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FX 60-160 AIRFOIL (fx60160-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 60-160 AIRFOIL (fx60160-il)
Reynolds number: 500,000
Max Cl/Cd: 96.91 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60160-il-500000.txt
Download as CSV file: xf-fx60160-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.5292   0.08378   0.08138  -0.0698   1.0000   0.0247
 -12.750  -0.5686   0.07431   0.07185  -0.0744   1.0000   0.0244
 -12.500  -0.5963   0.06851   0.06600  -0.0766   1.0000   0.0240
 -12.250  -0.6337   0.06150   0.05886  -0.0799   0.9995   0.0239
 -12.000  -0.6700   0.05099   0.04798  -0.0899   0.9951   0.0238
 -11.750  -0.7018   0.04242   0.03887  -0.0969   0.9878   0.0242
 -11.250  -0.6980   0.03420   0.02996  -0.1033   0.9742   0.0254
 -11.000  -0.6685   0.03319   0.02892  -0.1060   0.9717   0.0260
 -10.750  -0.6362   0.03234   0.02803  -0.1089   0.9700   0.0266
 -10.500  -0.6161   0.03121   0.02680  -0.1094   0.9636   0.0274
 -10.250  -0.5915   0.02909   0.02440  -0.1113   0.9598   0.0286
 -10.000  -0.5618   0.02732   0.02227  -0.1137   0.9574   0.0297
  -9.750  -0.5335   0.02436   0.01906  -0.1161   0.9554   0.0307
  -9.500  -0.5126   0.02366   0.01835  -0.1157   0.9471   0.0314
  -9.250  -0.4812   0.02292   0.01757  -0.1173   0.9428   0.0324
  -9.000  -0.4538   0.02206   0.01660  -0.1180   0.9369   0.0335
  -8.750  -0.4297   0.02101   0.01541  -0.1179   0.9283   0.0344
  -8.500  -0.4039   0.02011   0.01436  -0.1180   0.9202   0.0352
  -8.250  -0.3778   0.01965   0.01374  -0.1180   0.9108   0.0360
  -8.000  -0.3549   0.01788   0.01190  -0.1177   0.9001   0.0373
  -7.750  -0.3287   0.01717   0.01115  -0.1178   0.8904   0.0382
  -7.500  -0.3027   0.01659   0.01050  -0.1178   0.8800   0.0393
  -7.250  -0.2782   0.01605   0.00988  -0.1175   0.8686   0.0403
  -7.000  -0.2529   0.01562   0.00937  -0.1173   0.8583   0.0417
  -6.750  -0.2272   0.01523   0.00886  -0.1171   0.8490   0.0428
  -6.500  -0.2029   0.01489   0.00843  -0.1167   0.8395   0.0435
  -6.250  -0.1818   0.01393   0.00740  -0.1159   0.8313   0.0450
  -6.000  -0.1597   0.01343   0.00688  -0.1152   0.8228   0.0464
  -5.750  -0.1349   0.01311   0.00650  -0.1150   0.8160   0.0480
  -5.500  -0.1111   0.01282   0.00618  -0.1145   0.8088   0.0500
  -5.250  -0.0859   0.01254   0.00581  -0.1142   0.8026   0.0517
  -5.000  -0.0607   0.01232   0.00554  -0.1140   0.7964   0.0529
  -4.750  -0.0390   0.01168   0.00486  -0.1133   0.7903   0.0561
  -4.500  -0.0129   0.01143   0.00455  -0.1133   0.7851   0.0592
  -4.250   0.0123   0.01121   0.00430  -0.1130   0.7794   0.0625
  -4.000   0.0377   0.01091   0.00395  -0.1128   0.7741   0.0669
  -3.750   0.0643   0.01067   0.00367  -0.1128   0.7693   0.0733
  -3.500   0.0897   0.01040   0.00343  -0.1126   0.7641   0.0849
  -3.250   0.1095   0.00929   0.00297  -0.1121   0.7589   0.2557
  -3.000   0.1299   0.00827   0.00267  -0.1116   0.7542   0.4672
