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FX 60-160 AIRFOIL (fx60160-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 60-160 AIRFOIL (fx60160-il)
Reynolds number: 500,000
Max Cl/Cd: 88.96 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60160-il-500000-n5.txt
Download as CSV file: xf-fx60160-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 60-160 AIRFOIL                               
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.7825   0.07449   0.07153  -0.0826   1.0000   0.0153
 -16.000  -0.8198   0.06522   0.06204  -0.0878   1.0000   0.0153
 -15.750  -0.8372   0.05988   0.05657  -0.0902   1.0000   0.0154
 -15.500  -0.8532   0.05530   0.05186  -0.0918   1.0000   0.0156
 -15.250  -0.8671   0.05150   0.04792  -0.0926   1.0000   0.0157
 -15.000  -0.8796   0.04821   0.04452  -0.0927   1.0000   0.0159
 -14.750  -0.8894   0.04551   0.04171  -0.0921   1.0000   0.0161
 -14.500  -0.8949   0.04284   0.03891  -0.0922   0.9996   0.0163
 -14.250  -0.8857   0.04009   0.03598  -0.0948   0.9978   0.0167
 -14.000  -0.8758   0.03752   0.03322  -0.0971   0.9953   0.0171
 -13.750  -0.8635   0.03547   0.03103  -0.0988   0.9925   0.0175
 -13.500  -0.8493   0.03374   0.02925  -0.1006   0.9893   0.0179
 -13.250  -0.8294   0.03247   0.02793  -0.1026   0.9865   0.0183
 -13.000  -0.8092   0.03101   0.02639  -0.1048   0.9842   0.0186
 -12.750  -0.7912   0.02988   0.02520  -0.1060   0.9803   0.0190
 -12.500  -0.7720   0.02860   0.02382  -0.1074   0.9765   0.0195
 -12.250  -0.7493   0.02732   0.02242  -0.1093   0.9737   0.0200
 -12.000  -0.7268   0.02609   0.02106  -0.1110   0.9704   0.0206
 -11.750  -0.7070   0.02497   0.01980  -0.1119   0.9650   0.0211
 -11.500  -0.6801   0.02395   0.01863  -0.1139   0.9617   0.0215
 -11.250  -0.6535   0.02265   0.01728  -0.1162   0.9585   0.0222
 -11.000  -0.6368   0.02184   0.01640  -0.1160   0.9499   0.0226
 -10.750  -0.6084   0.02123   0.01575  -0.1176   0.9451   0.0232
 -10.500  -0.5901   0.02065   0.01509  -0.1170   0.9361   0.0237
 -10.250  -0.5632   0.01999   0.01435  -0.1180   0.9297   0.0243
 -10.000  -0.5442   0.01937   0.01365  -0.1172   0.9186   0.0249
  -9.750  -0.5216   0.01876   0.01293  -0.1171   0.9076   0.0255
  -9.500  -0.4978   0.01819   0.01225  -0.1171   0.8955   0.0261
  -9.250  -0.4740   0.01762   0.01155  -0.1171   0.8818   0.0265
  -9.000  -0.4526   0.01691   0.01072  -0.1166   0.8668   0.0270
  -8.750  -0.4317   0.01631   0.01004  -0.1161   0.8518   0.0277
  -8.500  -0.4098   0.01589   0.00952  -0.1155   0.8384   0.0283
  -8.250  -0.3879   0.01553   0.00907  -0.1149   0.8267   0.0288
  -8.000  -0.3654   0.01521   0.00868  -0.1144   0.8164   0.0296
  -7.750  -0.3430   0.01488   0.00825  -0.1138   0.8072   0.0304
  -7.500  -0.3204   0.01455   0.00784  -0.1132   0.7984   0.0312
  -7.250  -0.2976   0.01420   0.00741  -0.1127   0.7911   0.0318
  -7.000  -0.2743   0.01388   0.00701  -0.1122   0.7840   0.0325
  -6.500  -0.2285   0.01312   0.00612  -0.1113   0.7710   0.0341
  -6.250  -0.2044   0.01281   0.00578  -0.1109   0.7650   0.0353
  -6.000  -0.1795   0.01259   0.00550  -0.1107   0.7599   0.0365
  -5.750  -0.1542   0.01235   0.00524  -0.1105   0.7545   0.0378
