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FX 73-K-170/22 (fx73k170-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 73-K-170/22 (fx73k170-il)
Reynolds number: 200,000
Max Cl/Cd: 65.58 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73k170-il-200000-n5.txt
Download as CSV file: xf-fx73k170-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-K-170/22                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.1604   0.06478   0.05989  -0.1464   0.8198   0.0135
 -11.500  -0.1801   0.05826   0.05325  -0.1512   0.8175   0.0135
 -11.250  -0.1914   0.05407   0.04898  -0.1537   0.8146   0.0133
 -11.000  -0.2092   0.04967   0.04443  -0.1559   0.8113   0.0133
 -10.750  -0.2221   0.04619   0.04080  -0.1570   0.8083   0.0132
 -10.500  -0.2410   0.04250   0.03684  -0.1572   0.8055   0.0133
 -10.250  -0.2517   0.03984   0.03399  -0.1565   0.8026   0.0132
 -10.000  -0.2579   0.03797   0.03201  -0.1549   0.7991   0.0131
  -9.750  -0.2711   0.03597   0.02977  -0.1520   0.7956   0.0132
  -9.500  -0.2731   0.03409   0.02765  -0.1498   0.7926   0.0132
  -9.250  -0.2685   0.03228   0.02557  -0.1481   0.7903   0.0132
  -9.000  -0.2602   0.03044   0.02340  -0.1467   0.7884   0.0133
  -8.750  -0.2505   0.02894   0.02168  -0.1449   0.7852   0.0134
  -8.500  -0.2368   0.02763   0.02015  -0.1435   0.7822   0.0135
  -8.250  -0.2205   0.02632   0.01869  -0.1425   0.7796   0.0137
  -8.000  -0.2027   0.02513   0.01740  -0.1416   0.7774   0.0140
  -7.750  -0.1831   0.02419   0.01636  -0.1409   0.7754   0.0143
  -7.500  -0.1627   0.02333   0.01540  -0.1403   0.7737   0.0149
  -7.250  -0.1446   0.02257   0.01457  -0.1392   0.7712   0.0153
  -7.000  -0.1270   0.02189   0.01382  -0.1379   0.7681   0.0160
  -6.750  -0.1083   0.02120   0.01305  -0.1368   0.7652   0.0166
  -6.500  -0.0883   0.02055   0.01232  -0.1360   0.7627   0.0177
  -6.250  -0.0670   0.02000   0.01175  -0.1355   0.7607   0.0194
  -6.000  -0.0444   0.01946   0.01113  -0.1351   0.7590   0.0212
  -5.750  -0.0226   0.01894   0.01050  -0.1346   0.7571   0.0225
  -5.500  -0.0048   0.01845   0.01003  -0.1334   0.7536   0.0248
  -5.250   0.0166   0.01804   0.00954  -0.1326   0.7506   0.0283
  -5.000   0.0390   0.01756   0.00905  -0.1322   0.7480   0.0350
  -4.750   0.0624   0.01703   0.00856  -0.1319   0.7459   0.0511
  -4.500   0.0865   0.01648   0.00811  -0.1318   0.7442   0.0840
  -4.250   0.1099   0.01575   0.00767  -0.1318   0.7427   0.1549
  -4.000   0.1242   0.01498   0.00748  -0.1305   0.7388   0.2832
  -3.750   0.1408   0.01427   0.00741  -0.1292   0.7356   0.4330
  -3.500   0.1643   0.01422   0.00757  -0.1284   0.7330   0.5077
  -3.250   0.1910   0.01430   0.00763  -0.1281   0.7309   0.5471
  -3.000   0.2189   0.01443   0.00768  -0.1280   0.7293   0.5727
  -2.750   0.2475   0.01459   0.00773  -0.1280   0.7278   0.5951
  -2.500   0.2682   0.01488   0.00803  -0.1267   0.7240   0.6079
  -2.250   0.2920   0.01504   0.00814  -0.1260   0.7206   0.6177
  -2.000   0.3182   0.01512   0.00813  -0.1257   0.7181   0.6262
  -1.750   0.3455   0.01515   0.00808  -0.1257   0.7161   0.6323
  -1.500   0.3740   0.01515   0.00802  -0.1258   0.7144   0.6376
  -1.250   0.4036   0.01511   0.00784  -0.1263   0.7129   0.6439
  -1.000   0.4222   0.01532   0.00808  -0.1248   0.7084   0.6478
  -0.750   0.4460   0.01540   0.00814  -0.1242   0.7052   0.6516
  -0.500   0.4725   0.01540   0.00809  -0.1241   0.7027   0.6559
  -0.250   0.5007   0.01537   0.00796  -0.1244   0.7007   0.6605
   0.000   0.5298   0.01532   0.00786  -0.1248   0.6990   0.6634
   0.250   0.5530   0.01542   0.00797  -0.1241   0.6961   0.6665
   0.500   0.5728   0.01559   0.00816  -0.1229   0.6920   0.6699
   0.750   0.5977   0.01563   0.00817  -0.1226   0.6891   0.6734
   1.000   0.6252   0.01562   0.00810  -0.1228   0.6869   0.6768
   1.250   0.6543   0.01556   0.00803  -0.1231   0.6850   0.6792
   1.500   0.6829   0.01553   0.00798  -0.1235   0.6831   0.6818
   1.750   0.6971   0.01583   0.00836  -0.1212   0.6782   0.6847
   2.000   0.7202   0.01592   0.00845  -0.1206   0.6750   0.6878
   2.250   0.7474   0.01591   0.00842  -0.1207   0.6725   0.6911
