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WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 76-100 (fx76100-il)
Reynolds number: 200,000
Max Cl/Cd: 46.1 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76100-il-200000-n5.txt
Download as CSV file: xf-fx76100-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.8688   0.09910   0.09505  -0.0091   1.0000   0.0183
 -14.250  -0.9235   0.08301   0.07872  -0.0195   1.0000   0.0178
 -14.000  -0.9659   0.07058   0.06599  -0.0279   1.0000   0.0171
 -13.750  -0.9832   0.06367   0.05890  -0.0328   1.0000   0.0173
 -13.500  -0.9996   0.05752   0.05255  -0.0368   1.0000   0.0174
 -13.250  -1.0117   0.05265   0.04748  -0.0395   1.0000   0.0175
 -13.000  -1.0224   0.04852   0.04315  -0.0411   1.0000   0.0177
 -12.750  -1.0295   0.04532   0.03977  -0.0415   1.0000   0.0181
 -12.500  -1.0349   0.04263   0.03687  -0.0411   1.0000   0.0186
 -12.250  -1.0405   0.04005   0.03406  -0.0398   1.0000   0.0190
 -12.000  -1.0428   0.03786   0.03167  -0.0378   1.0000   0.0192
 -11.750  -1.0436   0.03601   0.02956  -0.0354   1.0000   0.0198
 -11.500  -1.0425   0.03431   0.02768  -0.0327   1.0000   0.0203
 -11.250  -1.0387   0.03282   0.02612  -0.0301   1.0000   0.0208
 -11.000  -1.0302   0.03159   0.02479  -0.0280   1.0000   0.0213
 -10.750  -1.0200   0.03037   0.02347  -0.0260   1.0000   0.0221
 -10.500  -1.0083   0.02915   0.02211  -0.0241   1.0000   0.0229
 -10.250  -0.9951   0.02803   0.02083  -0.0222   1.0000   0.0240
 -10.000  -0.9808   0.02690   0.01953  -0.0204   1.0000   0.0250
  -9.750  -0.9669   0.02573   0.01825  -0.0186   1.0000   0.0260
  -9.500  -0.9520   0.02479   0.01727  -0.0169   1.0000   0.0273
  -9.250  -0.9357   0.02392   0.01631  -0.0152   1.0000   0.0287
  -9.000  -0.9190   0.02303   0.01532  -0.0136   1.0000   0.0300
  -8.750  -0.9014   0.02223   0.01438  -0.0120   1.0000   0.0316
  -8.500  -0.8852   0.02132   0.01343  -0.0102   1.0000   0.0335
  -8.250  -0.8675   0.02059   0.01266  -0.0086   1.0000   0.0354
  -8.000  -0.8490   0.01992   0.01190  -0.0071   1.0000   0.0377
  -7.750  -0.8299   0.01931   0.01118  -0.0055   1.0000   0.0400
  -7.500  -0.8127   0.01851   0.01038  -0.0038   1.0000   0.0427
  -7.250  -0.7936   0.01793   0.00976  -0.0023   1.0000   0.0460
  -7.000  -0.7740   0.01740   0.00914  -0.0008   1.0000   0.0494
  -6.750  -0.7556   0.01676   0.00850   0.0009   1.0000   0.0540
  -6.500  -0.7359   0.01627   0.00797   0.0023   1.0000   0.0595
  -6.250  -0.7169   0.01572   0.00743   0.0039   1.0000   0.0658
  -6.000  -0.6971   0.01526   0.00695   0.0054   1.0000   0.0743
  -5.750  -0.6776   0.01478   0.00650   0.0069   1.0000   0.0860
  -5.500  -0.6584   0.01429   0.00610   0.0085   1.0000   0.1021
  -5.250  -0.6389   0.01386   0.00575   0.0100   1.0000   0.1225
  -5.000  -0.6191   0.01348   0.00546   0.0114   1.0000   0.1446
  -4.750  -0.5991   0.01316   0.00519   0.0128   1.0000   0.1662
  -4.500  -0.5789   0.01287   0.00496   0.0142   1.0000   0.1870
  -4.250  -0.5587   0.01259   0.00476   0.0156   1.0000   0.2072
  -4.000  -0.5384   0.01235   0.00457   0.0170   1.0000   0.2283
  -3.750  -0.5124   0.01209   0.00439   0.0172   0.9984   0.2511
  -3.500  -0.4782   0.01183   0.00421   0.0156   0.9936   0.2783
  -3.250  -0.4438   0.01154   0.00406   0.0140   0.9891   0.3108
  -3.000  -0.4101   0.01124   0.00390   0.0126   0.9833   0.3465
  -2.750  -0.3754   0.01094   0.00375   0.0110   0.9767   0.3857
  -2.500  -0.3390   0.01062   0.00361   0.0091   0.9702   0.4281
  -2.250  -0.3070   0.01032   0.00347   0.0083   0.9623   0.4684
  -2.000  -0.2737   0.01001   0.00336   0.0072   0.9556   0.5150
  -1.750  -0.2407   0.00972   0.00326   0.0063   0.9474   0.5637
  -1.500  -0.2078   0.00944   0.00317   0.0055   0.9374   0.6119
  -1.250  -0.1730   0.00917   0.00310   0.0044   0.9276   0.6593
  -1.000  -0.1399   0.00895   0.00305   0.0037   0.9153   0.7048
  -0.750  -0.1070   0.00878   0.00303   0.0032   0.9011   0.7466
