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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 500,000
Max Cl/Cd: 96.44 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx83w160-il-500000-n5.txt
Download as CSV file: xf-fx83w160-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 83-W-160                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.7400   0.12437   0.12099  -0.0670   1.0000   0.0187
 -18.750  -0.7570   0.11794   0.11448  -0.0699   1.0000   0.0189
 -18.500  -0.7743   0.11157   0.10802  -0.0728   1.0000   0.0191
 -18.250  -0.7911   0.10544   0.10180  -0.0755   1.0000   0.0193
 -18.000  -0.8084   0.09947   0.09574  -0.0780   1.0000   0.0194
 -17.750  -0.8245   0.09384   0.09003  -0.0803   1.0000   0.0195
 -17.500  -0.8417   0.08823   0.08433  -0.0825   1.0000   0.0196
 -17.250  -0.8582   0.08291   0.07891  -0.0845   1.0000   0.0198
 -17.000  -0.8730   0.07786   0.07376  -0.0864   1.0000   0.0200
 -16.750  -0.8776   0.07240   0.06816  -0.0908   0.9992   0.0202
 -16.500  -0.8825   0.06695   0.06261  -0.0953   0.9981   0.0205
 -16.250  -0.8850   0.06196   0.05753  -0.0995   0.9966   0.0208
 -16.000  -0.8864   0.05727   0.05274  -0.1036   0.9946   0.0209
 -15.750  -0.8858   0.05321   0.04859  -0.1071   0.9925   0.0212
 -15.500  -0.8828   0.04954   0.04484  -0.1104   0.9901   0.0216
 -15.250  -0.8773   0.04619   0.04140  -0.1137   0.9879   0.0219
 -15.000  -0.8687   0.04320   0.03830  -0.1169   0.9861   0.0224
 -14.750  -0.8636   0.04051   0.03553  -0.1188   0.9820   0.0227
 -14.500  -0.8528   0.03810   0.03302  -0.1213   0.9789   0.0232
 -14.000  -0.8298   0.03371   0.02844  -0.1255   0.9713   0.0239
 -13.750  -0.8180   0.03142   0.02610  -0.1279   0.9674   0.0246
 -13.500  -0.8003   0.02949   0.02412  -0.1306   0.9649   0.0253
 -13.250  -0.7878   0.02785   0.02241  -0.1318   0.9585   0.0259
 -13.000  -0.7668   0.02629   0.02078  -0.1342   0.9547   0.0267
 -12.750  -0.7412   0.02478   0.01917  -0.1374   0.9521   0.0275
 -12.500  -0.7239   0.02341   0.01773  -0.1389   0.9452   0.0282
 -12.250  -0.6974   0.02203   0.01630  -0.1421   0.9412   0.0293
 -12.000  -0.6662   0.02083   0.01503  -0.1457   0.9382   0.0305
 -11.750  -0.6468   0.01985   0.01397  -0.1467   0.9306   0.0317
 -11.500  -0.6222   0.01887   0.01290  -0.1486   0.9248   0.0328
 -11.250  -0.6039   0.01809   0.01207  -0.1488   0.9180   0.0341
 -11.000  -0.5827   0.01745   0.01137  -0.1490   0.9117   0.0355
 -10.750  -0.5558   0.01690   0.01073  -0.1500   0.9072   0.0372
 -10.500  -0.5388   0.01637   0.01015  -0.1490   0.9006   0.0384
 -10.250  -0.5171   0.01586   0.00960  -0.1488   0.8949   0.0403
 -10.000  -0.4910   0.01541   0.00907  -0.1493   0.8903   0.0425
  -9.750  -0.4727   0.01501   0.00864  -0.1482   0.8840   0.0443
  -9.500  -0.4505   0.01460   0.00821  -0.1478   0.8785   0.0469
  -9.250  -0.4249   0.01425   0.00779  -0.1480   0.8741   0.0495
  -9.000  -0.4037   0.01389   0.00742  -0.1472   0.8692   0.0523
  -8.750  -0.3810   0.01359   0.00708  -0.1467   0.8640   0.0557
  -8.500  -0.3563   0.01327   0.00673  -0.1466   0.8594   0.0591
  -8.250  -0.3309   0.01298   0.00641  -0.1465   0.8552   0.0632
  -8.000  -0.3083   0.01272   0.00613  -0.1458   0.8503   0.0670
  -7.750  -0.2841   0.01244   0.00584  -0.1455   0.8458   0.0717
  -7.500  -0.2581   0.01220   0.00555  -0.1454   0.8416   0.0762
