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


Details Polar file
Airfoil: WORTMANN FX 76-100 (fx76100-il)
Reynolds number: 100,000
Max Cl/Cd: 36.18 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76100-il-100000-n5.txt
Download as CSV file: xf-fx76100-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.8048   0.08954   0.08394  -0.0191   1.0000   0.0321
 -12.750  -0.8316   0.07996   0.07428  -0.0257   1.0000   0.0317
 -12.500  -0.8574   0.07158   0.06576  -0.0318   1.0000   0.0313
 -12.250  -0.8837   0.06453   0.05850  -0.0367   1.0000   0.0313
 -12.000  -0.9034   0.05940   0.05317  -0.0389   1.0000   0.0311
 -11.750  -0.9262   0.05495   0.04844  -0.0395   1.0000   0.0315
 -11.500  -0.9436   0.05145   0.04466  -0.0382   1.0000   0.0317
 -11.250  -0.9573   0.04855   0.04146  -0.0355   1.0000   0.0319
 -11.000  -0.9635   0.04596   0.03868  -0.0329   1.0000   0.0326
 -10.750  -0.9599   0.04386   0.03650  -0.0311   1.0000   0.0335
 -10.500  -0.9552   0.04181   0.03428  -0.0291   1.0000   0.0342
 -10.250  -0.9488   0.03977   0.03203  -0.0271   1.0000   0.0352
 -10.000  -0.9402   0.03782   0.02984  -0.0252   1.0000   0.0365
  -9.750  -0.9299   0.03594   0.02765  -0.0233   1.0000   0.0382
  -9.500  -0.9179   0.03422   0.02554  -0.0213   1.0000   0.0402
  -9.250  -0.9039   0.03242   0.02372  -0.0199   1.0000   0.0419
  -9.000  -0.8883   0.03102   0.02224  -0.0184   1.0000   0.0436
  -8.750  -0.8722   0.02972   0.02081  -0.0168   1.0000   0.0460
  -8.500  -0.8550   0.02851   0.01934  -0.0152   1.0000   0.0492
  -8.250  -0.8387   0.02712   0.01789  -0.0136   1.0000   0.0517
  -8.000  -0.8219   0.02602   0.01675  -0.0120   1.0000   0.0547
  -7.750  -0.8041   0.02502   0.01563  -0.0105   1.0000   0.0588
  -7.500  -0.7871   0.02395   0.01450  -0.0087   1.0000   0.0630
  -7.250  -0.7699   0.02302   0.01354  -0.0071   1.0000   0.0675
  -7.000  -0.7516   0.02217   0.01256  -0.0054   1.0000   0.0735
  -6.750  -0.7346   0.02127   0.01170  -0.0037   1.0000   0.0808
  -6.500  -0.7168   0.02044   0.01086  -0.0020   1.0000   0.0897
  -6.250  -0.6985   0.01968   0.01012  -0.0004   1.0000   0.1020
  -6.000  -0.6801   0.01895   0.00947   0.0012   1.0000   0.1183
  -5.750  -0.6611   0.01831   0.00887   0.0027   1.0000   0.1390
  -5.500  -0.6419   0.01774   0.00839   0.0042   1.0000   0.1632
  -5.250  -0.6223   0.01725   0.00796   0.0056   1.0000   0.1887
  -5.000  -0.6024   0.01681   0.00755   0.0071   1.0000   0.2137
  -4.750  -0.5827   0.01638   0.00719   0.0085   1.0000   0.2379
  -4.500  -0.5627   0.01601   0.00686   0.0099   1.0000   0.2625
  -4.250  -0.5430   0.01562   0.00655   0.0114   1.0000   0.2878
  -4.000  -0.5234   0.01524   0.00628   0.0129   1.0000   0.3151
  -3.750  -0.5038   0.01488   0.00601   0.0145   1.0000   0.3448
  -3.500  -0.4843   0.01453   0.00579   0.0160   1.0000   0.3763
  -3.250  -0.4648   0.01420   0.00559   0.0176   1.0000   0.4107
  -3.000  -0.4454   0.01389   0.00541   0.0192   1.0000   0.4480
  -2.750  -0.4261   0.01359   0.00529   0.0209   1.0000   0.4883
  -2.500  -0.4066   0.01332   0.00521   0.0225   1.0000   0.5332
  -2.250  -0.3868   0.01309   0.00518   0.0242   1.0000   0.5828
  -2.000  -0.3662   0.01290   0.00518   0.0258   1.0000   0.6337
  -1.750  -0.3432   0.01275   0.00524   0.0270   0.9997   0.6875
  -1.500  -0.3007   0.01269   0.00538   0.0244   0.9917   0.7487
  -1.250  -0.2568   0.01273   0.00554   0.0216   0.9844   0.8010
  -1.000  -0.2102   0.01283   0.00569   0.0182   0.9772   0.8436
  -0.750  -0.1596   0.01294   0.00582   0.0141   0.9693   0.8769
