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FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 83-W-160 (fx83w160-il)
Reynolds number: 100,000
Max Cl/Cd: 42.76 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx83w160-il-100000-n5.txt
Download as CSV file: xf-fx83w160-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.6023   0.09266   0.08703  -0.0727   1.0000   0.0492
 -13.250  -0.6767   0.07882   0.07300  -0.0793   1.0000   0.0486
 -13.000  -0.7202   0.07105   0.06505  -0.0827   0.9993   0.0485
 -12.750  -0.7430   0.06313   0.05679  -0.0900   0.9947   0.0487
 -12.500  -0.7580   0.05723   0.05055  -0.0951   0.9890   0.0492
 -12.250  -0.7599   0.05334   0.04643  -0.0987   0.9839   0.0501
 -12.000  -0.7492   0.05129   0.04436  -0.1007   0.9788   0.0512
 -11.750  -0.7433   0.04890   0.04185  -0.1029   0.9733   0.0525
 -11.500  -0.7401   0.04645   0.03921  -0.1045   0.9669   0.0536
 -11.250  -0.7413   0.04430   0.03684  -0.1046   0.9594   0.0549
 -11.000  -0.7340   0.04197   0.03415  -0.1056   0.9537   0.0566
 -10.750  -0.7220   0.04050   0.03261  -0.1054   0.9481   0.0580
 -10.500  -0.7075   0.03927   0.03135  -0.1054   0.9424   0.0597
 -10.250  -0.6864   0.03778   0.02969  -0.1066   0.9388   0.0623
 -10.000  -0.6778   0.03649   0.02814  -0.1052   0.9322   0.0648
  -9.750  -0.6603   0.03540   0.02705  -0.1050   0.9276   0.0670
  -9.500  -0.6365   0.03430   0.02588  -0.1059   0.9244   0.0700
  -9.250  -0.6174   0.03327   0.02465  -0.1057   0.9201   0.0735
  -9.000  -0.6044   0.03244   0.02378  -0.1043   0.9138   0.0764
  -8.750  -0.5807   0.03157   0.02287  -0.1048   0.9102   0.0805
  -8.500  -0.5535   0.03064   0.02177  -0.1058   0.9078   0.0856
  -8.250  -0.5396   0.03003   0.02119  -0.1043   0.9023   0.0893
  -8.000  -0.5209   0.02940   0.02046  -0.1035   0.8971   0.0945
  -7.750  -0.4952   0.02863   0.01966  -0.1040   0.8939   0.1002
  -7.500  -0.4659   0.02793   0.01887  -0.1051   0.8916   0.1076
  -7.250  -0.4462   0.02737   0.01831  -0.1044   0.8875   0.1136
  -7.000  -0.4316   0.02698   0.01787  -0.1027   0.8813   0.1199
  -6.750  -0.4058   0.02637   0.01725  -0.1030   0.8780   0.1280
  -6.500  -0.3759   0.02582   0.01661  -0.1039   0.8756   0.1379
  -6.250  -0.3451   0.02518   0.01601  -0.1052   0.8738   0.1488
  -6.000  -0.3368   0.02505   0.01588  -0.1022   0.8668   0.1571
  -5.750  -0.3131   0.02468   0.01547  -0.1020   0.8628   0.1700
  -5.500  -0.2846   0.02416   0.01499  -0.1027   0.8601   0.1862
  -5.250  -0.2536   0.02359   0.01450  -0.1039   0.8581   0.2063
  -5.000  -0.2212   0.02302   0.01402  -0.1053   0.8565   0.2318
  -4.750  -0.2164   0.02311   0.01419  -0.1018   0.8484   0.2506
  -4.500  -0.1907   0.02276   0.01395  -0.1020   0.8451   0.2835
  -4.250  -0.1610   0.02238   0.01371  -0.1027   0.8427   0.3243
  -4.000  -0.1292   0.02207   0.01355  -0.1036   0.8408   0.3666
  -3.750  -0.0961   0.02189   0.01348  -0.1046   0.8394   0.4081
  -3.500  -0.0926   0.02241   0.01405  -0.1006   0.8304   0.4306
  -3.250  -0.0648   0.02249   0.01415  -0.1005   0.8273   0.4587
  -3.000  -0.0335   0.02252   0.01412  -0.1011   0.8250   0.4829
  -2.750  -0.0008   0.02255   0.01412  -0.1018   0.8233   0.5020
  -2.500   0.0118   0.02304   0.01453  -0.0994   0.8167   0.5170
  -2.250   0.0337   0.02330   0.01477  -0.0984   0.8120   0.5305
  -2.000   0.0623   0.02341   0.01485  -0.0984   0.8093   0.5443
  -1.750   0.0930   0.02347   0.01486  -0.0988   0.8074   0.5580
  -1.500   0.1254   0.02348   0.01482  -0.0995   0.8058   0.5722
  -1.250   0.1298   0.02426   0.01563  -0.0957   0.7975   0.5811
  -1.000   0.1550   0.02441   0.01576  -0.0952   0.7937   0.5927
  -0.750   0.1847   0.02444   0.01577  -0.0955   0.7913   0.6037
  -0.500   0.2159   0.02441   0.01572  -0.0959   0.7895   0.6123
  -0.250   0.2490   0.02432   0.01560  -0.0968   0.7882   0.6207
   0.250   0.2776   0.02525   0.01655  -0.0927   0.7751   0.6343
   0.500   0.3111   0.02511   0.01636  -0.0937   0.7730   0.6428
   0.750   0.3455   0.02487   0.01614  -0.0946   0.7714   0.6486
   1.250   0.3753   0.02591   0.01717  -0.0911   0.7582   0.6616
   1.500   0.4063   0.02578   0.01710  -0.0914   0.7561   0.6674