  -7.250  -0.2328   0.01194   0.00529  -0.1453   0.8376   0.0818
  -7.000  -0.2088   0.01171   0.00506  -0.1448   0.8331   0.0875
  -6.750  -0.1837   0.01148   0.00483  -0.1445   0.8289   0.0947
  -6.500  -0.1575   0.01125   0.00460  -0.1445   0.8252   0.1022
  -6.250  -0.1301   0.01107   0.00439  -0.1446   0.8219   0.1093
  -6.000  -0.1058   0.01085   0.00420  -0.1441   0.8179   0.1175
  -5.750  -0.0802   0.01068   0.00402  -0.1439   0.8137   0.1249
  -5.500  -0.0540   0.01048   0.00383  -0.1437   0.8097   0.1346
  -5.250  -0.0269   0.01029   0.00365  -0.1438   0.8062   0.1461
  -5.000  -0.0006   0.01011   0.00349  -0.1437   0.8029   0.1577
  -4.750   0.0249   0.00992   0.00334  -0.1434   0.7992   0.1724
  -4.500   0.0506   0.00969   0.00319  -0.1432   0.7954   0.1936
  -4.250   0.0771   0.00947   0.00303  -0.1431   0.7919   0.2191
  -4.000   0.1042   0.00925   0.00287  -0.1432   0.7885   0.2468
  -3.750   0.1298   0.00904   0.00276  -0.1430   0.7847   0.2771
  -3.500   0.1554   0.00885   0.00266  -0.1427   0.7804   0.3059
  -3.250   0.1819   0.00869   0.00256  -0.1425   0.7764   0.3329
  -3.000   0.2093   0.00857   0.00248  -0.1425   0.7729   0.3579
  -2.750   0.2368   0.00845   0.00243  -0.1426   0.7698   0.3863
  -2.500   0.2628   0.00834   0.00242  -0.1423   0.7664   0.4163
  -2.250   0.2894   0.00828   0.00243  -0.1421   0.7630   0.4400
  -2.000   0.3169   0.00825   0.00242  -0.1420   0.7596   0.4560
  -1.750   0.3449   0.00825   0.00242  -0.1420   0.7566   0.4696
  -1.500   0.3736   0.00826   0.00242  -0.1422   0.7538   0.4814
  -1.250   0.4003   0.00827   0.00246  -0.1419   0.7505   0.4919
  -1.000   0.4270   0.00828   0.00250  -0.1417   0.7468   0.5036
  -0.750   0.4543   0.00832   0.00254  -0.1415   0.7431   0.5151
  -0.500   0.4820   0.00835   0.00257  -0.1415   0.7396   0.5241
   0.000   0.5368   0.00843   0.00264  -0.1412   0.7326   0.5381
   0.250   0.5632   0.00845   0.00269  -0.1409   0.7288   0.5438
   0.500   0.5903   0.00848   0.00272  -0.1407   0.7250   0.5483
   1.000   0.6441   0.00855   0.00279  -0.1402   0.7164   0.5574
   1.250   0.6688   0.00858   0.00284  -0.1395   0.7102   0.5621
   1.500   0.6949   0.00862   0.00287  -0.1391   0.7045   0.5660
   1.750   0.7200   0.00867   0.00290  -0.1384   0.6983   0.5693
   2.000   0.7425   0.00870   0.00292  -0.1372   0.6878   0.5726
   2.250   0.7633   0.00874   0.00295  -0.1356   0.6749   0.5763
   2.500   0.7839   0.00881   0.00299  -0.1340   0.6614   0.5803
   2.750   0.8055   0.00890   0.00305  -0.1326   0.6505   0.5845
   3.000   0.8280   0.00897   0.00312  -0.1315   0.6407   0.5886
   3.250   0.8496   0.00904   0.00320  -0.1301   0.6324   0.5921
   3.500   0.8694   0.00911   0.00329  -0.1284   0.6215   0.5955
   3.750   0.8882   0.00921   0.00338  -0.1265   0.6090   0.5988
   4.000   0.9033   0.00938   0.00349  -0.1238   0.5897   0.6021
   4.250   0.9156   0.00963   0.00366  -0.1206   0.5664   0.6057
   4.500   0.9283   0.00992   0.00387  -0.1175   0.5421   0.6091
   4.750   0.9371   0.01032   0.00415  -0.1137   0.5105   0.6127
   5.000   0.9405   0.01089   0.00454  -0.1090   0.4706   0.6163
   5.250   0.9466   0.01147   0.00496  -0.1050   0.4340   0.6207
   5.500   0.9522   0.01212   0.00544  -0.1009   0.3983   0.6251
   5.750   0.9591   0.01276   0.00595  -0.0973   0.3633   0.6294
   6.000   0.9682   0.01337   0.00645  -0.0941   0.3345   0.6339
