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WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 76-100 (fx76100-il)
Reynolds number: 500,000
Max Cl/Cd: 61.35 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76100-il-500000-n5.txt
Download as CSV file: xf-fx76100-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 76-100                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.9325   0.14501   0.14229   0.0191   1.0000   0.0097
 -17.500  -0.9716   0.13157   0.12869   0.0122   1.0000   0.0097
 -17.250  -0.9999   0.12126   0.11825   0.0068   1.0000   0.0095
 -17.000  -1.0249   0.11195   0.10882   0.0019   1.0000   0.0096
 -16.750  -1.0538   0.10233   0.09906  -0.0032   1.0000   0.0094
 -16.500  -1.0778   0.09383   0.09046  -0.0078   1.0000   0.0096
 -16.250  -1.1067   0.08484   0.08131  -0.0126   1.0000   0.0095
 -16.000  -1.1292   0.07695   0.07327  -0.0169   1.0000   0.0093
 -15.750  -1.1543   0.06856   0.06477  -0.0219   1.0000   0.0095
 -15.500  -1.1728   0.06138   0.05742  -0.0263   1.0000   0.0094
 -15.250  -1.1906   0.05440   0.05027  -0.0308   1.0000   0.0094
 -15.000  -1.2036   0.04859   0.04429  -0.0345   1.0000   0.0095
 -14.750  -1.2114   0.04398   0.03956  -0.0372   1.0000   0.0097
 -14.500  -1.2191   0.04000   0.03539  -0.0389   1.0000   0.0097
 -14.250  -1.2171   0.03752   0.03282  -0.0395   1.0000   0.0100
 -14.000  -1.2189   0.03495   0.03011  -0.0393   1.0000   0.0100
 -13.750  -1.2201   0.03270   0.02773  -0.0385   1.0000   0.0102
 -13.500  -1.2152   0.03117   0.02610  -0.0374   1.0000   0.0105
 -13.250  -1.2097   0.02980   0.02462  -0.0358   1.0000   0.0107
 -13.000  -1.2038   0.02855   0.02326  -0.0339   1.0000   0.0110
 -12.750  -1.1991   0.02733   0.02192  -0.0315   1.0000   0.0112
 -12.500  -1.1912   0.02638   0.02086  -0.0291   1.0000   0.0116
 -12.250  -1.1837   0.02540   0.01977  -0.0265   1.0000   0.0118
 -12.000  -1.1729   0.02443   0.01868  -0.0243   1.0000   0.0120
 -11.750  -1.1618   0.02342   0.01757  -0.0222   1.0000   0.0124
 -11.500  -1.1485   0.02252   0.01660  -0.0203   1.0000   0.0128
 -11.250  -1.1330   0.02177   0.01578  -0.0186   1.0000   0.0133
 -11.000  -1.1162   0.02109   0.01504  -0.0171   1.0000   0.0138
 -10.750  -1.0993   0.02039   0.01426  -0.0155   1.0000   0.0144
 -10.500  -1.0814   0.01977   0.01356  -0.0140   1.0000   0.0150
 -10.250  -1.0628   0.01920   0.01288  -0.0126   1.0000   0.0156
 -10.000  -1.0454   0.01850   0.01213  -0.0110   1.0000   0.0164
  -9.750  -1.0266   0.01792   0.01152  -0.0096   1.0000   0.0172
  -9.500  -1.0068   0.01742   0.01098  -0.0083   1.0000   0.0182
  -9.250  -0.9870   0.01693   0.01042  -0.0070   1.0000   0.0192
  -9.000  -0.9668   0.01649   0.00989  -0.0056   1.0000   0.0199
  -8.750  -0.9479   0.01591   0.00928  -0.0041   1.0000   0.0210
  -8.500  -0.9280   0.01545   0.00880  -0.0027   1.0000   0.0223
  -8.250  -0.9075   0.01505   0.00837  -0.0014   1.0000   0.0237
  -8.000  -0.8869   0.01469   0.00795   0.0000   1.0000   0.0251
  -7.750  -0.8671   0.01424   0.00747   0.0015   1.0000   0.0267
  -7.500  -0.8472   0.01384   0.00705   0.0029   1.0000   0.0284
  -7.250  -0.8269   0.01349   0.00668   0.0044   1.0000   0.0303