   1.750   0.4404   0.02558   0.01692  -0.0923   0.7544   0.6748
   2.250   0.4705   0.02655   0.01797  -0.0887   0.7407   0.6874
   2.500   0.5057   0.02623   0.01767  -0.0896   0.7385   0.6942
   2.750   0.5429   0.02585   0.01733  -0.0909   0.7369   0.7003
   3.250   0.5753   0.02669   0.01827  -0.0875   0.7223   0.7132
   3.500   0.6141   0.02614   0.01778  -0.0889   0.7203   0.7199
   4.000   0.6536   0.02658   0.01834  -0.0864   0.7054   0.7347
   4.250   0.6950   0.02578   0.01763  -0.0878   0.7031   0.7423
   4.750   0.7491   0.02505   0.01706  -0.0865   0.6866   0.7599
   5.000   0.7615   0.02526   0.01734  -0.0839   0.6736   0.7699
   5.250   0.8106   0.02383   0.01599  -0.0861   0.6684   0.7798
   5.500   0.8168   0.02434   0.01662  -0.0826   0.6546   0.7925
   5.750   0.8324   0.02448   0.01688  -0.0805   0.6424   0.8078
   6.000   0.8699   0.02357   0.01608  -0.0811   0.6339   0.8267
   6.250   0.8815   0.02383   0.01651  -0.0784   0.6190   0.8549
   6.500   0.9007   0.02375   0.01664  -0.0771   0.6033   0.9535
   6.750   0.9200   0.02389   0.01679  -0.0758   0.5869   1.0000
   7.000   0.9449   0.02382   0.01670  -0.0752   0.5675   1.0000
   7.250   0.9655   0.02396   0.01681  -0.0740   0.5429   1.0000
   7.500   0.9902   0.02389   0.01663  -0.0732   0.5107   1.0000
   7.750   1.0169   0.02378   0.01626  -0.0724   0.4693   1.0000
   8.000   1.0338   0.02425   0.01647  -0.0707   0.4244   1.0000
   8.250   1.0441   0.02514   0.01706  -0.0683   0.3823   1.0000
   8.500   1.0513   0.02625   0.01792  -0.0658   0.3458   1.0000
   8.750   1.0583   0.02745   0.01892  -0.0634   0.3131   1.0000
   9.000   1.0654   0.02869   0.02000  -0.0611   0.2849   1.0000
   9.250   1.0730   0.02996   0.02111  -0.0590   0.2608   1.0000
   9.500   1.0816   0.03121   0.02224  -0.0571   0.2398   1.0000
   9.750   1.0908   0.03246   0.02339  -0.0554   0.2214   1.0000
  10.000   1.1005   0.03372   0.02456  -0.0537   0.2060   1.0000
  10.500   1.1222   0.03616   0.02693  -0.0509   0.1804   1.0000
  10.750   1.1334   0.03740   0.02815  -0.0495   0.1700   1.0000
  11.000   1.1434   0.03874   0.02944  -0.0482   0.1613   1.0000
  11.250   1.1559   0.03995   0.03070  -0.0470   0.1523   1.0000
  11.500   1.1651   0.04139   0.03208  -0.0457   0.1452   1.0000
  11.750   1.1781   0.04260   0.03339  -0.0447   0.1376   1.0000
  12.000   1.1872   0.04410   0.03485  -0.0435   0.1312   1.0000
  12.250   1.1991   0.04544   0.03629  -0.0425   0.1245   1.0000
  12.500   1.2086   0.04696   0.03783  -0.0414   0.1188   1.0000
  12.750   1.2184   0.04850   0.03940  -0.0404   0.1131   1.0000
  13.000   1.2282   0.05006   0.04105  -0.0395   0.1076   1.0000
  13.500   1.2456   0.05346   0.04456  -0.0377   0.0980   1.0000
  13.750   1.2533   0.05527   0.04643  -0.0369   0.0938   1.0000
  14.000   1.2601   0.05720   0.04836  -0.0361   0.0901   1.0000
  14.250   1.2685   0.05906   0.05038  -0.0354   0.0859   1.0000
  14.500   1.2748   0.06111   0.05250  -0.0348   0.0826   1.0000
  14.750   1.2800   0.06327   0.05463  -0.0342   0.0798   1.0000
  15.000   1.2868   0.06542   0.05701  -0.0336   0.0764   1.0000
  15.250   1.2920   0.06771   0.05940  -0.0332   0.0736   1.0000
  15.500   1.2957   0.07013   0.06187  -0.0329   0.0712   1.0000
  15.750   1.3002   0.07258   0.06438  -0.0326   0.0690   1.0000
  16.000   1.3034   0.07530   0.06731  -0.0324   0.0665   1.0000
  16.250   1.3054   0.07812   0.07026  -0.0323   0.0643   1.0000
  16.500   1.3068   0.08098   0.07320  -0.0324   0.0624   1.0000
  16.750   1.3097   0.08370   0.07592  -0.0325   0.0608   1.0000
  17.000   1.3077   0.08732   0.07982  -0.0329   0.0590   1.0000
  17.250   1.3055   0.09096   0.08366  -0.0335   0.0573   1.0000
  17.500   1.3030   0.09464   0.08748  -0.0343   0.0557   1.0000
  17.750   1.3016   0.09816   0.09110  -0.0351   0.0544   1.0000
  18.000   1.3022   0.10136   0.09431  -0.0360   0.0532   1.0000
  18.250   1.2939   0.10620   0.09938  -0.0376   0.0520   1.0000
  18.500   1.2827   0.11169   0.10514  -0.0398   0.0509   1.0000
  18.750   1.2711   0.11737   0.11105  -0.0423   0.0499   1.0000
  19.000   1.2584   0.12339   0.11728  -0.0453   0.0490   1.0000
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