  -2.750   0.1552   0.00809   0.00271  -0.1112   0.7494   0.5372
  -2.500   0.1819   0.00808   0.00277  -0.1110   0.7442   0.5720
  -2.250   0.2099   0.00815   0.00280  -0.1110   0.7395   0.5914
  -2.000   0.2380   0.00826   0.00287  -0.1110   0.7350   0.6066
  -1.750   0.2652   0.00835   0.00297  -0.1108   0.7300   0.6191
  -1.500   0.2930   0.00844   0.00302  -0.1108   0.7253   0.6287
  -1.250   0.3218   0.00859   0.00310  -0.1110   0.7210   0.6375
  -1.000   0.3488   0.00867   0.00319  -0.1108   0.7163   0.6450
  -0.750   0.3764   0.00876   0.00328  -0.1107   0.7114   0.6517
  -0.500   0.4044   0.00888   0.00334  -0.1107   0.7070   0.6593
  -0.250   0.4321   0.00900   0.00348  -0.1106   0.7026   0.6653
   0.000   0.4593   0.00904   0.00351  -0.1105   0.6975   0.6699
   0.250   0.4872   0.00909   0.00350  -0.1106   0.6929   0.6738
   0.500   0.5157   0.00915   0.00354  -0.1107   0.6885   0.6770
   0.750   0.5421   0.00918   0.00362  -0.1105   0.6834   0.6809
   1.000   0.5693   0.00924   0.00367  -0.1104   0.6784   0.6854
   1.250   0.5978   0.00933   0.00369  -0.1106   0.6738   0.6897
   1.500   0.6242   0.00934   0.00375  -0.1103   0.6688   0.6929
   1.750   0.6509   0.00937   0.00382  -0.1101   0.6634   0.6963
   2.000   0.6786   0.00944   0.00386  -0.1102   0.6586   0.7000
   2.250   0.7055   0.00951   0.00393  -0.1101   0.6534   0.7039
   2.500   0.7319   0.00952   0.00396  -0.1099   0.6476   0.7069
   2.750   0.7591   0.00957   0.00399  -0.1098   0.6418   0.7093
   3.000   0.7838   0.00957   0.00405  -0.1092   0.6338   0.7120
   3.250   0.8098   0.00963   0.00407  -0.1089   0.6259   0.7150
   3.500   0.8340   0.00964   0.00412  -0.1082   0.6163   0.7182
   3.750   0.8580   0.00969   0.00414  -0.1075   0.6045   0.7211
   4.000   0.8815   0.00972   0.00416  -0.1066   0.5933   0.7235
   4.250   0.9052   0.00977   0.00424  -0.1059   0.5822   0.7260
   4.500   0.9287   0.00984   0.00434  -0.1051   0.5708   0.7289
   4.750   0.9514   0.00995   0.00443  -0.1041   0.5580   0.7319
   5.000   0.9735   0.01008   0.00454  -0.1031   0.5441   0.7347
   5.250   0.9933   0.01025   0.00465  -0.1016   0.5244   0.7374
   5.500   1.0106   0.01045   0.00479  -0.0996   0.5022   0.7401
   5.750   1.0274   0.01069   0.00498  -0.0975   0.4782   0.7428
   6.000   1.0414   0.01101   0.00521  -0.0949   0.4543   0.7456
   6.250   1.0537   0.01133   0.00544  -0.0920   0.4282   0.7487
   6.500   1.0632   0.01179   0.00577  -0.0887   0.3980   0.7518
   6.750   1.0689   0.01240   0.00620  -0.0847   0.3592   0.7546
   7.000   1.0672   0.01335   0.00687  -0.0796   0.2998   0.7574
   7.250   1.0509   0.01503   0.00799  -0.0725   0.2012   0.7607
   7.500   1.0317   0.01704   0.00943  -0.0655   0.1020   0.7643
   7.750   1.0351   0.01812   0.01038  -0.0621   0.0788   0.7675
   8.000   1.0438   0.01894   0.01121  -0.0595   0.0701   0.7705
   8.250   1.0561   0.01961   0.01194  -0.0575   0.0657   0.7736
