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WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 76-100 (fx76100-il)
Reynolds number: 200,000
Max Cl/Cd: 47.1 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76100-il-200000.txt
Download as CSV file: xf-fx76100-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.7038   0.11053   0.10673  -0.0075   1.0000   0.0505
 -12.250  -0.6951   0.10925   0.10544  -0.0062   1.0000   0.0515
 -12.000  -0.9277   0.05715   0.05250  -0.0415   1.0000   0.0330
 -11.750  -0.9467   0.05335   0.04853  -0.0407   1.0000   0.0332
 -11.500  -0.9643   0.05019   0.04516  -0.0384   1.0000   0.0332
 -11.250  -0.9759   0.04759   0.04238  -0.0352   1.0000   0.0335
 -11.000  -0.9565   0.04736   0.04233  -0.0345   1.0000   0.0353
 -10.750  -0.9698   0.04376   0.03838  -0.0312   1.0000   0.0353
 -10.500  -0.9666   0.04181   0.03625  -0.0290   1.0000   0.0364
 -10.250  -0.9663   0.03913   0.03325  -0.0262   1.0000   0.0373
 -10.000  -0.9624   0.03648   0.03024  -0.0236   1.0000   0.0379
  -9.750  -0.9547   0.03410   0.02750  -0.0211   1.0000   0.0386
  -9.500  -0.9440   0.03225   0.02529  -0.0187   1.0000   0.0397
  -9.250  -0.9328   0.02961   0.02233  -0.0166   1.0000   0.0412
  -9.000  -0.9159   0.02802   0.02076  -0.0153   1.0000   0.0433
  -8.750  -0.8985   0.02680   0.01941  -0.0138   1.0000   0.0454
  -8.500  -0.8804   0.02552   0.01795  -0.0121   1.0000   0.0477
  -8.250  -0.8615   0.02453   0.01672  -0.0105   1.0000   0.0496
  -8.000  -0.8437   0.02256   0.01473  -0.0091   1.0000   0.0529
  -7.750  -0.8244   0.02166   0.01381  -0.0076   1.0000   0.0563
  -7.500  -0.8046   0.02075   0.01278  -0.0061   1.0000   0.0596
  -7.250  -0.7865   0.01949   0.01151  -0.0044   1.0000   0.0636
  -7.000  -0.7677   0.01871   0.01073  -0.0028   1.0000   0.0686
  -6.750  -0.7482   0.01799   0.00989  -0.0012   1.0000   0.0737
  -6.500  -0.7314   0.01702   0.00902   0.0008   1.0000   0.0811
  -6.250  -0.7138   0.01621   0.00823   0.0027   1.0000   0.0900
  -6.000  -0.6961   0.01548   0.00754   0.0046   1.0000   0.1025
  -5.750  -0.6786   0.01476   0.00694   0.0064   1.0000   0.1217
  -5.500  -0.6609   0.01412   0.00645   0.0083   1.0000   0.1513
  -5.250  -0.6421   0.01363   0.00608   0.0099   1.0000   0.1844
  -5.000  -0.6228   0.01324   0.00579   0.0115   1.0000   0.2133
  -4.750  -0.6034   0.01290   0.00552   0.0130   1.0000   0.2382
  -4.500  -0.5835   0.01260   0.00527   0.0145   1.0000   0.2628
  -4.250  -0.5639   0.01230   0.00506   0.0161   1.0000   0.2868
  -4.000  -0.5443   0.01200   0.00485   0.0176   1.0000   0.3127
  -3.750  -0.5248   0.01172   0.00466   0.0191   1.0000   0.3409
  -3.500  -0.5056   0.01143   0.00451   0.0207   1.0000   0.3723
  -3.250  -0.4869   0.01114   0.00439   0.0224   1.0000   0.4091
  -3.000  -0.4689   0.01083   0.00429   0.0243   1.0000   0.4531
  -2.750  -0.4518   0.01052   0.00422   0.0263   1.0000   0.5048
  -2.500  -0.4353   0.01023   0.00420   0.0285   1.0000   0.5624
  -2.250  -0.4192   0.00997   0.00422   0.0309   1.0000   0.6239
  -2.000  -0.4029   0.00976   0.00429   0.0333   1.0000   0.6852
  -1.750  -0.3853   0.00963   0.00441   0.0356   1.0000   0.7473
  -1.500  -0.3419   0.00966   0.00467   0.0328   0.9937   0.8142
  -1.250  -0.2926   0.00979   0.00490   0.0289   0.9877   0.8665
  -1.000  -0.2372   0.00995   0.00510   0.0238   0.9822   0.9028
  -0.750  -0.1811   0.01012   0.00525   0.0185   0.9766   0.9273