   6.250   0.9776   0.01402   0.00698  -0.0911   0.3045   0.6386
   6.500   0.9859   0.01474   0.00755  -0.0879   0.2756   0.6432
   6.750   0.9957   0.01542   0.00814  -0.0851   0.2466   0.6480
   7.000   1.0055   0.01614   0.00874  -0.0824   0.2215   0.6537
   7.250   1.0173   0.01680   0.00933  -0.0801   0.2006   0.6599
   7.500   1.0305   0.01741   0.00990  -0.0780   0.1851   0.6664
   7.750   1.0444   0.01800   0.01047  -0.0760   0.1725   0.6746
   8.000   1.0584   0.01859   0.01106  -0.0741   0.1618   0.6833
   8.250   1.0738   0.01913   0.01162  -0.0724   0.1529   0.6935
   8.500   1.0875   0.01976   0.01226  -0.0706   0.1444   0.7047
   8.750   1.1028   0.02032   0.01287  -0.0689   0.1364   0.7183
   9.250   1.1307   0.02155   0.01419  -0.0654   0.1217   0.7569
   9.500   1.1436   0.02218   0.01491  -0.0635   0.1144   0.7902
   9.750   1.1609   0.02270   0.01567  -0.0625   0.1072   0.8816
  10.000   1.1901   0.02347   0.01649  -0.0644   0.0994   1.0000
  10.250   1.2049   0.02425   0.01726  -0.0630   0.0938   1.0000
  10.500   1.2192   0.02507   0.01807  -0.0617   0.0887   1.0000
  10.750   1.2339   0.02589   0.01889  -0.0604   0.0840   1.0000
  11.000   1.2474   0.02679   0.01977  -0.0591   0.0794   1.0000
  11.250   1.2616   0.02765   0.02065  -0.0578   0.0755   1.0000
  11.500   1.2749   0.02860   0.02160  -0.0565   0.0716   1.0000
  11.750   1.2882   0.02957   0.02258  -0.0553   0.0682   1.0000
  12.000   1.3016   0.03054   0.02357  -0.0541   0.0644   1.0000
  12.250   1.3137   0.03162   0.02465  -0.0528   0.0612   1.0000
  12.500   1.3268   0.03264   0.02570  -0.0517   0.0585   1.0000
  12.750   1.3391   0.03374   0.02682  -0.0506   0.0552   1.0000
  13.000   1.3503   0.03495   0.02804  -0.0494   0.0524   1.0000
  13.250   1.3625   0.03610   0.02923  -0.0483   0.0503   1.0000
  13.500   1.3734   0.03737   0.03051  -0.0472   0.0476   1.0000
  13.750   1.3832   0.03874   0.03191  -0.0461   0.0456   1.0000
  14.000   1.3945   0.04002   0.03323  -0.0451   0.0437   1.0000
  14.250   1.4042   0.04146   0.03471  -0.0441   0.0418   1.0000
  14.500   1.4129   0.04300   0.03627  -0.0431   0.0401   1.0000
  14.750   1.4225   0.04450   0.03782  -0.0422   0.0384   1.0000
  15.000   1.4318   0.04605   0.03943  -0.0413   0.0366   1.0000
  15.250   1.4393   0.04778   0.04119  -0.0405   0.0350   1.0000
  15.500   1.4467   0.04955   0.04301  -0.0397   0.0338   1.0000
  15.750   1.4549   0.05129   0.04482  -0.0390   0.0325   1.0000
  16.000   1.4623   0.05313   0.04672  -0.0383   0.0313   1.0000
  16.250   1.4681   0.05517   0.04881  -0.0377   0.0301   1.0000
  16.500   1.4730   0.05734   0.05103  -0.0371   0.0292   1.0000
  16.750   1.4791   0.05942   0.05320  -0.0366   0.0283   1.0000
  17.000   1.4841   0.06165   0.05550  -0.0362   0.0274   1.0000
  17.250   1.4880   0.06405   0.05797  -0.0359   0.0266   1.0000
  17.500   1.4907   0.06663   0.06061  -0.0357   0.0257   1.0000
  17.750   1.4916   0.06950   0.06353  -0.0356   0.0250   1.0000
  18.000   1.4947   0.07215   0.06629  -0.0356   0.0243   1.0000
  18.250   1.4960   0.07505   0.06928  -0.0357   0.0237   1.0000
  18.500   1.4967   0.07808   0.07240  -0.0359   0.0231   1.0000
  18.750   1.4964   0.08132   0.07573  -0.0363   0.0226   1.0000
  19.000   1.4939   0.08493   0.07942  -0.0369   0.0220   1.0000
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