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FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 60-177 AIRFOIL (fx60177-il)
Reynolds number: 500,000
Max Cl/Cd: 81.51 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60177-il-500000.txt
Download as CSV file: xf-fx60177-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 60-177 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6117   0.11354   0.11091  -0.0571   1.0001   0.0097
 -15.500  -0.6441   0.10335   0.10061  -0.0617   1.0001   0.0095
 -15.250  -0.6737   0.09468   0.09181  -0.0655   1.0001   0.0094
 -15.000  -0.6982   0.08609   0.08306  -0.0706   0.9997   0.0093
 -14.750  -0.7181   0.07756   0.07432  -0.0766   0.9985   0.0092
 -14.500  -0.7354   0.07015   0.06669  -0.0817   0.9971   0.0091
 -14.250  -0.7500   0.06363   0.05993  -0.0860   0.9957   0.0090
 -14.000  -0.7617   0.05794   0.05398  -0.0894   0.9944   0.0089
 -13.750  -0.7716   0.05320   0.04898  -0.0912   0.9923   0.0087
 -13.500  -0.7778   0.04900   0.04451  -0.0925   0.9898   0.0086
 -13.250  -0.7781   0.04537   0.04061  -0.0936   0.9877   0.0085
 -13.000  -0.7722   0.04239   0.03739  -0.0947   0.9861   0.0084
 -12.750  -0.7608   0.03997   0.03477  -0.0957   0.9849   0.0083
 -12.500  -0.7451   0.03791   0.03254  -0.0969   0.9840   0.0083
 -12.250  -0.7367   0.03628   0.03079  -0.0960   0.9800   0.0083
 -12.000  -0.7222   0.03469   0.02909  -0.0961   0.9773   0.0083
 -11.750  -0.7046   0.03320   0.02749  -0.0967   0.9754   0.0083
 -11.500  -0.6846   0.03180   0.02600  -0.0976   0.9739   0.0084
 -11.250  -0.6628   0.03046   0.02458  -0.0988   0.9727   0.0085
 -11.000  -0.6395   0.02918   0.02321  -0.1002   0.9718   0.0086
 -10.750  -0.6354   0.02825   0.02223  -0.0975   0.9652   0.0086
 -10.500  -0.6159   0.02712   0.02103  -0.0980   0.9628   0.0088
 -10.250  -0.5939   0.02599   0.01984  -0.0989   0.9611   0.0089
 -10.000  -0.5695   0.02488   0.01867  -0.1003   0.9597   0.0091
  -9.750  -0.5431   0.02381   0.01754  -0.1020   0.9587   0.0093
  -9.500  -0.5446   0.02325   0.01693  -0.0977   0.9503   0.0095
  -9.250  -0.5214   0.02235   0.01597  -0.0984   0.9480   0.0097
  -9.000  -0.4965   0.02129   0.01486  -0.0996   0.9464   0.0102
  -8.750  -0.4681   0.02037   0.01392  -0.1012   0.9452   0.0109
  -8.500  -0.4755   0.02007   0.01359  -0.0954   0.9358   0.0112
  -8.250  -0.4526   0.01937   0.01284  -0.0955   0.9334   0.0124
  -8.000  -0.4257   0.01847   0.01191  -0.0967   0.9319   0.0156
  -7.750  -0.3955   0.01758   0.01106  -0.0985   0.9308   0.0223
  -7.500  -0.4009   0.01732   0.01080  -0.0930   0.9215   0.0262
  -7.250  -0.3723   0.01671   0.01024  -0.0942   0.9196   0.0365
  -7.000  -0.3405   0.01609   0.00967  -0.0960   0.9183   0.0476
  -6.750  -0.3072   0.01542   0.00907  -0.0982   0.9172   0.0640
  -6.500  -0.2735   0.01457   0.00841  -0.1008   0.9161   0.1004
  -6.250  -0.2632   0.01412   0.00809  -0.0983   0.9091   0.1301
  -6.000  -0.2343   0.01334   0.00754  -0.0999   0.9064   0.1824
  -5.750  -0.1996   0.01229   0.00686  -0.1029   0.9047   0.2656
  -5.500  -0.1598   0.01116   0.00618  -0.1073   0.9037   0.3743
  -5.250  -0.1156   0.01016   0.00563  -0.1123   0.9029   0.4807