  -0.500  -0.1199   0.01027   0.00538   0.0121   0.9715   0.9423
  -0.250  -0.0605   0.01036   0.00545   0.0062   0.9652   0.9515
   0.000   0.0003   0.01041   0.00548   0.0000   0.9598   0.9598
   0.250   0.0604   0.01036   0.00545  -0.0061   0.9517   0.9653
   0.500   0.1205   0.01028   0.00538  -0.0122   0.9425   0.9716
   0.750   0.1806   0.01011   0.00524  -0.0184   0.9264   0.9763
   1.000   0.2373   0.00995   0.00509  -0.0238   0.9021   0.9821
   1.250   0.2923   0.00978   0.00490  -0.0289   0.8666   0.9876
   1.500   0.3418   0.00966   0.00467  -0.0328   0.8143   0.9937
   1.750   0.3853   0.00963   0.00441  -0.0356   0.7468   1.0000
   2.000   0.4028   0.00976   0.00429  -0.0333   0.6850   1.0000
   2.250   0.4191   0.00998   0.00422  -0.0308   0.6226   1.0000
   2.500   0.4352   0.01023   0.00419  -0.0285   0.5620   1.0000
   2.750   0.4518   0.01052   0.00422  -0.0263   0.5050   1.0000
   3.000   0.4689   0.01083   0.00429  -0.0242   0.4533   1.0000
   3.250   0.4868   0.01114   0.00439  -0.0224   0.4091   1.0000
   3.500   0.5056   0.01143   0.00451  -0.0207   0.3726   1.0000
   3.750   0.5247   0.01172   0.00466  -0.0191   0.3405   1.0000
   4.000   0.5443   0.01200   0.00485  -0.0176   0.3125   1.0000
   4.250   0.5638   0.01229   0.00505  -0.0160   0.2867   1.0000
   4.500   0.5833   0.01261   0.00527  -0.0145   0.2624   1.0000
   4.750   0.6033   0.01290   0.00552  -0.0130   0.2379   1.0000
   5.000   0.6228   0.01324   0.00579  -0.0115   0.2131   1.0000
   5.250   0.6420   0.01363   0.00608  -0.0099   0.1845   1.0000
   5.500   0.6608   0.01411   0.00645  -0.0082   0.1514   1.0000
   5.750   0.6785   0.01477   0.00694  -0.0064   0.1218   1.0000
   6.000   0.6959   0.01549   0.00755  -0.0045   0.1020   1.0000
   6.250   0.7137   0.01622   0.00823  -0.0026   0.0897   1.0000
   6.500   0.7314   0.01701   0.00901  -0.0008   0.0807   1.0000
   6.750   0.7479   0.01802   0.00992   0.0012   0.0734   1.0000
   7.000   0.7677   0.01870   0.01071   0.0028   0.0685   1.0000
   7.250   0.7864   0.01951   0.01151   0.0044   0.0636   1.0000
   7.500   0.8045   0.02080   0.01282   0.0061   0.0597   1.0000
   7.750   0.8245   0.02168   0.01384   0.0076   0.0564   1.0000
   8.000   0.8439   0.02264   0.01483   0.0091   0.0532   1.0000
   8.250   0.8617   0.02466   0.01684   0.0104   0.0498   1.0000
   8.500   0.8805   0.02554   0.01797   0.0121   0.0477   1.0000
   8.750   0.8986   0.02679   0.01941   0.0138   0.0455   1.0000
   9.000   0.9161   0.02787   0.02058   0.0153   0.0432   1.0000
   9.250   0.9329   0.02956   0.02229   0.0166   0.0413   1.0000
   9.500   0.9442   0.03220   0.02524   0.0187   0.0397   1.0000
   9.750   0.9551   0.03409   0.02748   0.0210   0.0387   1.0000
  10.000   0.9627   0.03644   0.03020   0.0235   0.0378   1.0000
  10.250   0.9666   0.03904   0.03315   0.0262   0.0369   1.0000
  10.500   0.9663   0.04190   0.03635   0.0290   0.0365   1.0000
  10.750   0.9670   0.04416   0.03883   0.0314   0.0354   1.0000
  11.000   0.9608   0.04696   0.04187   0.0342   0.0350   1.0000
  11.250   0.9779   0.04745   0.04222   0.0350   0.0334   1.0000
  11.500   0.9610   0.05048   0.04550   0.0386   0.0334   1.0000
  11.750   0.9498   0.05333   0.04846   0.0405   0.0330   1.0000
  12.000   0.9249   0.05738   0.05278   0.0413   0.0332   1.0000
  12.250   0.7949   0.08058   0.07672   0.0237   0.0383   1.0000
  12.500   0.7647   0.09160   0.08777   0.0166   0.0396   1.0000
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