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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 200,000
Max Cl/Cd: 76.48 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx83w160-il-200000.txt
Download as CSV file: xf-fx83w160-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6635   0.08760   0.08357  -0.0775   1.0000   0.0496
 -13.750  -0.7034   0.08007   0.07598  -0.0797   1.0000   0.0491
 -13.500  -0.7459   0.07343   0.06924  -0.0815   1.0000   0.0487
 -13.250  -0.7867   0.06793   0.06362  -0.0823   1.0000   0.0485
 -13.000  -0.8195   0.06228   0.05777  -0.0850   0.9987   0.0484
 -12.750  -0.8390   0.05574   0.05089  -0.0918   0.9940   0.0485
 -12.500  -0.8538   0.05090   0.04571  -0.0966   0.9877   0.0488
 -12.250  -0.8703   0.04759   0.04205  -0.0987   0.9794   0.0493
 -12.000  -0.8727   0.04450   0.03862  -0.0999   0.9730   0.0500
 -11.750  -0.8547   0.04263   0.03676  -0.1006   0.9688   0.0511
 -11.500  -0.8322   0.04108   0.03512  -0.1025   0.9657   0.0525
 -11.250  -0.8225   0.03960   0.03350  -0.1018   0.9596   0.0536
 -11.000  -0.8048   0.03771   0.03134  -0.1028   0.9550   0.0552
 -10.750  -0.7803   0.03572   0.02893  -0.1051   0.9521   0.0572
 -10.500  -0.7709   0.03449   0.02777  -0.1029   0.9456   0.0585
 -10.250  -0.7466   0.03348   0.02673  -0.1036   0.9420   0.0605
 -10.000  -0.7182   0.03223   0.02530  -0.1051   0.9395   0.0630
  -9.500  -0.6820   0.03008   0.02296  -0.1039   0.9297   0.0676
  -9.250  -0.6541   0.02932   0.02216  -0.1048   0.9266   0.0709
  -9.000  -0.6228   0.02848   0.02107  -0.1064   0.9244   0.0746
  -8.750  -0.5902   0.02730   0.02001  -0.1082   0.9230   0.0789
  -8.500  -0.5858   0.02701   0.01966  -0.1046   0.9149   0.0818
  -8.250  -0.5585   0.02617   0.01872  -0.1052   0.9115   0.0865
  -8.000  -0.5267   0.02549   0.01809  -0.1067   0.9093   0.0920
  -7.750  -0.4928   0.02474   0.01724  -0.1084   0.9078   0.0985
  -7.500  -0.4836   0.02450   0.01704  -0.1057   0.9014   0.1028
  -7.250  -0.4609   0.02423   0.01664  -0.1052   0.8969   0.1094
  -7.000  -0.4313   0.02347   0.01599  -0.1062   0.8943   0.1176
  -6.750  -0.3971   0.02281   0.01531  -0.1079   0.8925   0.1274
  -6.500  -0.3603   0.02237   0.01479  -0.1100   0.8912   0.1383
  -6.250  -0.3586   0.02228   0.01481  -0.1059   0.8833   0.1445
  -6.000  -0.3333   0.02196   0.01445  -0.1058   0.8797   0.1557
  -5.750  -0.3017   0.02148   0.01399  -0.1070   0.8775   0.1695
  -5.500  -0.2670   0.02089   0.01347  -0.1087   0.8758   0.1871
  -5.250  -0.2308   0.02022   0.01295  -0.1108   0.8746   0.2095
  -5.000  -0.2287   0.02044   0.01323  -0.1067   0.8664   0.2251
  -4.750  -0.2025   0.02002   0.01297  -0.1069   0.8628   0.2586
  -4.500  -0.1704   0.01946   0.01266  -0.1082   0.8606   0.3111
  -4.250  -0.1363   0.01899   0.01245  -0.1097   0.8591   0.3722
  -4.000  -0.0998   0.01874   0.01235  -0.1114   0.8579   0.4227
  -3.750  -0.0984   0.01939   0.01303  -0.1069   0.8493   0.4463