  -0.500  -0.0720   0.00866   0.00301   0.0023   0.8851   0.7843
  -0.250  -0.0358   0.00859   0.00301   0.0011   0.8670   0.8169
   0.000   0.0001   0.00857   0.00302   0.0000   0.8439   0.8443
   0.250   0.0359   0.00859   0.00301  -0.0011   0.8170   0.8670
   0.500   0.0721   0.00866   0.00302  -0.0023   0.7850   0.8852
   0.750   0.1069   0.00878   0.00302  -0.0031   0.7459   0.9009
   1.000   0.1399   0.00895   0.00305  -0.0037   0.7046   0.9153
   1.250   0.1729   0.00917   0.00310  -0.0043   0.6583   0.9275
   1.500   0.2077   0.00944   0.00317  -0.0054   0.6109   0.9374
   1.750   0.2406   0.00971   0.00326  -0.0063   0.5645   0.9474
   2.000   0.2737   0.01001   0.00336  -0.0072   0.5148   0.9557
   2.250   0.3069   0.01032   0.00347  -0.0083   0.4686   0.9622
   2.500   0.3390   0.01062   0.00361  -0.0091   0.4272   0.9702
   2.750   0.3754   0.01094   0.00375  -0.0110   0.3853   0.9767
   3.000   0.4101   0.01124   0.00390  -0.0126   0.3469   0.9833
   3.250   0.4439   0.01154   0.00406  -0.0140   0.3105   0.9891
   3.500   0.4785   0.01182   0.00421  -0.0156   0.2794   0.9937
   3.750   0.5125   0.01210   0.00439  -0.0172   0.2504   0.9984
   4.000   0.5383   0.01235   0.00457  -0.0170   0.2282   1.0000
   4.250   0.5586   0.01259   0.00475  -0.0156   0.2069   1.0000
   4.500   0.5787   0.01288   0.00496  -0.0142   0.1864   1.0000
   4.750   0.5990   0.01316   0.00519  -0.0128   0.1658   1.0000
   5.000   0.6190   0.01349   0.00546  -0.0114   0.1443   1.0000
   5.250   0.6389   0.01386   0.00575  -0.0099   0.1224   1.0000
   5.500   0.6583   0.01429   0.00610  -0.0085   0.1020   1.0000
   5.750   0.6776   0.01478   0.00650  -0.0069   0.0863   1.0000
   6.000   0.6970   0.01526   0.00695  -0.0054   0.0740   1.0000
   6.250   0.7168   0.01572   0.00743  -0.0039   0.0656   1.0000
   6.500   0.7359   0.01627   0.00796  -0.0023   0.0592   1.0000
   6.750   0.7556   0.01676   0.00850  -0.0008   0.0537   1.0000
   7.000   0.7740   0.01740   0.00914   0.0008   0.0493   1.0000
   7.250   0.7936   0.01794   0.00977   0.0023   0.0459   1.0000
   7.500   0.8126   0.01853   0.01040   0.0038   0.0429   1.0000
   7.750   0.8298   0.01931   0.01119   0.0056   0.0400   1.0000
   8.000   0.8490   0.01992   0.01190   0.0071   0.0377   1.0000
   8.250   0.8673   0.02062   0.01270   0.0087   0.0356   1.0000
   8.500   0.8852   0.02133   0.01345   0.0102   0.0336   1.0000
   8.750   0.9008   0.02231   0.01445   0.0120   0.0318   1.0000
   9.000   0.9187   0.02308   0.01536   0.0136   0.0302   1.0000
   9.250   0.9356   0.02395   0.01634   0.0153   0.0288   1.0000
   9.500   0.9523   0.02476   0.01722   0.0168   0.0273   1.0000
   9.750   0.9674   0.02571   0.01823   0.0185   0.0261   1.0000
  10.000   0.9812   0.02687   0.01949   0.0204   0.0249   1.0000
  10.250   0.9957   0.02794   0.02075   0.0221   0.0238   1.0000
  10.500   1.0086   0.02915   0.02211   0.0240   0.0229   1.0000
  10.750   1.0203   0.03035   0.02344   0.0259   0.0220   1.0000
  11.000   1.0309   0.03153   0.02473   0.0279   0.0213   1.0000
  11.250   1.0394   0.03281   0.02612   0.0300   0.0208   1.0000
  11.500   1.0432   0.03429   0.02767   0.0326   0.0203   1.0000
  11.750   1.0443   0.03600   0.02955   0.0353   0.0198   1.0000
  12.000   1.0439   0.03786   0.03165   0.0377   0.0193   1.0000
  12.250   1.0410   0.04001   0.03404   0.0396   0.0187   1.0000
  12.500   1.0372   0.04239   0.03662   0.0409   0.0184   1.0000
  12.750   1.0319   0.04505   0.03949   0.0413   0.0178   1.0000
  13.000   1.0233   0.04852   0.04316   0.0409   0.0176   1.0000
  13.250   1.0140   0.05245   0.04728   0.0394   0.0174   1.0000
  13.500   1.0019   0.05734   0.05235   0.0367   0.0173   1.0000
  13.750   0.9867   0.06328   0.05849   0.0328   0.0171   1.0000
  14.000   0.9637   0.07128   0.06672   0.0273   0.0172   1.0000
  14.250   0.9285   0.08232   0.07801   0.0197   0.0175   1.0000
  14.500   0.8707   0.09907   0.09502   0.0089   0.0183   1.0000
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