   8.500   1.0653   0.02048   0.01283  -0.0551   0.0618   0.7773
   8.750   1.0738   0.02144   0.01384  -0.0528   0.0588   0.7810
   9.000   1.0866   0.02218   0.01465  -0.0512   0.0571   0.7843
   9.250   1.0980   0.02300   0.01555  -0.0494   0.0554   0.7880
   9.500   1.1087   0.02391   0.01652  -0.0476   0.0541   0.7922
   9.750   1.1185   0.02492   0.01759  -0.0459   0.0527   0.7967
  10.000   1.1250   0.02618   0.01889  -0.0439   0.0507   0.8010
  10.250   1.1257   0.02786   0.02066  -0.0415   0.0491   0.8058
  10.500   1.1385   0.02879   0.02167  -0.0404   0.0485   0.8114
  10.750   1.1500   0.02981   0.02278  -0.0392   0.0476   0.8176
  11.000   1.1613   0.03087   0.02394  -0.0380   0.0465   0.8254
  11.250   1.1720   0.03200   0.02517  -0.0369   0.0454   0.8349
  11.500   1.1817   0.03321   0.02650  -0.0357   0.0444   0.8498
  11.750   1.2010   0.03446   0.02795  -0.0366   0.0431   0.8947
  12.000   1.2171   0.03630   0.02988  -0.0379   0.0418   1.0000
  12.250   1.2185   0.03849   0.03210  -0.0366   0.0407   1.0000
  12.500   1.2299   0.03987   0.03354  -0.0360   0.0400   1.0000
  12.750   1.2424   0.04117   0.03491  -0.0355   0.0391   1.0000
  13.000   1.2534   0.04262   0.03642  -0.0350   0.0382   1.0000
  13.250   1.2637   0.04414   0.03800  -0.0345   0.0373   1.0000
  13.500   1.2742   0.04568   0.03958  -0.0341   0.0362   1.0000
  13.750   1.2838   0.04732   0.04125  -0.0337   0.0352   1.0000
  14.000   1.2889   0.04939   0.04334  -0.0331   0.0340   1.0000
  14.250   1.2946   0.05144   0.04545  -0.0326   0.0329   1.0000
  14.500   1.3070   0.05295   0.04705  -0.0326   0.0317   1.0000
  14.750   1.3180   0.05460   0.04877  -0.0326   0.0303   1.0000
  15.000   1.3282   0.05635   0.05055  -0.0326   0.0289   1.0000
  15.250   1.3313   0.05886   0.05307  -0.0324   0.0275   1.0000
  15.500   1.3426   0.06055   0.05487  -0.0325   0.0257   1.0000
  15.750   1.3539   0.06229   0.05665  -0.0327   0.0236   1.0000
  16.000   1.3597   0.06465   0.05904  -0.0328   0.0215   1.0000
  16.250   1.3680   0.06673   0.06119  -0.0329   0.0195   1.0000
  16.500   1.3709   0.06950   0.06396  -0.0332   0.0181   1.0000
  16.750   1.3746   0.07217   0.06673  -0.0333   0.0169   1.0000
  17.000   1.3786   0.07488   0.06950  -0.0337   0.0158   1.0000
  17.250   1.3798   0.07799   0.07266  -0.0341   0.0150   1.0000
  17.500   1.3779   0.08157   0.07629  -0.0347   0.0144   1.0000
  17.750   1.3791   0.08475   0.07958  -0.0353   0.0139   1.0000
  18.000   1.3782   0.08828   0.08321  -0.0360   0.0134   1.0000
  18.250   1.3788   0.09165   0.08666  -0.0369   0.0128   1.0000
  18.500   1.3770   0.09542   0.09052  -0.0379   0.0125   1.0000
  18.750   1.3744   0.09939   0.09455  -0.0391   0.0121   1.0000
  19.000   1.3685   0.10387   0.09911  -0.0405   0.0118   1.0000
  19.250   1.3629   0.10836   0.10369  -0.0421   0.0116   1.0000
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