  -0.500  -0.1071   0.01302   0.00590   0.0095   0.9599   0.9021
  -0.250  -0.0543   0.01306   0.00594   0.0049   0.9490   0.9213
   0.000   0.0001   0.01308   0.00595   0.0000   0.9368   0.9369
   0.250   0.0546   0.01306   0.00594  -0.0050   0.9213   0.9491
   0.500   0.1071   0.01302   0.00590  -0.0095   0.9020   0.9599
   0.750   0.1596   0.01294   0.00582  -0.0141   0.8770   0.9692
   1.000   0.2102   0.01283   0.00569  -0.0182   0.8439   0.9772
   1.250   0.2570   0.01273   0.00554  -0.0216   0.8013   0.9845
   1.500   0.3008   0.01269   0.00537  -0.0243   0.7474   0.9917
   1.750   0.3432   0.01276   0.00524  -0.0270   0.6865   0.9998
   2.250   0.3868   0.01309   0.00518  -0.0242   0.5829   1.0000
   2.500   0.4066   0.01332   0.00522  -0.0225   0.5337   1.0000
   2.750   0.4260   0.01359   0.00529  -0.0208   0.4880   1.0000
   3.000   0.4453   0.01389   0.00541  -0.0192   0.4481   1.0000
   3.250   0.4648   0.01420   0.00559  -0.0176   0.4107   1.0000
   3.500   0.4843   0.01453   0.00579  -0.0160   0.3764   1.0000
   3.750   0.5038   0.01488   0.00601  -0.0144   0.3449   1.0000
   4.000   0.5234   0.01524   0.00626  -0.0129   0.3157   1.0000
   4.250   0.5429   0.01562   0.00655  -0.0114   0.2881   1.0000
   4.500   0.5626   0.01601   0.00686  -0.0099   0.2623   1.0000
   4.750   0.5826   0.01639   0.00719  -0.0085   0.2377   1.0000
   5.000   0.6023   0.01681   0.00756  -0.0070   0.2132   1.0000
   5.250   0.6221   0.01725   0.00795  -0.0056   0.1884   1.0000
   5.500   0.6419   0.01774   0.00839  -0.0042   0.1632   1.0000
   5.750   0.6610   0.01832   0.00887  -0.0027   0.1390   1.0000
   6.000   0.6800   0.01895   0.00947  -0.0012   0.1181   1.0000
   6.250   0.6984   0.01968   0.01012   0.0004   0.1018   1.0000
   6.500   0.7167   0.02044   0.01086   0.0020   0.0895   1.0000
   6.750   0.7346   0.02128   0.01171   0.0037   0.0808   1.0000
   7.000   0.7515   0.02218   0.01257   0.0054   0.0735   1.0000
   7.250   0.7699   0.02303   0.01355   0.0071   0.0674   1.0000
   7.500   0.7871   0.02396   0.01450   0.0088   0.0629   1.0000
   7.750   0.8041   0.02502   0.01564   0.0105   0.0587   1.0000
   8.000   0.8220   0.02601   0.01674   0.0120   0.0546   1.0000
   8.250   0.8388   0.02713   0.01790   0.0136   0.0518   1.0000
   8.500   0.8551   0.02851   0.01935   0.0152   0.0492   1.0000
   8.750   0.8723   0.02973   0.02082   0.0168   0.0461   1.0000
   9.000   0.8885   0.03103   0.02225   0.0183   0.0437   1.0000
   9.250   0.9040   0.03245   0.02375   0.0199   0.0419   1.0000
   9.500   0.9183   0.03429   0.02560   0.0213   0.0403   1.0000
   9.750   0.9304   0.03603   0.02773   0.0232   0.0386   1.0000
  10.000   0.9404   0.03789   0.02992   0.0252   0.0367   1.0000
  10.250   0.9488   0.03984   0.03211   0.0271   0.0353   1.0000
  10.500   0.9554   0.04187   0.03436   0.0291   0.0343   1.0000
  10.750   0.9605   0.04381   0.03644   0.0310   0.0334   1.0000
  11.000   0.9651   0.04580   0.03848   0.0327   0.0325   1.0000
  11.250   0.9589   0.04845   0.04135   0.0354   0.0320   1.0000
  11.500   0.9429   0.05138   0.04461   0.0381   0.0315   1.0000
  11.750   0.9253   0.05491   0.04843   0.0394   0.0312   1.0000
  12.000   0.9051   0.05920   0.05297   0.0388   0.0310   1.0000
  12.250   0.8814   0.06485   0.05885   0.0361   0.0310   1.0000
  12.500   0.8591   0.07145   0.06563   0.0317   0.0313   1.0000
  12.750   0.8291   0.08069   0.07504   0.0248   0.0316   1.0000
  13.000   0.8001   0.09094   0.08538   0.0176   0.0320   1.0000
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