  -5.500  -0.1289   0.01213   0.00496  -0.1103   0.7491   0.0392
  -5.250  -0.1033   0.01193   0.00469  -0.1101   0.7445   0.0403
  -5.000  -0.0778   0.01167   0.00440  -0.1100   0.7398   0.0417
  -4.750  -0.0523   0.01141   0.00412  -0.1098   0.7349   0.0439
  -4.500  -0.0261   0.01124   0.00391  -0.1097   0.7303   0.0463
  -4.250   0.0004   0.01109   0.00373  -0.1097   0.7261   0.0488
  -4.000   0.0271   0.01094   0.00355  -0.1096   0.7216   0.0509
  -3.750   0.0533   0.01074   0.00333  -0.1095   0.7170   0.0549
  -3.250   0.1069   0.01046   0.00301  -0.1095   0.7086   0.0645
  -3.000   0.1334   0.01028   0.00286  -0.1095   0.7040   0.0763
  -2.750   0.1583   0.00987   0.00266  -0.1094   0.6995   0.1423
  -2.500   0.1802   0.00897   0.00233  -0.1091   0.6953   0.3172
  -2.250   0.2049   0.00850   0.00216  -0.1090   0.6904   0.4035
  -2.000   0.2300   0.00819   0.00210  -0.1088   0.6856   0.4843
  -1.750   0.2565   0.00810   0.00210  -0.1086   0.6813   0.5290
  -1.500   0.2838   0.00806   0.00213  -0.1086   0.6768   0.5542
  -1.250   0.3112   0.00807   0.00215  -0.1085   0.6720   0.5724
  -1.000   0.3387   0.00810   0.00218  -0.1085   0.6676   0.5864
  -0.750   0.3662   0.00815   0.00223  -0.1085   0.6633   0.6010
  -0.500   0.3938   0.00819   0.00228  -0.1085   0.6585   0.6101
  -0.250   0.4214   0.00825   0.00230  -0.1085   0.6536   0.6187
   0.000   0.4487   0.00832   0.00236  -0.1084   0.6492   0.6262
   0.250   0.4764   0.00836   0.00239  -0.1084   0.6441   0.6326
   0.500   0.5037   0.00842   0.00244  -0.1083   0.6390   0.6371
   0.750   0.5308   0.00849   0.00248  -0.1082   0.6342   0.6414
   1.000   0.5583   0.00853   0.00253  -0.1082   0.6290   0.6459
   1.250   0.5856   0.00860   0.00257  -0.1082   0.6235   0.6502
   1.500   0.6123   0.00866   0.00263  -0.1080   0.6185   0.6531
   1.750   0.6395   0.00871   0.00271  -0.1080   0.6130   0.6564
   2.000   0.6661   0.00878   0.00277  -0.1078   0.6069   0.6603
   2.250   0.6928   0.00886   0.00283  -0.1076   0.6013   0.6638
   2.500   0.7194   0.00892   0.00291  -0.1075   0.5948   0.6667
   2.750   0.7447   0.00900   0.00299  -0.1070   0.5865   0.6692
   3.000   0.7698   0.00909   0.00307  -0.1065   0.5756   0.6717
   3.250   0.7948   0.00919   0.00316  -0.1061   0.5654   0.6742
   3.500   0.8188   0.00931   0.00325  -0.1054   0.5530   0.6769
   3.750   0.8408   0.00948   0.00335  -0.1043   0.5334   0.6796
   4.000   0.8607   0.00971   0.00347  -0.1028   0.5100   0.6820
   4.250   0.8816   0.00991   0.00363  -0.1016   0.4900   0.6840
   4.500   0.9012   0.01016   0.00382  -0.1001   0.4686   0.6863
   4.750   0.9202   0.01044   0.00402  -0.0985   0.4485   0.6888
   5.000   0.9393   0.01072   0.00424  -0.0969   0.4286   0.6913
   5.250   0.9547   0.01106   0.00448  -0.0947   0.4046   0.6938
   5.500   0.9661   0.01151   0.00477  -0.0917   0.3731   0.6962
   5.750   0.9758   0.01204   0.00515  -0.0884   0.3363   0.6984
   6.000   0.9824   0.01276   0.00565  -0.0847   0.2900   0.7007
   6.250   0.9828   0.01378   0.00635  -0.0802   0.2255   0.7031
   6.500   0.9788   0.01506   0.00726  -0.0751   0.1560   0.7056
   6.750   0.9736   0.01646   0.00829  -0.0700   0.0847   0.7083
   7.000   0.9874   0.01703   0.00883  -0.0680   0.0736   0.7109