  -3.500  -0.0722   0.01954   0.01323  -0.1065   0.8457   0.4722
  -3.250  -0.0396   0.01963   0.01331  -0.1073   0.8436   0.4948
  -3.000  -0.0043   0.01970   0.01332  -0.1085   0.8421   0.5149
  -2.750   0.0325   0.01974   0.01332  -0.1099   0.8410   0.5323
  -2.500   0.0285   0.02072   0.01433  -0.1046   0.8319   0.5406
  -2.250   0.0558   0.02091   0.01447  -0.1044   0.8284   0.5543
  -2.000   0.0891   0.02093   0.01451  -0.1052   0.8264   0.5658
  -1.750   0.1243   0.02088   0.01445  -0.1063   0.8250   0.5765
  -1.500   0.1617   0.02081   0.01431  -0.1079   0.8240   0.5886
  -1.250   0.1517   0.02202   0.01559  -0.1017   0.8138   0.5939
  -1.000   0.1808   0.02212   0.01567  -0.1019   0.8107   0.6049
  -0.750   0.2161   0.02198   0.01556  -0.1028   0.8089   0.6147
  -0.500   0.2552   0.02173   0.01528  -0.1046   0.8077   0.6267
  -0.250   0.2944   0.02143   0.01504  -0.1062   0.8068   0.6358
   0.000   0.2814   0.02283   0.01641  -0.0998   0.7952   0.6425
   0.250   0.3121   0.02277   0.01640  -0.1001   0.7929   0.6497
   0.500   0.3486   0.02254   0.01617  -0.1015   0.7914   0.6570
   0.750   0.3882   0.02217   0.01579  -0.1034   0.7904   0.6641
   1.000   0.4273   0.02183   0.01549  -0.1052   0.7895   0.6709
   1.250   0.4687   0.02152   0.01516  -0.1075   0.7887   0.6786
   1.500   0.5090   0.02118   0.01486  -0.1096   0.7872   0.6839
   1.750   0.4933   0.02231   0.01603  -0.1023   0.7743   0.6887
   2.000   0.5356   0.02185   0.01557  -0.1046   0.7733   0.6956
   2.250   0.5803   0.02128   0.01504  -0.1074   0.7723   0.7014
   2.500   0.6301   0.02063   0.01444  -0.1110   0.7715   0.7082
   2.750   0.6824   0.02002   0.01383  -0.1152   0.7701   0.7159
   3.000   0.6624   0.02089   0.01478  -0.1065   0.7574   0.7207
   3.250   0.7216   0.01981   0.01375  -0.1116   0.7563   0.7272
   3.500   0.8056   0.01793   0.01184  -0.1208   0.7542   0.7340
   3.750   0.8063   0.01809   0.01209  -0.1155   0.7430   0.7391
   4.000   0.8620   0.01713   0.01116  -0.1200   0.7388   0.7461
   4.250   0.8840   0.01701   0.01108  -0.1186   0.7310   0.7530
   4.500   0.9137   0.01668   0.01083  -0.1186   0.7240   0.7594
   4.750   0.9647   0.01607   0.01023  -0.1226   0.7193   0.7676
   5.000   0.9669   0.01622   0.01050  -0.1174   0.7086   0.7750
   5.250   1.0083   0.01567   0.00998  -0.1195   0.7007   0.7841
   5.500   1.0208   0.01554   0.00994  -0.1161   0.6891   0.7932
   5.750   1.0370   0.01538   0.00984  -0.1135   0.6778   0.8041
   6.000   1.0638   0.01504   0.00956  -0.1128   0.6662   0.8152
   6.250   1.0761   0.01489   0.00951  -0.1094   0.6527   0.8296
   6.500   1.0852   0.01486   0.00957  -0.1054   0.6370   0.8495
   6.750   1.0987   0.01475   0.00956  -0.1023   0.6193   0.8813
   7.000   1.1205   0.01465   0.00958  -0.1012   0.5959   1.0000
   7.250   1.1348   0.01488   0.00967  -0.0988   0.5653   1.0000
   7.500   1.1432   0.01532   0.00989  -0.0953   0.5245   1.0000
   7.750   1.1445   0.01607   0.01030  -0.0907   0.4733   1.0000
