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WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il)
Reynolds number: 50,000
Max Cl/Cd: 15.37 at α=12°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx3-il-50000-n5.txt
Download as CSV file: xf-fx3-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 3 AIRFOIL                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.5310   0.12256   0.11568  -0.0842   0.9516   0.0560
 -12.000  -0.5592   0.11638   0.10948  -0.0849   0.9530   0.0555
 -11.750  -0.5890   0.11068   0.10375  -0.0851   0.9545   0.0551
 -11.500  -0.6203   0.10571   0.09871  -0.0841   0.9562   0.0546
 -11.250  -0.6535   0.10168   0.09464  -0.0810   0.9576   0.0542
 -11.000  -0.6862   0.09785   0.09073  -0.0777   0.9589   0.0538
 -10.750  -0.7194   0.09457   0.08738  -0.0734   0.9614   0.0535
 -10.500  -0.7519   0.09149   0.08420  -0.0689   0.9643   0.0533
 -10.250  -0.7830   0.08858   0.08116  -0.0644   0.9662   0.0531
 -10.000  -0.8135   0.08598   0.07842  -0.0595   0.9678   0.0530
  -9.750  -0.8399   0.08325   0.07551  -0.0551   0.9710   0.0532
  -9.500  -0.8671   0.08056   0.07270  -0.0490   0.9757   0.0533
  -9.250  -0.8841   0.07745   0.06932  -0.0451   0.9780   0.0540
  -9.000  -0.8960   0.07423   0.06575  -0.0417   0.9804   0.0548
  -8.500  -0.9402   0.06878   0.05996  -0.0278   1.0001   0.0556
  -8.250  -0.9370   0.06528   0.05589  -0.0260   1.0001   0.0569
  -8.000  -0.9275   0.06249   0.05285  -0.0247   1.0001   0.0588
  -7.750  -0.9148   0.06064   0.05093  -0.0238   1.0001   0.0614
  -7.500  -0.9011   0.05867   0.04871  -0.0227   1.0001   0.0645
  -7.250  -0.8853   0.05652   0.04615  -0.0214   1.0001   0.0676
  -7.000  -0.8684   0.05460   0.04386  -0.0202   1.0001   0.0713
  -6.750  -0.8510   0.05323   0.04250  -0.0191   1.0001   0.0754
  -6.500  -0.8320   0.05202   0.04107  -0.0177   1.0001   0.0799
  -6.250  -0.8125   0.05106   0.03973  -0.0163   1.0001   0.0854
  -6.000  -0.7917   0.05037   0.03920  -0.0143   1.0001   0.0908
  -5.750  -0.7709   0.05003   0.03872  -0.0124   1.0001   0.0978
  -5.500  -0.7482   0.05007   0.03873  -0.0100   1.0001   0.1043
  -5.250  -0.7291   0.05002   0.03865  -0.0076   1.0001   0.1114
  -5.000  -0.7120   0.04992   0.03849  -0.0051   1.0001   0.1186
  -4.750  -0.6977   0.04962   0.03822  -0.0027   1.0001   0.1249
  -4.500  -0.6840   0.04925   0.03775  -0.0006   1.0001   0.1323
  -4.250  -0.6729   0.04857   0.03715   0.0013   1.0001   0.1416
  -4.000  -0.6611   0.04784   0.03648   0.0029   1.0001   0.1526
  -3.750  -0.6488   0.04700   0.03572   0.0042   1.0001   0.1672
  -3.500  -0.5685   0.05377   0.04539   0.0039   0.9654   0.5717
  -3.250  -0.5709   0.05263   0.04395   0.0033   0.9648   0.6439
  -3.000  -0.5487   0.05433   0.04530   0.0036   0.9605   0.6863
  -2.750  -0.5213   0.05678   0.04751   0.0066   0.9481   0.7147
  -2.250  -0.4740   0.05963   0.04994   0.0126   0.9328   0.7581
  -2.000  -0.4490   0.06095   0.05106   0.0147   0.9277   0.7840
  -1.750  -0.4221   0.06157   0.05151   0.0165   0.9194   0.8027
  -1.500  -0.3944   0.06183   0.05156   0.0163   0.9143   0.8128
  -1.250  -0.3777   0.06159   0.05114   0.0168   0.9065   0.8178
  -1.000  -0.3565   0.06135   0.05074   0.0169   0.9006   0.8208
  -0.750  -0.3281   0.06157   0.05076   0.0155   0.8957   0.8240
  -0.500  -0.3168   0.06104   0.05011   0.0171   0.8872   0.8273
  -0.250  -0.2957   0.06103   0.04994   0.0167   0.8817   0.8305
   0.000  -0.2790   0.06079   0.04958   0.0172   0.8741   0.8331
   0.250  -0.2569   0.06073   0.04940   0.0170   0.8681   0.8350
   0.500  -0.2298   0.06092   0.04946   0.0159   0.8623   0.8368
   0.750  -0.2152   0.06063   0.04909   0.0168   0.8547   0.8389
   1.000  -0.1870   0.06090   0.04925   0.0154   0.8499   0.8406
   1.250  -0.1730   0.06064   0.04893   0.0163   0.8416   0.8423
   1.500  -0.1471   0.06084   0.04904   0.0151   0.8362   0.8439
   1.750  -0.1284   0.06083   0.04896   0.0151   0.8289   0.8454
   2.000  -0.1043   0.06097   0.04905   0.0142   0.8228   0.8464
   2.250  -0.0786   0.06121   0.04923   0.0131   0.8171   0.8474
   2.500  -0.0602   0.06117   0.04917   0.0133   0.8097   0.8485