  -7.000  -0.8062   0.01320   0.00635   0.0058   1.0000   0.0321
  -6.750  -0.7866   0.01281   0.00596   0.0073   1.0000   0.0349
  -6.500  -0.7666   0.01250   0.00564   0.0088   1.0000   0.0378
  -6.250  -0.7440   0.01223   0.00534   0.0098   0.9997   0.0406
  -6.000  -0.7114   0.01184   0.00498   0.0086   0.9972   0.0469
  -5.750  -0.6791   0.01151   0.00465   0.0075   0.9941   0.0532
  -5.500  -0.6468   0.01118   0.00435   0.0064   0.9910   0.0622
  -5.250  -0.6145   0.01083   0.00406   0.0053   0.9883   0.0748
  -5.000  -0.5840   0.01048   0.00378   0.0046   0.9848   0.0907
  -4.750  -0.5519   0.01013   0.00353   0.0035   0.9821   0.1119
  -4.500  -0.5212   0.00980   0.00331   0.0028   0.9785   0.1353
  -4.250  -0.4905   0.00953   0.00311   0.0021   0.9743   0.1562
  -4.000  -0.4564   0.00925   0.00292   0.0007   0.9710   0.1771
  -3.750  -0.4249   0.00900   0.00274  -0.0001   0.9638   0.1968
  -3.500  -0.3878   0.00873   0.00255  -0.0021   0.9593   0.2202
  -3.250  -0.3569   0.00851   0.00241  -0.0028   0.9526   0.2400
  -3.000  -0.3222   0.00827   0.00226  -0.0043   0.9464   0.2647
  -2.750  -0.2894   0.00802   0.00212  -0.0053   0.9365   0.2940
  -2.500  -0.2554   0.00778   0.00197  -0.0066   0.9246   0.3234
  -2.250  -0.2235   0.00756   0.00185  -0.0074   0.9106   0.3549
  -2.000  -0.1936   0.00737   0.00173  -0.0078   0.8938   0.3854
  -1.750  -0.1651   0.00721   0.00163  -0.0077   0.8733   0.4152
  -1.500  -0.1383   0.00706   0.00153  -0.0074   0.8510   0.4474
  -1.250  -0.1130   0.00694   0.00145  -0.0066   0.8242   0.4791
  -1.000  -0.0892   0.00683   0.00137  -0.0056   0.7942   0.5153
  -0.750  -0.0661   0.00676   0.00132  -0.0043   0.7626   0.5523
  -0.500  -0.0438   0.00672   0.00128  -0.0030   0.7291   0.5885
  -0.250  -0.0217   0.00670   0.00125  -0.0015   0.6947   0.6230
   0.000   0.0001   0.00670   0.00124   0.0000   0.6579   0.6570
   0.250   0.0217   0.00670   0.00125   0.0015   0.6220   0.6944
   0.750   0.0661   0.00677   0.00132   0.0043   0.5518   0.7619
   1.000   0.0892   0.00682   0.00138   0.0056   0.5172   0.7964
   1.250   0.1131   0.00694   0.00145   0.0066   0.4797   0.8247
   1.500   0.1382   0.00706   0.00153   0.0074   0.4468   0.8509
   1.750   0.1651   0.00721   0.00163   0.0078   0.4145   0.8734
   2.000   0.1936   0.00737   0.00173   0.0078   0.3855   0.8939
   2.250   0.2234   0.00757   0.00185   0.0074   0.3535   0.9109
   2.750   0.2894   0.00801   0.00211   0.0053   0.2950   0.9364
   3.000   0.3221   0.00827   0.00226   0.0043   0.2646   0.9463
   3.250   0.3569   0.00851   0.00241   0.0028   0.2411   0.9525
   3.500   0.3879   0.00874   0.00256   0.0021   0.2192   0.9593
   3.750   0.4249   0.00900   0.00274   0.0001   0.1958   0.9638
   4.000   0.4564   0.00925   0.00292  -0.0007   0.1766   0.9709
   4.250   0.4905   0.00953   0.00311  -0.0021   0.1554   0.9744
   4.500   0.5214   0.00980   0.00331  -0.0028   0.1354   0.9786
   4.750   0.5521   0.01013   0.00353  -0.0035   0.1131   0.9821
   5.000   0.5841   0.01047   0.00378  -0.0046   0.0913   0.9848
   5.250   0.6146   0.01084   0.00406  -0.0053   0.0742   0.9884
   5.500   0.6468   0.01119   0.00435  -0.0064   0.0616   0.9911
