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WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il)
Reynolds number: 100,000
Max Cl/Cd: 23.45 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx3-il-100000-n5.txt
Download as CSV file: xf-fx3-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.3202   0.09341   0.08726  -0.1596   0.8762   0.0306
 -14.500  -0.3508   0.08602   0.07976  -0.1632   0.8765   0.0305
 -14.250  -0.3797   0.08014   0.07371  -0.1652   0.8767   0.0303
 -14.000  -0.4076   0.07537   0.06875  -0.1658   0.8770   0.0303
 -13.750  -0.4340   0.07149   0.06466  -0.1651   0.8773   0.0304
 -13.500  -0.4594   0.06826   0.06120  -0.1634   0.8776   0.0306
 -13.250  -0.4789   0.06600   0.05878  -0.1610   0.8778   0.0309
 -13.000  -0.4933   0.06493   0.05766  -0.1577   0.8775   0.0312
 -12.750  -0.5086   0.06410   0.05678  -0.1538   0.8777   0.0316
 -12.500  -0.5264   0.06348   0.05611  -0.1492   0.8780   0.0319
 -12.250  -0.5470   0.06296   0.05553  -0.1438   0.8784   0.0322
 -12.000  -0.5687   0.06248   0.05498  -0.1380   0.8788   0.0325
 -11.750  -0.6047   0.06251   0.05499  -0.1288   0.8794   0.0324
 -11.500  -0.6245   0.06190   0.05429  -0.1230   0.8791   0.0327
 -11.250  -0.6649   0.06191   0.05429  -0.1127   0.8799   0.0325
 -11.000  -0.7000   0.06162   0.05397  -0.1036   0.8810   0.0324
 -10.750  -0.7225   0.06097   0.05325  -0.0969   0.8816   0.0327
 -10.500  -0.7372   0.06011   0.05229  -0.0917   0.8814   0.0332
 -10.250  -0.7601   0.05941   0.05151  -0.0848   0.8824   0.0335
 -10.000  -0.7736   0.05839   0.05036  -0.0795   0.8834   0.0342
  -9.750  -0.7761   0.05696   0.04870  -0.0761   0.8835   0.0353
  -9.500  -0.7698   0.05524   0.04667  -0.0736   0.8829   0.0367
  -9.250  -0.7652   0.05373   0.04478  -0.0705   0.8833   0.0384
  -9.000  -0.7616   0.05293   0.04402  -0.0677   0.8838   0.0397
  -8.750  -0.7578   0.05225   0.04330  -0.0650   0.8844   0.0411
  -8.500  -0.7458   0.05141   0.04233  -0.0634   0.8837   0.0434
  -8.250  -0.7276   0.05042   0.04107  -0.0620   0.8829   0.0464
  -8.000  -0.7146   0.04966   0.04028  -0.0602   0.8827   0.0488
  -7.750  -0.7048   0.04909   0.03970  -0.0582   0.8828   0.0514
  -7.500  -0.6902   0.04850   0.03896  -0.0566   0.8826   0.0550
  -7.250  -0.6689   0.04793   0.03827  -0.0558   0.8815   0.0589
  -7.000  -0.6463   0.04754   0.03790  -0.0557   0.8803   0.0632
  -6.500  -0.6175   0.04673   0.03689  -0.0520   0.8778   0.0713
  -6.250  -0.6131   0.04597   0.03621  -0.0485   0.8749   0.0745
  -6.000  -0.6005   0.04552   0.03573  -0.0467   0.8731   0.0790
  -5.750  -0.5843   0.04518   0.03529  -0.0453   0.8710   0.0837
  -5.500  -0.5663   0.04473   0.03487  -0.0441   0.8688   0.0883
  -5.250  -0.5453   0.04442   0.03455  -0.0438   0.8669   0.0939
  -5.000  -0.5211   0.04430   0.03434  -0.0438   0.8654   0.0996
  -4.750  -0.5048   0.04390   0.03394  -0.0426   0.8615   0.1045
  -4.500  -0.4929   0.04341   0.03346  -0.0407   0.8575   0.1113