   8.000   1.1401   0.01716   0.01105  -0.0855   0.4223   1.0000
   8.250   1.1341   0.01847   0.01204  -0.0804   0.3759   1.0000
   8.500   1.1293   0.01987   0.01317  -0.0759   0.3339   1.0000
   8.750   1.1272   0.02130   0.01436  -0.0719   0.2976   1.0000
   9.000   1.1280   0.02271   0.01556  -0.0686   0.2680   1.0000
   9.250   1.1311   0.02408   0.01676  -0.0657   0.2439   1.0000
   9.750   1.1438   0.02666   0.01909  -0.0610   0.2091   1.0000
  10.000   1.1535   0.02781   0.02019  -0.0592   0.1951   1.0000
  10.250   1.1637   0.02897   0.02131  -0.0574   0.1827   1.0000
  10.500   1.1737   0.03019   0.02246  -0.0557   0.1724   1.0000
  10.750   1.1838   0.03140   0.02361  -0.0541   0.1625   1.0000
  11.000   1.1958   0.03252   0.02476  -0.0527   0.1533   1.0000
  11.250   1.2052   0.03387   0.02598  -0.0511   0.1449   1.0000
  11.500   1.2180   0.03494   0.02716  -0.0499   0.1370   1.0000
  11.750   1.2280   0.03631   0.02841  -0.0485   0.1299   1.0000
  12.000   1.2403   0.03745   0.02967  -0.0473   0.1232   1.0000
  12.250   1.2504   0.03885   0.03098  -0.0460   0.1171   1.0000
  12.500   1.2625   0.04008   0.03231  -0.0449   0.1114   1.0000
  12.750   1.2725   0.04148   0.03370  -0.0437   0.1060   1.0000
  13.000   1.2844   0.04286   0.03508  -0.0426   0.1011   1.0000
  13.250   1.2948   0.04425   0.03657  -0.0416   0.0963   1.0000
  13.500   1.3048   0.04574   0.03800  -0.0406   0.0921   1.0000
  13.750   1.3157   0.04723   0.03958  -0.0396   0.0881   1.0000
  14.000   1.3252   0.04878   0.04120  -0.0386   0.0842   1.0000
  14.250   1.3357   0.05033   0.04270  -0.0377   0.0808   1.0000
  14.500   1.3457   0.05199   0.04447  -0.0368   0.0775   1.0000
  14.750   1.3538   0.05373   0.04631  -0.0360   0.0744   1.0000
  15.000   1.3620   0.05548   0.04804  -0.0352   0.0715   1.0000
  15.250   1.3736   0.05716   0.04976  -0.0345   0.0687   1.0000
  15.500   1.3790   0.05925   0.05202  -0.0337   0.0663   1.0000
  15.750   1.3858   0.06122   0.05406  -0.0331   0.0640   1.0000
  16.000   1.3958   0.06295   0.05574  -0.0325   0.0618   1.0000
  16.250   1.4032   0.06510   0.05801  -0.0319   0.0597   1.0000
  16.500   1.4050   0.06770   0.06080  -0.0314   0.0579   1.0000
  16.750   1.4084   0.07014   0.06335  -0.0310   0.0562   1.0000
  17.000   1.4148   0.07229   0.06552  -0.0308   0.0546   1.0000
  17.250   1.4271   0.07405   0.06724  -0.0304   0.0527   1.0000
  17.500   1.4217   0.07756   0.07100  -0.0303   0.0516   1.0000
  17.750   1.4189   0.08092   0.07457  -0.0304   0.0505   1.0000
  18.000   1.4167   0.08424   0.07805  -0.0307   0.0492   1.0000
  18.250   1.4175   0.08721   0.08110  -0.0310   0.0480   1.0000
  18.500   1.4246   0.08937   0.08323  -0.0311   0.0467   1.0000
  18.750   1.4275   0.09235   0.08628  -0.0314   0.0456   1.0000
  19.000   1.4139   0.09741   0.09162  -0.0326   0.0450   1.0000
  19.250   1.4017   0.10248   0.09695  -0.0342   0.0443   1.0000
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