   5.750   0.6791   0.01152   0.00466  -0.0075   0.0527   0.9941
   6.000   0.7114   0.01185   0.00499  -0.0086   0.0466   0.9973
   6.250   0.7440   0.01224   0.00534  -0.0098   0.0404   0.9997
   6.500   0.7664   0.01250   0.00564  -0.0088   0.0377   1.0000
   6.750   0.7865   0.01282   0.00596  -0.0073   0.0349   1.0000
   7.000   0.8060   0.01322   0.00636  -0.0057   0.0322   1.0000
   7.250   0.8266   0.01351   0.00671  -0.0043   0.0306   1.0000
   7.500   0.8471   0.01384   0.00707  -0.0029   0.0286   1.0000
   7.750   0.8670   0.01425   0.00748  -0.0014   0.0267   1.0000
   8.000   0.8869   0.01468   0.00794   0.0000   0.0250   1.0000
   8.250   0.9076   0.01504   0.00835   0.0014   0.0237   1.0000
   8.500   0.9280   0.01545   0.00880   0.0027   0.0223   1.0000
   8.750   0.9479   0.01591   0.00929   0.0041   0.0211   1.0000
   9.000   0.9667   0.01649   0.00990   0.0056   0.0200   1.0000
   9.250   0.9868   0.01695   0.01044   0.0070   0.0192   1.0000
   9.500   1.0070   0.01741   0.01096   0.0083   0.0182   1.0000
   9.750   1.0267   0.01791   0.01151   0.0096   0.0173   1.0000
  10.000   1.0457   0.01848   0.01211   0.0110   0.0164   1.0000
  10.250   1.0633   0.01916   0.01284   0.0125   0.0156   1.0000
  10.500   1.0816   0.01977   0.01356   0.0140   0.0151   1.0000
  10.750   1.0996   0.02039   0.01426   0.0155   0.0144   1.0000
  11.000   1.1168   0.02106   0.01501   0.0170   0.0138   1.0000
  11.250   1.1336   0.02173   0.01575   0.0185   0.0133   1.0000
  11.500   1.1489   0.02251   0.01659   0.0202   0.0129   1.0000
  11.750   1.1623   0.02340   0.01755   0.0221   0.0124   1.0000
  12.000   1.1735   0.02441   0.01865   0.0242   0.0120   1.0000
  12.250   1.1855   0.02533   0.01970   0.0262   0.0117   1.0000
  12.500   1.1934   0.02629   0.02077   0.0288   0.0115   1.0000
  12.750   1.2008   0.02726   0.02185   0.0313   0.0111   1.0000
  13.000   1.2091   0.02825   0.02294   0.0334   0.0107   1.0000
  13.250   1.2123   0.02967   0.02448   0.0356   0.0106   1.0000
  13.500   1.2198   0.03088   0.02579   0.0370   0.0103   1.0000
  13.750   1.2217   0.03266   0.02768   0.0383   0.0101   1.0000
  14.000   1.2244   0.03452   0.02965   0.0391   0.0099   1.0000
  14.250   1.2240   0.03691   0.03216   0.0393   0.0097   1.0000
  14.500   1.2202   0.04000   0.03540   0.0387   0.0097   1.0000
  14.750   1.2142   0.04381   0.03934   0.0370   0.0095   1.0000
  15.000   1.2004   0.04929   0.04499   0.0338   0.0093   1.0000
  15.250   1.1897   0.05481   0.05067   0.0302   0.0093   1.0000
  15.750   1.1537   0.06901   0.06519   0.0212   0.0093   1.0000
  16.000   1.1271   0.07765   0.07396   0.0162   0.0092   1.0000
  16.250   1.1086   0.08488   0.08134   0.0122   0.0093   1.0000
  16.500   1.0810   0.09370   0.09029   0.0074   0.0093   1.0000
  16.750   1.0559   0.10233   0.09907   0.0028   0.0095   1.0000
  17.000   1.0300   0.11145   0.10830  -0.0020   0.0095   1.0000
  17.250   1.0046   0.12077   0.11774  -0.0069   0.0095   1.0000
  17.500   0.9743   0.13152   0.12863  -0.0125   0.0096   1.0000
  17.750   0.9430   0.14307   0.14031  -0.0185   0.0095   1.0000
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