  -5.000  -0.0738   0.00968   0.00542  -0.1159   0.9022   0.5543
  -4.750  -0.0336   0.00950   0.00533  -0.1187   0.9012   0.5965
  -4.500  -0.0063   0.00954   0.00538  -0.1186   0.8968   0.6167
  -4.250   0.0242   0.00951   0.00531  -0.1192   0.8926   0.6308
  -4.000   0.0586   0.00949   0.00527  -0.1204   0.8900   0.6434
  -3.750   0.0942   0.00946   0.00523  -0.1218   0.8879   0.6521
  -3.500   0.1342   0.00939   0.00507  -0.1244   0.8860   0.6610
  -3.250   0.1555   0.00951   0.00523  -0.1228   0.8804   0.6661
  -3.000   0.1854   0.00954   0.00523  -0.1232   0.8761   0.6729
  -2.750   0.2216   0.00946   0.00509  -0.1249   0.8731   0.6784
  -2.500   0.2564   0.00943   0.00504  -0.1262   0.8704   0.6815
  -2.250   0.2775   0.00951   0.00513  -0.1247   0.8640   0.6854
  -2.000   0.3110   0.00944   0.00501  -0.1259   0.8596   0.6901
  -1.750   0.3474   0.00934   0.00484  -0.1277   0.8557   0.6939
  -1.500   0.3690   0.00940   0.00494  -0.1262   0.8487   0.6966
  -1.250   0.3988   0.00941   0.00493  -0.1265   0.8432   0.6996
  -1.000   0.4305   0.00939   0.00488  -0.1273   0.8378   0.7029
  -0.750   0.4584   0.00933   0.00479  -0.1274   0.8297   0.7069
  -0.500   0.4915   0.00928   0.00469  -0.1285   0.8237   0.7098
  -0.250   0.5130   0.00935   0.00479  -0.1270   0.8154   0.7120
   0.000   0.5437   0.00939   0.00480  -0.1275   0.8094   0.7144
   0.250   0.5675   0.00944   0.00488  -0.1266   0.8009   0.7171
   0.500   0.5996   0.00944   0.00482  -0.1276   0.7937   0.7203
   0.750   0.6277   0.00942   0.00478  -0.1279   0.7838   0.7240
   1.000   0.6535   0.00945   0.00479  -0.1274   0.7737   0.7259
   1.250   0.6789   0.00952   0.00485  -0.1268   0.7626   0.7278
   1.500   0.7019   0.00961   0.00494  -0.1257   0.7504   0.7300
   1.750   0.7261   0.00969   0.00500  -0.1249   0.7364   0.7325
   2.000   0.7511   0.00977   0.00502  -0.1244   0.7196   0.7353
   2.250   0.7773   0.00984   0.00501  -0.1243   0.7011   0.7384
   2.500   0.8015   0.00994   0.00503  -0.1237   0.6810   0.7408
   2.750   0.8212   0.01009   0.00514  -0.1220   0.6596   0.7424
   3.000   0.8396   0.01030   0.00527  -0.1200   0.6365   0.7441
   3.250   0.8566   0.01052   0.00541  -0.1179   0.6120   0.7460
   3.500   0.8730   0.01080   0.00558  -0.1157   0.5868   0.7483
   3.750   0.8903   0.01111   0.00577  -0.1137   0.5587   0.7511
   4.000   0.9094   0.01146   0.00599  -0.1123   0.5313   0.7542
   4.250   0.9292   0.01183   0.00623  -0.1111   0.5045   0.7565
   4.500   0.9465   0.01221   0.00652  -0.1093   0.4801   0.7581
   4.750   0.9643   0.01261   0.00684  -0.1075   0.4583   0.7598
   5.000   0.9832   0.01298   0.00716  -0.1061   0.4345   0.7617
   5.250   1.0000   0.01347   0.00753  -0.1043   0.4103   0.7637
   5.500   1.0196   0.01389   0.00787  -0.1032   0.3861   0.7658
   5.750   1.0391   0.01436   0.00823  -0.1021   0.3637   0.7681
   6.000   1.0599   0.01481   0.00859  -0.1013   0.3459   0.7705
   6.250   1.0814   0.01523   0.00895  -0.1007   0.3295   0.7724
   6.500   1.1002   0.01563   0.00932  -0.0993   0.3126   0.7740
   6.750   1.1179   0.01610   0.00975  -0.0979   0.2961   0.7757
