0.02265   0.01481   0.0080   0.9745   0.3999
  -5.750  -0.6818   0.02219   0.01441   0.0025   0.9669   0.4161
  -5.500  -0.6250   0.02185   0.01408  -0.0031   0.9586   0.4341
  -5.250  -0.5721   0.02166   0.01387  -0.0080   0.9469   0.4523
  -5.000  -0.5240   0.02169   0.01386  -0.0118   0.9332   0.4692
  -4.750  -0.4861   0.02206   0.01435  -0.0132   0.9155   0.4809
  -4.500  -0.4581   0.02223   0.01445  -0.0131   0.8981   0.4948
  -4.250  -0.4323   0.02256   0.01484  -0.0121   0.8806   0.5054
  -4.000  -0.4108   0.02255   0.01476  -0.0106   0.8644   0.5171
  -3.750  -0.3843   0.02269   0.01495  -0.0095   0.8503   0.5270
  -3.500  -0.3642   0.02255   0.01471  -0.0078   0.8350   0.5387
  -3.250  -0.3379   0.02264   0.01487  -0.0067   0.8213   0.5477
  -3.000  -0.3168   0.02244   0.01450  -0.0051   0.8098   0.5600
  -2.750  -0.2896   0.02243   0.01459  -0.0042   0.7961   0.5680
  -2.500  -0.2673   0.02232   0.01438  -0.0028   0.7836   0.5794
  -2.250  -0.2413   0.02217   0.01422  -0.0017   0.7719   0.5883
  -2.000  -0.2169   0.02218   0.01423  -0.0007   0.7593   0.5982
  -1.750  -0.1930   0.02199   0.01395   0.0005   0.7487   0.6089
  -1.500  -0.1671   0.02207   0.01410   0.0014   0.7361   0.6181
  -1.250  -0.1444   0.02195   0.01384   0.0028   0.7256   0.6305
  -1.000  -0.1177   0.02210   0.01411   0.0036   0.7135   0.6401
  -0.750  -0.0952   0.02207   0.01398   0.0049   0.7035   0.6537
  -0.500  -0.0677   0.02221   0.01422   0.0056   0.6934   0.6627
  -0.250  -0.0444   0.02219   0.01416   0.0067   0.6825   0.6742
   0.000  -0.0172   0.02217   0.01411   0.0074   0.6743   0.6830
   0.250   0.0065   0.02230   0.01433   0.0082   0.6628   0.6930
   0.500   0.0317   0.02223   0.01420   0.0091   0.6545   0.7039
   0.750   0.0568   0.02237   0.01441   0.0099   0.6437   0.7133
   1.000   0.0807   0.02222   0.01418   0.0110   0.6328   0.7251
   1.250   0.1072   0.02225   0.01427   0.0119   0.6216   0.7343
   1.500   0.1302   0.02216   0.01413   0.0131   0.6105   0.7474
   1.750   0.1584   0.02217   0.01416   0.0139   0.6018   0.7565
   2.000   0.1805   0.02222   0.01426   0.0149   0.5906   0.7692
   2.250   0.2093   0.02216   0.01418   0.0156   0.5826   0.7788
   2.500   0.2309   0.02230   0.01439   0.0167   0.5720   0.7924
   2.750   0.2585   0.02226   0.01438   0.0176   0.5626   0.8024
   3.000   0.2827   0.02231   0.01443   0.0186   0.5534   0.8154
   3.250   0.3079   0.02234   0.01454   0.0196   0.5426   0.8268
   3.500   0.3354   0.02225   0.01436   0.0204   0.5343   0.8395
   3.750   0.3569   0.02235   0.01459   0.0218   0.5221   0.8540
   4.000   0.3850   0.02217   0.01427   0.0225   0.5135   0.8691
   4.250   0.4072   0.02222   0.01446   0.0236   0.5001   0.8852
   4.500   0.4384   0.02191   0.01401   0.0236   0.4902   0.9026
   4.750   0.4657   0.02169   0.01391   0.0236   0.4757   0.9242
   5.000   0.5127   0.02143   0.01367   0.0197   0.4599   0.9437
   5.250   0.5779   0.02144   0.01365   0.0123   0.4408   0.9557