  -4.250  -0.4736   0.04317   0.03325  -0.0400   0.8550   0.1216
  -4.000  -0.4500   0.04296   0.03315  -0.0401   0.8525   0.1406
  -3.750  -0.4232   0.04211   0.03300  -0.0419   0.8505   0.2436
  -3.250  -0.4188   0.04650   0.03945  -0.0240   0.8411   0.6065
  -2.750  -0.3396   0.04779   0.04017  -0.0338   0.8358   0.6804
  -2.500  -0.3103   0.04898   0.04121  -0.0333   0.8341   0.6932
  -2.250  -0.3131   0.04918   0.04141  -0.0268   0.8265   0.6985
  -2.000  -0.2906   0.04977   0.04188  -0.0256   0.8232   0.7094
  -1.750  -0.2645   0.05048   0.04248  -0.0249   0.8209   0.7219
  -1.500  -0.2563   0.05103   0.04300  -0.0196   0.8163   0.7290
  -1.250  -0.2406   0.05112   0.04301  -0.0179   0.8112   0.7387
  -1.000  -0.2193   0.05134   0.04316  -0.0162   0.8082   0.7437
  -0.750  -0.1885   0.05140   0.04309  -0.0178   0.8062   0.7476
  -0.500  -0.1691   0.05115   0.04274  -0.0185   0.8005   0.7511
  -0.250  -0.1458   0.05102   0.04253  -0.0188   0.7963   0.7533
   0.000  -0.1191   0.05100   0.04243  -0.0192   0.7937   0.7548
   0.250  -0.0876   0.05105   0.04240  -0.0206   0.7919   0.7562
   0.500  -0.0780   0.05084   0.04216  -0.0186   0.7846   0.7581
   0.750  -0.0497   0.05083   0.04209  -0.0197   0.7816   0.7600
   1.000  -0.0166   0.05087   0.04206  -0.0217   0.7796   0.7616
   1.250  -0.0009   0.05077   0.04193  -0.0212   0.7728   0.7631
   1.500   0.0300   0.05078   0.04189  -0.0232   0.7697   0.7647
   1.750   0.0660   0.05083   0.04189  -0.0260   0.7676   0.7663
   2.000   0.0850   0.05084   0.04189  -0.0264   0.7606   0.7676
   2.250   0.1173   0.05084   0.04186  -0.0285   0.7576   0.7684
   2.500   0.1492   0.05077   0.04177  -0.0298   0.7556   0.7692
   2.750   0.1611   0.05074   0.04178  -0.0283   0.7476   0.7702
   3.000   0.1928   0.05066   0.04170  -0.0298   0.7450   0.7710
   3.250   0.2109   0.05072   0.04178  -0.0295   0.7380   0.7716
   3.500   0.2414   0.05064   0.04171  -0.0309   0.7344   0.7722
   3.750   0.2754   0.05053   0.04162  -0.0328   0.7322   0.7731
   4.000   0.2907   0.05066   0.04180  -0.0321   0.7237   0.7739
   4.250   0.3246   0.05054   0.04171  -0.0340   0.7209   0.7745
   4.500   0.3440   0.05070   0.04192  -0.0341   0.7131   0.7750
   4.750   0.3748   0.05059   0.04187  -0.0355   0.7091   0.7757
   5.000   0.4101   0.05035   0.04169  -0.0375   0.7066   0.7764
   5.250   0.4267   0.05068   0.04209  -0.0373   0.6970   0.7766
   5.500   0.4611   0.05045   0.04192  -0.0393   0.6937   0.7767
   5.750   0.4818   0.05073   0.04229  -0.0395   0.6853   0.7770
   6.000   0.5125   0.05059   0.04224  -0.0409   0.6805   0.7776
   6.250   0.5485   0.05020   0.04195  -0.0429   0.6776   0.7781
   6.500   0.5664   0.05065   0.04250  -0.0429   0.6673   0.7782
   6.750   0.6015   0.05024   0.04220  -0.0447   0.6634   0.7782
   7.250   0.6569   0.05008   0.04229  -0.0466   0.6490   0.7782
   7.500   0.6946   0.04932   0.04167  -0.0485   0.6458   0.7782