   7.000   1.1354   0.01660   0.01020  -0.0964   0.2811   0.7775
   7.250   1.1539   0.01709   0.01065  -0.0952   0.2666   0.7795
   7.750   1.1926   0.01810   0.01158  -0.0932   0.2389   0.7837
   8.000   1.2124   0.01863   0.01208  -0.0925   0.2260   0.7859
   8.250   1.2329   0.01918   0.01259  -0.0919   0.2141   0.7880
   8.500   1.2496   0.01972   0.01312  -0.0905   0.2020   0.7896
   8.750   1.2658   0.02032   0.01369  -0.0890   0.1903   0.7913
   9.000   1.2827   0.02090   0.01427  -0.0877   0.1807   0.7932
   9.250   1.2988   0.02156   0.01493  -0.0863   0.1723   0.7952
   9.500   1.3165   0.02217   0.01555  -0.0852   0.1633   0.7974
   9.750   1.3340   0.02283   0.01621  -0.0842   0.1539   0.7996
  10.000   1.3504   0.02359   0.01694  -0.0832   0.1439   0.8016
  10.250   1.3671   0.02438   0.01769  -0.0823   0.1342   0.8036
  10.500   1.3815   0.02513   0.01845  -0.0808   0.1257   0.8053
  10.750   1.3936   0.02605   0.01935  -0.0792   0.1162   0.8070
  11.000   1.4075   0.02689   0.02020  -0.0778   0.1060   0.8087
  11.250   1.4202   0.02785   0.02115  -0.0764   0.0973   0.8105
  11.500   1.4316   0.02894   0.02221  -0.0749   0.0890   0.8124
  11.750   1.4436   0.03003   0.02330  -0.0736   0.0802   0.8144
  12.000   1.4552   0.03119   0.02444  -0.0723   0.0721   0.8164
  12.250   1.4646   0.03255   0.02577  -0.0709   0.0636   0.8183
  12.500   1.4738   0.03390   0.02713  -0.0696   0.0580   0.8199
  12.750   1.4831   0.03520   0.02846  -0.0681   0.0533   0.8215
  13.000   1.4913   0.03661   0.02991  -0.0667   0.0478   0.8231
  13.250   1.4985   0.03814   0.03147  -0.0652   0.0434   0.8249
  13.500   1.5028   0.03999   0.03331  -0.0637   0.0366   0.8269
  13.750   1.5083   0.04182   0.03516  -0.0625   0.0327   0.8290
  14.000   1.5130   0.04381   0.03718  -0.0613   0.0292   0.8310
  14.250   1.5177   0.04587   0.03929  -0.0604   0.0249   0.8328
  14.500   1.5210   0.04816   0.04160  -0.0595   0.0193   0.8345
  14.750   1.5086   0.05195   0.04536  -0.0579   0.0106   0.8359
  15.000   1.5029   0.05522   0.04871  -0.0568   0.0065   0.8373
  15.250   1.4968   0.05867   0.05225  -0.0561   0.0050   0.8388
  15.500   1.4944   0.06184   0.05553  -0.0556   0.0046   0.8403
  15.750   1.4918   0.06514   0.05894  -0.0554   0.0043   0.8420
  16.000   1.4885   0.06868   0.06260  -0.0555   0.0041   0.8437
  16.250   1.4853   0.07231   0.06635  -0.0557   0.0040   0.8454
  16.500   1.4812   0.07616   0.07033  -0.0562   0.0039   0.8472
  16.750   1.4754   0.08033   0.07464  -0.0569   0.0039   0.8488
  17.000   1.4684   0.08477   0.07921  -0.0578   0.0038   0.8503
  17.250   1.4601   0.08938   0.08397  -0.0588   0.0037   0.8518
  17.500   1.4511   0.09417   0.08890  -0.0600   0.0037   0.8532
  17.750   1.4415   0.09912   0.09400  -0.0615   0.0037   0.8546
  18.000   1.4300   0.10448   0.09950  -0.0632   0.0036   0.8560
  18.250   1.4169   0.11022   0.10540  -0.0653   0.0036   0.8573
  18.500   1.4046   0.11595   0.11127  -0.0676   0.0036   0.8588
  18.750   1.3916   0.12190   0.11736  -0.0702   0.0035   0.8603
  19.000   1.3782   0.12802   0.12363  -0.0731   0.0035   0.8618
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