   5.500   0.6446   0.02173   0.01389   0.0047   0.4209   0.9627
   5.750   0.7062   0.02211   0.01418  -0.0018   0.4023   0.9693
   6.000   0.7620   0.02255   0.01457  -0.0073   0.3844   0.9786
   6.250   0.8000   0.02324   0.01536  -0.0105   0.3698   1.0000
   6.500   0.8110   0.02335   0.01526  -0.0084   0.3627   1.0000
   6.750   0.8236   0.02390   0.01593  -0.0066   0.3526   1.0000
   7.000   0.8460   0.02424   0.01613  -0.0059   0.3443   1.0000
   7.250   0.8665   0.02497   0.01692  -0.0052   0.3360   1.0000
   7.500   0.8892   0.02555   0.01751  -0.0046   0.3278   1.0000
   7.750   0.9162   0.02609   0.01787  -0.0045   0.3211   1.0000
   8.000   0.9353   0.02692   0.01893  -0.0036   0.3124   1.0000
   8.250   0.9629   0.02711   0.01892  -0.0034   0.3039   1.0000
   8.500   0.9824   0.02771   0.01965  -0.0026   0.2933   1.0000
   8.750   1.0105   0.02777   0.01942  -0.0025   0.2833   1.0000
   9.000   1.0285   0.02841   0.02028  -0.0015   0.2731   1.0000
   9.250   1.0564   0.02879   0.02042  -0.0015   0.2651   1.0000
   9.500   1.0737   0.02967   0.02157  -0.0005   0.2565   1.0000
   9.750   1.0997   0.03008   0.02180  -0.0004   0.2482   1.0000
  10.000   1.1169   0.03104   0.02295   0.0006   0.2395   1.0000
  10.250   1.1413   0.03151   0.02329   0.0009   0.2305   1.0000
  10.500   1.1563   0.03255   0.02452   0.0020   0.2213   1.0000
  10.750   1.1811   0.03311   0.02482   0.0022   0.2113   1.0000
  11.000   1.1895   0.03421   0.02622   0.0039   0.2009   1.0000
  11.250   1.2033   0.03519   0.02719   0.0051   0.1898   1.0000
  11.500   1.2173   0.03608   0.02791   0.0062   0.1778   1.0000
  11.750   1.2179   0.03753   0.02952   0.0083   0.1658   1.0000
  12.000   1.2137   0.03929   0.03137   0.0109   0.1554   1.0000
  12.250   1.2139   0.04102   0.03305   0.0124   0.1462   1.0000
  12.500   1.2141   0.04295   0.03495   0.0134   0.1377   1.0000
  12.750   1.2110   0.04560   0.03774   0.0140   0.1303   1.0000
  13.000   1.2204   0.04724   0.03918   0.0143   0.1241   1.0000
  13.250   1.2146   0.05055   0.04274   0.0142   0.1189   1.0000
  13.500   1.2228   0.05249   0.04458   0.0142   0.1142   1.0000
  13.750   1.2229   0.05554   0.04775   0.0140   0.1104   1.0000
  14.000   1.2228   0.05864   0.05099   0.0135   0.1070   1.0000
  14.250   1.2379   0.06009   0.05229   0.0139   0.1036   1.0000
  14.500   1.2362   0.06357   0.05592   0.0134   0.1011   1.0000
  14.750   1.2269   0.06791   0.06051   0.0122   0.0991   1.0000
  15.000   1.2221   0.07182   0.06456   0.0112   0.0971   1.0000
  15.250   1.2364   0.07338   0.06601   0.0114   0.0945   1.0000
  15.500   1.2416   0.07628   0.06894   0.0111   0.0927   1.0000
  15.750   1.2148   0.08312   0.07611   0.0082   0.0919   1.0000
  16.000   1.1808   0.09142   0.08475   0.0043   0.0915   1.0000
  16.250   1.1282   0.10343   0.09713  -0.0022   0.0918   1.0000
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