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FX 60-160 AIRFOIL (fx60160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 60-160 AIRFOIL (fx60160-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.83 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60160-il-1000000-n5.txt
Download as CSV file: xf-fx60160-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.9843   0.07526   0.07245  -0.0844   1.0000   0.0096
 -18.500  -1.0074   0.06838   0.06542  -0.0882   1.0000   0.0098
 -18.250  -1.0244   0.06275   0.05967  -0.0911   1.0000   0.0098
 -18.000  -1.0363   0.05815   0.05496  -0.0932   1.0000   0.0100
 -17.750  -1.0468   0.05399   0.05068  -0.0949   1.0000   0.0101
 -17.500  -1.0536   0.05054   0.04714  -0.0960   1.0000   0.0103
 -17.250  -1.0588   0.04751   0.04402  -0.0966   1.0000   0.0105
 -17.000  -1.0628   0.04483   0.04124  -0.0969   1.0000   0.0106
 -16.750  -1.0676   0.04234   0.03866  -0.0967   1.0000   0.0108
 -16.500  -1.0712   0.04018   0.03642  -0.0961   1.0000   0.0109
 -16.250  -1.0725   0.03803   0.03420  -0.0959   0.9998   0.0111
 -16.000  -1.0603   0.03592   0.03202  -0.0979   0.9990   0.0115
 -15.750  -1.0453   0.03413   0.03018  -0.0997   0.9977   0.0120
 -15.500  -1.0302   0.03244   0.02844  -0.1013   0.9958   0.0123
 -15.250  -1.0156   0.03092   0.02685  -0.1025   0.9929   0.0127
 -15.000  -1.0006   0.02944   0.02529  -0.1036   0.9902   0.0130
 -14.750  -0.9824   0.02814   0.02392  -0.1049   0.9877   0.0135
 -14.500  -0.9635   0.02686   0.02255  -0.1063   0.9855   0.0137
 -14.250  -0.9431   0.02561   0.02123  -0.1079   0.9838   0.0140
 -14.000  -0.9264   0.02451   0.02010  -0.1086   0.9803   0.0145
 -13.750  -0.9061   0.02353   0.01909  -0.1095   0.9771   0.0149
 -13.500  -0.8816   0.02265   0.01817  -0.1111   0.9747   0.0155
 -13.250  -0.8547   0.02171   0.01718  -0.1132   0.9728   0.0158
 -13.000  -0.8289   0.02091   0.01632  -0.1148   0.9697   0.0164
 -12.750  -0.8026   0.02011   0.01545  -0.1165   0.9661   0.0168
 -12.500  -0.7738   0.01934   0.01462  -0.1186   0.9628   0.0171
 -12.250  -0.7430   0.01852   0.01373  -0.1211   0.9594   0.0174
 -12.000  -0.7233   0.01767   0.01284  -0.1217   0.9520   0.0181
 -11.750  -0.6977   0.01700   0.01212  -0.1230   0.9454   0.0185
 -11.500  -0.6826   0.01647   0.01154  -0.1220   0.9357   0.0189
 -11.250  -0.6637   0.01603   0.01104  -0.1213   0.9264   0.0193
 -11.000  -0.6438   0.01561   0.01055  -0.1207   0.9142   0.0198
 -10.750  -0.6245   0.01520   0.01006  -0.1198   0.8982   0.0202
 -10.500  -0.6039   0.01489   0.00964  -0.1191   0.8781   0.0207
 -10.250  -0.5844   0.01461   0.00922  -0.1180   0.8562   0.0211
 -10.000  -0.5649   0.01435   0.00884  -0.1170   0.8371   0.0213
  -9.750  -0.5457   0.01404   0.00842  -0.1159   0.8214   0.0217
  -9.500  -0.5272   0.01363   0.00791  -0.1147   0.8087   0.0223
  -9.250  -0.5058   0.01331   0.00755  -0.1140   0.7987   0.0229
  -9.000  -0.4837   0.01304   0.00721  -0.1134   0.7900   0.0234
  -8.750  -0.4608   0.01277   0.00689  -0.1129   0.7813   0.0239
  -8.500  -0.4376   0.01251   0.00658  -0.1124   0.7741   0.0244
  -8.250  -0.4138   0.01225   0.00627  -0.1120   0.7673   0.0249
  -8.000  -0.3900   0.01202   0.00596  -0.1116   0.7609   0.0253
  -7.750  -0.3653   0.01176   0.00566  -0.1113   0.7551   0.0258
  -7.500  -0.3405   0.01155   0.00540  -0.1110   0.7490   0.0263
  -7.250  -0.3153   0.01137   0.00516  -0.1108   0.7439   0.0266