   7.250   1.0021   0.01757   0.00936  -0.0662   0.0658   0.7131
   7.500   1.0171   0.01808   0.00991  -0.0645   0.0602   0.7154
   7.750   1.0315   0.01864   0.01049  -0.0627   0.0554   0.7179
   8.000   1.0468   0.01918   0.01106  -0.0611   0.0519   0.7204
   8.250   1.0607   0.01980   0.01169  -0.0594   0.0486   0.7229
   8.500   1.0740   0.02049   0.01239  -0.0576   0.0460   0.7256
   8.750   1.0887   0.02111   0.01307  -0.0561   0.0447   0.7283
   9.000   1.1026   0.02178   0.01380  -0.0546   0.0432   0.7307
   9.250   1.1158   0.02251   0.01458  -0.0530   0.0417   0.7332
   9.500   1.1285   0.02330   0.01541  -0.0515   0.0404   0.7360
   9.750   1.1399   0.02420   0.01635  -0.0499   0.0384   0.7390
  10.000   1.1498   0.02524   0.01742  -0.0482   0.0371   0.7422
  10.250   1.1626   0.02610   0.01836  -0.0469   0.0365   0.7451
  10.500   1.1750   0.02702   0.01935  -0.0456   0.0358   0.7480
  10.750   1.1865   0.02802   0.02042  -0.0443   0.0353   0.7512
  11.000   1.1985   0.02901   0.02148  -0.0431   0.0342   0.7548
  11.250   1.2096   0.03010   0.02264  -0.0419   0.0334   0.7587
  11.500   1.2201   0.03125   0.02386  -0.0408   0.0326   0.7626
  11.750   1.2302   0.03247   0.02513  -0.0396   0.0315   0.7670
  12.000   1.2388   0.03383   0.02655  -0.0385   0.0307   0.7716
  12.250   1.2455   0.03540   0.02818  -0.0373   0.0296   0.7764
  12.500   1.2558   0.03670   0.02958  -0.0364   0.0291   0.7822
  12.750   1.2657   0.03806   0.03104  -0.0356   0.0287   0.7891
  13.000   1.2761   0.03938   0.03248  -0.0348   0.0281   0.7977
  13.250   1.2869   0.04068   0.03389  -0.0341   0.0268   0.8092
  13.500   1.2970   0.04212   0.03545  -0.0335   0.0260   0.8270
  13.750   1.3157   0.04373   0.03726  -0.0349   0.0245   0.8902
  14.000   1.3314   0.04563   0.03926  -0.0363   0.0232   1.0000
  14.250   1.3406   0.04731   0.04102  -0.0359   0.0224   1.0000
  14.500   1.3502   0.04896   0.04273  -0.0355   0.0204   1.0000
  14.750   1.3584   0.05078   0.04457  -0.0352   0.0184   1.0000
  15.000   1.3654   0.05276   0.04661  -0.0348   0.0155   1.0000
  15.500   1.3726   0.05754   0.05138  -0.0343   0.0107   1.0000
  15.750   1.3736   0.06029   0.05418  -0.0340   0.0097   1.0000
  16.000   1.3760   0.06297   0.05692  -0.0339   0.0092   1.0000
  16.250   1.3783   0.06571   0.05975  -0.0339   0.0087   1.0000
  16.500   1.3800   0.06856   0.06269  -0.0340   0.0084   1.0000
  16.750   1.3803   0.07163   0.06584  -0.0342   0.0080   1.0000
  17.000   1.3808   0.07474   0.06904  -0.0345   0.0077   1.0000
  17.250   1.3804   0.07804   0.07242  -0.0349   0.0074   1.0000
  17.500   1.3794   0.08147   0.07595  -0.0354   0.0071   1.0000
  17.750   1.3795   0.08483   0.07940  -0.0361   0.0071   1.0000
  18.000   1.3803   0.08811   0.08279  -0.0368   0.0069   1.0000
  18.250   1.3796   0.09168   0.08647  -0.0377   0.0068   1.0000
  18.500   1.3783   0.09538   0.09027  -0.0387   0.0066   1.0000
  18.750   1.3768   0.09917   0.09417  -0.0398   0.0065   1.0000
  19.000   1.3742   0.10317   0.09829  -0.0411   0.0063   1.0000
  19.250   1.3713   0.10728   0.10251  -0.0426   0.0063   1.0000
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