   2.750  -0.0284   0.06157   0.04952   0.0114   0.8054   0.8494
   3.000  -0.0146   0.06147   0.04942   0.0122   0.7970   0.8500
   3.250   0.0162   0.06181   0.04974   0.0103   0.7923   0.8508
   3.500   0.0318   0.06182   0.04976   0.0109   0.7843   0.8517
   3.750   0.0628   0.06215   0.05008   0.0090   0.7796   0.8524
   4.000   0.0789   0.06220   0.05016   0.0092   0.7715   0.8529
   4.250   0.1113   0.06253   0.05051   0.0072   0.7670   0.8535
   4.500   0.1272   0.06261   0.05063   0.0074   0.7586   0.8542
   4.750   0.1508   0.06282   0.05088   0.0066   0.7517   0.8547
   5.000   0.1787   0.06307   0.05118   0.0050   0.7455   0.8548
   5.250   0.1995   0.06329   0.05146   0.0044   0.7375   0.8550
   5.500   0.2325   0.06355   0.05179   0.0022   0.7324   0.8554
   5.750   0.2513   0.06380   0.05212   0.0019   0.7233   0.8558
   6.000   0.2784   0.06408   0.05248   0.0005   0.7165   0.8561
   6.250   0.3054   0.06435   0.05286  -0.0009   0.7090   0.8561
   6.500   0.3291   0.06470   0.05331  -0.0019   0.7007   0.8560
   6.750   0.3609   0.06491   0.05365  -0.0039   0.6941   0.8559
   7.000   0.3824   0.06533   0.05419  -0.0047   0.6847   0.8558
   7.250   0.4166   0.06544   0.05443  -0.0068   0.6786   0.8559
   7.500   0.4359   0.06593   0.05507  -0.0072   0.6680   0.8562
   7.750   0.4720   0.06586   0.05515  -0.0094   0.6622   0.8565
   8.000   0.4898   0.06642   0.05587  -0.0097   0.6505   0.8567
   8.250   0.5291   0.06610   0.05575  -0.0120   0.6452   0.8569
   8.500   0.5460   0.06674   0.05655  -0.0121   0.6324   0.8568
   8.750   0.5686   0.06716   0.05716  -0.0128   0.6212   0.8566
   9.000   0.6053   0.06674   0.05697  -0.0147   0.6140   0.8566
   9.250   0.6250   0.06724   0.05767  -0.0149   0.6008   0.8564
   9.500   0.6496   0.06733   0.05798  -0.0155   0.5881   0.8564
   9.750   0.6819   0.06657   0.05747  -0.0163   0.5757   0.8563
  10.000   0.7179   0.06505   0.05619  -0.0168   0.5617   0.8564
  10.250   0.7430   0.06424   0.05561  -0.0164   0.5429   0.8564
  10.500   0.7696   0.06327   0.05489  -0.0161   0.5236   0.8566
  10.750   0.7983   0.06219   0.05405  -0.0158   0.5034   0.8569
  11.000   0.8316   0.06071   0.05280  -0.0158   0.4822   0.8573
  11.250   0.8513   0.06081   0.05310  -0.0152   0.4538   0.8576
  11.500   0.8799   0.05994   0.05238  -0.0149   0.4196   0.8579
  11.750   0.9038   0.05959   0.05201  -0.0142   0.3747   0.8581
  12.000   0.9211   0.05992   0.05209  -0.0131   0.3204   0.8582
  12.250   0.9275   0.06154   0.05339  -0.0118   0.2699   0.8581
  12.500   0.9288   0.06391   0.05546  -0.0105   0.2276   0.8579
  12.750   0.9286   0.06657   0.05785  -0.0095   0.1939   0.8578
  13.000   0.9293   0.06932   0.06043  -0.0089   0.1660   0.8576
  13.250   0.9311   0.07205   0.06300  -0.0085   0.1445   0.8575
  13.500   0.9359   0.07459   0.06557  -0.0083   0.1262   0.8575
  13.750   0.9411   0.07711   0.06810  -0.0081   0.1108   0.8574
  14.000   0.9470   0.07961   0.07061  -0.0079   0.0976   0.8574
  14.250   0.9537   0.08202   0.07297  -0.0078   0.0871   0.8574
  14.500   0.9638   0.08417   0.07527  -0.0078   0.0772   0.8575
  14.750   0.9771   0.08598   0.07719  -0.0076   0.0699   0.8575
  15.000   0.9895   0.08790   0.07921  -0.0077   0.0640   0.8576
  15.250   1.0050   0.08959   0.08104  -0.0077   0.0591   0.8578
  15.500   1.0205   0.09147   0.08321  -0.0078   0.0552   0.8579
  15.750   1.0332   0.09348   0.08528  -0.0081   0.0523   0.8581
  16.000   1.0431   0.09613   0.08818  -0.0084   0.0497   0.8584
  16.250   1.0466   0.09962   0.09204  -0.0089   0.0475   0.8586
  16.500   1.0488   0.10321   0.09590  -0.0096   0.0459   0.8588
  16.750   1.0497   0.10701   0.09994  -0.0106   0.0448   0.8590
  17.000   1.0495   0.11092   0.10405  -0.0118   0.0438   0.8592
  17.250   1.0512   0.11455   0.10779  -0.0132   0.0428   0.8595
  17.500   1.0388   0.12053   0.11408  -0.0156   0.0423   0.8596
  17.750   1.0214   0.12763   0.12152  -0.0191   0.0421   0.8595
  18.000   1.0019   0.13558   0.12976  -0.0237   0.0421   0.8594
  18.250   0.9806   0.14457   0.13901  -0.0293   0.0422   0.8593
  18.500   0.9585   0.15470   0.14933  -0.0362   0.0424   0.8591
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