  -7.000  -0.2908   0.01103   0.00479  -0.1105   0.7391   0.0277
  -6.750  -0.2656   0.01080   0.00452  -0.1103   0.7339   0.0285
  -6.250  -0.2138   0.01041   0.00409  -0.1101   0.7248   0.0302
  -6.000  -0.1875   0.01024   0.00389  -0.1100   0.7203   0.0310
  -5.750  -0.1612   0.01009   0.00369  -0.1099   0.7158   0.0319
  -5.500  -0.1346   0.00995   0.00352  -0.1099   0.7117   0.0327
  -5.250  -0.1079   0.00977   0.00332  -0.1099   0.7077   0.0340
  -5.000  -0.0812   0.00960   0.00314  -0.1098   0.7035   0.0357
  -4.750  -0.0546   0.00947   0.00300  -0.1098   0.6992   0.0374
  -4.500  -0.0275   0.00935   0.00285  -0.1098   0.6954   0.0390
  -4.250  -0.0001   0.00924   0.00273  -0.1099   0.6915   0.0404
  -4.000   0.0270   0.00911   0.00258  -0.1099   0.6871   0.0427
  -3.750   0.0539   0.00900   0.00246  -0.1099   0.6828   0.0459
  -3.500   0.0812   0.00890   0.00236  -0.1099   0.6787   0.0488
  -3.250   0.1088   0.00881   0.00226  -0.1100   0.6741   0.0506
  -3.000   0.1359   0.00871   0.00215  -0.1100   0.6693   0.0557
  -2.750   0.1629   0.00863   0.00206  -0.1100   0.6649   0.0604
  -2.500   0.1905   0.00851   0.00197  -0.1101   0.6606   0.0699
  -2.250   0.2164   0.00819   0.00184  -0.1101   0.6560   0.1327
  -2.000   0.2418   0.00785   0.00168  -0.1099   0.6516   0.1992
  -1.750   0.2662   0.00729   0.00152  -0.1098   0.6475   0.3275
  -1.500   0.2918   0.00690   0.00140  -0.1098   0.6430   0.4126
  -1.250   0.3179   0.00668   0.00135  -0.1097   0.6381   0.4770
  -1.000   0.3448   0.00659   0.00134  -0.1096   0.6338   0.5110
  -0.750   0.3724   0.00653   0.00135  -0.1097   0.6290   0.5386
  -0.500   0.3999   0.00652   0.00137  -0.1097   0.6238   0.5581
  -0.250   0.4271   0.00654   0.00139  -0.1096   0.6189   0.5709
   0.000   0.4551   0.00655   0.00142  -0.1097   0.6140   0.5842
   0.250   0.4828   0.00657   0.00146  -0.1098   0.6088   0.5929
   0.750   0.5378   0.00666   0.00155  -0.1097   0.5984   0.6131
   1.000   0.5653   0.00672   0.00159  -0.1097   0.5923   0.6180
   1.250   0.5923   0.00678   0.00164  -0.1097   0.5868   0.6220
   1.500   0.6200   0.00683   0.00169  -0.1097   0.5813   0.6259
   1.750   0.6469   0.00690   0.00175  -0.1096   0.5748   0.6300
   2.000   0.6736   0.00698   0.00180  -0.1094   0.5653   0.6335
   2.250   0.6993   0.00709   0.00187  -0.1091   0.5541   0.6366
   2.500   0.7246   0.00720   0.00196  -0.1087   0.5421   0.6399
   2.750   0.7497   0.00733   0.00205  -0.1082   0.5274   0.6435
   3.000   0.7733   0.00752   0.00215  -0.1074   0.5060   0.6465
   3.250   0.7957   0.00777   0.00229  -0.1065   0.4817   0.6493
   3.500   0.8185   0.00799   0.00243  -0.1056   0.4612   0.6522
   3.750   0.8411   0.00821   0.00258  -0.1047   0.4410   0.6548
   4.000   0.8627   0.00848   0.00277  -0.1036   0.4194   0.6573
   4.250   0.8840   0.00875   0.00295  -0.1025   0.3971   0.6596
   4.500   0.9030   0.00911   0.00318  -0.1009   0.3685   0.6620
   4.750   0.9183   0.00960   0.00347  -0.0987   0.3277   0.6642
   5.000   0.9278   0.01021   0.00382  -0.0954   0.2778   0.6661
   5.250   0.9287   0.01108   0.00435  -0.0905   0.2084   0.6682
   5.500   0.9326   0.01192   0.00492  -0.0862   0.1520   0.6704
   5.750   0.9326   0.01295   0.00563  -0.0814   0.0836   0.6726
   6.000   0.9497   0.01331   0.00596  -0.0797   0.0727   0.6748
   6.250   0.9675   0.01365   0.00629  -0.0780   0.0653   0.6769