   2.500   0.7772   0.01584   0.00834  -0.1213   0.6704   0.6938
   2.750   0.8028   0.01587   0.00839  -0.1211   0.6677   0.6961
   3.000   0.8157   0.01617   0.00877  -0.1186   0.6626   0.6991
   3.250   0.8399   0.01622   0.00884  -0.1181   0.6593   0.7022
   3.500   0.8687   0.01617   0.00879  -0.1185   0.6567   0.7055
   3.750   0.9009   0.01608   0.00868  -0.1195   0.6546   0.7083
   4.000   0.9095   0.01645   0.00916  -0.1163   0.6490   0.7110
   4.250   0.9304   0.01656   0.00932  -0.1152   0.6450   0.7139
   4.500   0.9588   0.01652   0.00933  -0.1155   0.6421   0.7173
   4.750   0.9923   0.01641   0.00922  -0.1167   0.6397   0.7205
   5.000   0.9947   0.01687   0.00976  -0.1124   0.6333   0.7239
   5.250   1.0157   0.01693   0.00990  -0.1114   0.6290   0.7268
   5.500   1.0474   0.01685   0.00987  -0.1122   0.6259   0.7303
   5.750   1.0607   0.01713   0.01022  -0.1099   0.6209   0.7342
   6.000   1.0736   0.01745   0.01062  -0.1076   0.6153   0.7381
   6.250   1.1028   0.01738   0.01061  -0.1080   0.6113   0.7414
   6.500   1.1149   0.01773   0.01106  -0.1055   0.6052   0.7452
   6.750   1.1303   0.01800   0.01140  -0.1037   0.5986   0.7499
   7.000   1.1661   0.01778   0.01122  -0.1051   0.5945   0.7546
   7.250   1.1635   0.01862   0.01220  -0.1007   0.5851   0.7595
   7.500   1.1975   0.01839   0.01201  -0.1018   0.5797   0.7644
   7.750   1.1983   0.01932   0.01306  -0.0984   0.5698   0.7705
   8.000   1.2217   0.01949   0.01331  -0.0981   0.5615   0.7760
   8.250   1.2386   0.01992   0.01383  -0.0970   0.5510   0.7831
   8.500   1.2501   0.02070   0.01472  -0.0954   0.5396   0.7911
   8.750   1.2653   0.02132   0.01543  -0.0944   0.5268   0.8012
   9.000   1.2820   0.02193   0.01612  -0.0936   0.5119   0.8131
   9.250   1.2989   0.02254   0.01676  -0.0929   0.4923   0.8284
   9.500   1.3139   0.02342   0.01766  -0.0922   0.4654   0.8526
   9.750   1.3306   0.02465   0.01885  -0.0930   0.4254   0.9882
  10.000   1.3269   0.02606   0.02012  -0.0891   0.4011   1.0000
  10.250   1.3265   0.02780   0.02171  -0.0866   0.3720   1.0000
  10.500   1.3253   0.02967   0.02345  -0.0842   0.3442   1.0000
  10.750   1.3250   0.03158   0.02525  -0.0820   0.3201   1.0000
  11.000   1.3216   0.03381   0.02735  -0.0797   0.2921   1.0000
  11.250   1.3174   0.03622   0.02964  -0.0776   0.2635   1.0000
  11.500   1.3151   0.03860   0.03191  -0.0757   0.2375   1.0000
  11.750   1.3120   0.04113   0.03432  -0.0739   0.2116   1.0000
  12.000   1.3093   0.04373   0.03680  -0.0723   0.1867   1.0000
  12.250   1.3063   0.04642   0.03938  -0.0708   0.1616   1.0000
  12.500   1.3033   0.04918   0.04201  -0.0694   0.1374   1.0000
  12.750   1.3023   0.05182   0.04457  -0.0682   0.1175   1.0000
  13.000   1.3016   0.05451   0.04717  -0.0671   0.0978   1.0000
  13.250   1.3013   0.05719   0.04979  -0.0662   0.0821   1.0000
  13.500   1.3008   0.05995   0.05250  -0.0652   0.0687   1.0000
  13.750   1.3019   0.06260   0.05513  -0.0645   0.0578   1.0000
  14.000   1.3042   0.06517   0.05774  -0.0639   0.0505   1.0000
  14.250   1.3053   0.06792   0.06049  -0.0633   0.0441   1.0000
  14.500   1.3070   0.07064   0.06324  -0.0628   0.0388   1.0000
  14.750   1.3083   0.07345   0.06611  -0.0624   0.0355   1.0000
  15.000   1.3112   0.07611   0.06886  -0.0621   0.0322   1.0000
  15.250   1.3111   0.07918   0.07196  -0.0618   0.0295   1.0000
  15.500   1.3136   0.08198   0.07486  -0.0616   0.0270   1.0000
  15.750   1.3157   0.08483   0.07779  -0.0616   0.0246   1.0000
  16.000   1.3143   0.08815   0.08116  -0.0615   0.0227   1.0000
  16.250   1.3149   0.09127   0.08442  -0.0616   0.0213   1.0000
  16.500   1.3160   0.09437   0.08762  -0.0617   0.0198   1.0000
  16.750   1.3159   0.09765   0.09100  -0.0620   0.0184   1.0000
  17.000   1.3124   0.10144   0.09484  -0.0624   0.0173   1.0000
  17.250   1.3117   0.10490   0.09843  -0.0629   0.0165   1.0000
  17.500   1.3114   0.10830   0.10196  -0.0633   0.0154   1.0000
  17.750   1.3107   0.11180   0.10557  -0.0640   0.0145   1.0000
  18.000   1.3096   0.11539   0.10927  -0.0648   0.0141   1.0000
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