   7.750   0.7141   0.04972   0.04220  -0.0484   0.6345   0.7782
   8.000   0.7512   0.04879   0.04143  -0.0500   0.6303   0.7784
   8.250   0.7779   0.04812   0.04088  -0.0500   0.6162   0.7788
   8.500   0.8104   0.04683   0.03970  -0.0504   0.5990   0.7792
   8.750   0.8426   0.04589   0.03885  -0.0510   0.5812   0.7794
   9.000   0.8733   0.04536   0.03844  -0.0517   0.5644   0.7793
   9.250   0.9015   0.04506   0.03826  -0.0522   0.5443   0.7793
   9.500   0.9331   0.04447   0.03774  -0.0529   0.5198   0.7793
   9.750   0.9668   0.04368   0.03693  -0.0538   0.4874   0.7793
  10.000   0.9977   0.04311   0.03622  -0.0542   0.4431   0.7793
  10.250   1.0169   0.04337   0.03616  -0.0533   0.3801   0.7792
  10.500   1.0227   0.04474   0.03710  -0.0513   0.3100   0.7791
  10.750   1.0230   0.04670   0.03862  -0.0490   0.2449   0.7790
  11.000   1.0244   0.04874   0.04028  -0.0471   0.1914   0.7789
  11.250   1.0301   0.05055   0.04185  -0.0457   0.1550   0.7788
  11.750   1.0485   0.05380   0.04495  -0.0439   0.1128   0.7787
  12.000   1.0584   0.05542   0.04656  -0.0432   0.0966   0.7787
  12.250   1.0675   0.05714   0.04831  -0.0424   0.0824   0.7788
  12.500   1.0756   0.05897   0.05014  -0.0416   0.0697   0.7790
  12.750   1.0828   0.06093   0.05210  -0.0407   0.0591   0.7792
  13.000   1.0893   0.06300   0.05419  -0.0399   0.0516   0.7793
  13.250   1.0974   0.06497   0.05626  -0.0392   0.0456   0.7794
  13.500   1.1033   0.06716   0.05847  -0.0385   0.0416   0.7794
  13.750   1.1110   0.06922   0.06067  -0.0379   0.0381   0.7793
  14.000   1.1171   0.07147   0.06300  -0.0374   0.0360   0.7793
  14.250   1.1222   0.07385   0.06547  -0.0369   0.0342   0.7792
  14.500   1.1301   0.07598   0.06777  -0.0365   0.0323   0.7791
  14.750   1.1374   0.07819   0.07011  -0.0362   0.0305   0.7791
  15.000   1.1436   0.08054   0.07256  -0.0360   0.0290   0.7791
  15.250   1.1488   0.08300   0.07510  -0.0358   0.0279   0.7791
  15.500   1.1552   0.08532   0.07747  -0.0354   0.0270   0.7790
  15.750   1.1642   0.08747   0.07984  -0.0352   0.0263   0.7790
  16.000   1.1719   0.08981   0.08239  -0.0351   0.0254   0.7791
  16.250   1.1778   0.09241   0.08521  -0.0351   0.0244   0.7791
  16.500   1.1820   0.09521   0.08820  -0.0354   0.0236   0.7791
  16.750   1.1847   0.09822   0.09138  -0.0358   0.0228   0.7791
  17.000   1.1867   0.10136   0.09467  -0.0363   0.0222   0.7791
  17.250   1.1882   0.10461   0.09807  -0.0370   0.0218   0.7791
  17.500   1.1889   0.10801   0.10162  -0.0378   0.0214   0.7791
  17.750   1.1884   0.11165   0.10543  -0.0387   0.0210   0.7791
  18.250   1.1783   0.12068   0.11490  -0.0418   0.0206   0.7790
  18.500   1.1678   0.12634   0.12085  -0.0445   0.0205   0.7789
  18.750   1.1551   0.13265   0.12745  -0.0478   0.0204   0.7788
  19.000   1.1404   0.13965   0.13473  -0.0520   0.0203   0.7787
  19.250   1.1237   0.14753   0.14287  -0.0571   0.0203   0.7786
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