   6.500   0.9849   0.01401   0.00663  -0.0764   0.0585   0.6790
   6.750   1.0028   0.01436   0.00696  -0.0749   0.0534   0.6809
   7.000   1.0200   0.01472   0.00732  -0.0733   0.0490   0.6829
   7.250   1.0372   0.01510   0.00770  -0.0717   0.0447   0.6849
   7.500   1.0544   0.01547   0.00809  -0.0702   0.0421   0.6871
   7.750   1.0707   0.01589   0.00851  -0.0685   0.0391   0.6894
   8.000   1.0873   0.01633   0.00895  -0.0669   0.0368   0.6915
   8.250   1.1041   0.01675   0.00939  -0.0655   0.0356   0.6937
   8.500   1.1205   0.01720   0.00987  -0.0640   0.0343   0.6958
   8.750   1.1363   0.01769   0.01038  -0.0624   0.0333   0.6976
   9.000   1.1515   0.01821   0.01093  -0.0608   0.0323   0.6997
   9.250   1.1660   0.01879   0.01153  -0.0592   0.0312   0.7019
   9.500   1.1800   0.01940   0.01218  -0.0575   0.0302   0.7043
   9.750   1.1945   0.02002   0.01284  -0.0560   0.0293   0.7066
  10.000   1.2093   0.02064   0.01349  -0.0546   0.0290   0.7088
  10.250   1.2241   0.02127   0.01416  -0.0533   0.0283   0.7110
  10.500   1.2382   0.02197   0.01490  -0.0519   0.0278   0.7132
  10.750   1.2517   0.02271   0.01569  -0.0505   0.0272   0.7157
  11.000   1.2649   0.02349   0.01651  -0.0491   0.0264   0.7182
  11.250   1.2774   0.02434   0.01740  -0.0478   0.0256   0.7208
  11.500   1.2891   0.02527   0.01836  -0.0464   0.0246   0.7234
  11.750   1.3002   0.02628   0.01940  -0.0450   0.0237   0.7261
  12.250   1.3254   0.02813   0.02137  -0.0428   0.0223   0.7320
  12.500   1.3373   0.02915   0.02244  -0.0417   0.0212   0.7354
  12.750   1.3479   0.03028   0.02359  -0.0406   0.0194   0.7387
  13.000   1.3582   0.03148   0.02482  -0.0395   0.0181   0.7420
  13.250   1.3640   0.03304   0.02635  -0.0382   0.0120   0.7454
  13.500   1.3683   0.03477   0.02811  -0.0368   0.0096   0.7495
  13.750   1.3724   0.03659   0.02999  -0.0356   0.0083   0.7542
  14.000   1.3768   0.03843   0.03189  -0.0345   0.0075   0.7591
  14.250   1.3836   0.04009   0.03363  -0.0336   0.0071   0.7649
  14.500   1.3907   0.04178   0.03540  -0.0328   0.0069   0.7714
  14.750   1.3968   0.04358   0.03729  -0.0320   0.0066   0.7786
  15.000   1.4018   0.04554   0.03934  -0.0313   0.0062   0.7880
  15.250   1.4071   0.04748   0.04137  -0.0306   0.0061   0.8005
  15.500   1.4113   0.04951   0.04353  -0.0299   0.0058   0.8222
  15.750   1.4305   0.05214   0.04653  -0.0331   0.0056   0.9325
  16.000   1.4397   0.05481   0.04928  -0.0343   0.0054   1.0000
  16.250   1.4436   0.05715   0.05169  -0.0340   0.0052   1.0000
  16.500   1.4471   0.05959   0.05420  -0.0338   0.0052   1.0000
  16.750   1.4509   0.06205   0.05673  -0.0337   0.0050   1.0000
  17.000   1.4544   0.06458   0.05933  -0.0336   0.0049   1.0000
  17.250   1.4566   0.06732   0.06214  -0.0337   0.0048   1.0000
  17.500   1.4588   0.07009   0.06499  -0.0339   0.0047   1.0000
  17.750   1.4604   0.07296   0.06793  -0.0341   0.0047   1.0000
  18.000   1.4615   0.07597   0.07102  -0.0344   0.0045   1.0000
  18.250   1.4615   0.07918   0.07431  -0.0349   0.0045   1.0000
  18.500   1.4618   0.08238   0.07759  -0.0354   0.0044   1.0000
  18.750   1.4613   0.08575   0.08104  -0.0361   0.0043   1.0000
  19.000   1.4593   0.08936   0.08474  -0.0369   0.0042   1.0000
  19.250   1.4572   0.09308   0.08854  -0.0378   0.0042   1.0000
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