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WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il)
Reynolds number: 200,000
Max Cl/Cd: 29.12 at α=12.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx08s176-il-200000.txt
Download as CSV file: xf-fx08s176-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 08-S-176 AIRFOIL                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.0764   0.11342   0.10836  -0.0883   0.6597   0.0402
 -11.250  -0.0833   0.11053   0.10551  -0.0921   0.6589   0.0408
 -11.000  -0.0821   0.10729   0.10230  -0.0943   0.6580   0.0409
 -10.750  -0.0735   0.10199   0.09705  -0.0939   0.6570   0.0418
 -10.500  -0.0589   0.09940   0.09445  -0.0932   0.6558   0.0428
 -10.250  -0.0472   0.09724   0.09231  -0.0931   0.6547   0.0457
 -10.000  -0.0435   0.09431   0.08942  -0.0944   0.6536   0.0468
  -9.750  -0.0426   0.09113   0.08629  -0.0963   0.6527   0.0487
  -9.500  -0.0540   0.08738   0.08262  -0.1012   0.6519   0.0511
  -9.250  -0.0681   0.08278   0.07809  -0.1071   0.6511   0.0516
  -9.000  -0.0884   0.07903   0.07434  -0.1101   0.6502   0.0518
  -8.750  -0.1053   0.07675   0.07203  -0.1095   0.6492   0.0519
  -8.500  -0.1202   0.07475   0.06994  -0.1081   0.6482   0.0520
  -8.250  -0.1141   0.06800   0.06329  -0.1089   0.6470   0.0532
  -8.000  -0.0994   0.06549   0.06082  -0.1083   0.6458   0.0545
  -7.750  -0.0967   0.06332   0.05862  -0.1075   0.6448   0.0557
  -7.500  -0.0974   0.06104   0.05628  -0.1066   0.6439   0.0573
  -7.250  -0.0984   0.05868   0.05386  -0.1056   0.6429   0.0592
  -7.000  -0.0997   0.05639   0.05142  -0.1044   0.6419   0.0623
  -6.750  -0.1065   0.05747   0.05190  -0.1007   0.6408   0.0650
  -6.500  -0.1025   0.05072   0.04528  -0.1008   0.6397   0.0669
  -6.250  -0.0886   0.04839   0.04302  -0.1002   0.6382   0.0687
  -6.000  -0.0755   0.04669   0.04127  -0.0992   0.6367   0.0722
  -5.500  -0.0530   0.04256   0.03665  -0.0963   0.6338   0.0834
  -5.250  -0.0357   0.04090   0.03488  -0.0954   0.6326   0.0873
  -5.000  -0.0154   0.03522   0.02794  -0.0910   0.6317   0.0513
  -4.750   0.0056   0.03315   0.02556  -0.0901   0.6307   0.0511
  -4.500   0.0284   0.03157   0.02368  -0.0892   0.6297   0.0512
  -4.250   0.0518   0.03003   0.02188  -0.0885   0.6286   0.0508
  -4.000   0.0721   0.02922   0.02097  -0.0875   0.6265   0.0510
  -3.750   0.0934   0.02902   0.02065  -0.0866   0.6242   0.0520
  -3.500   0.1150   0.02770   0.01933  -0.0860   0.6225   0.0548
  -3.250   0.1374   0.02732   0.01895  -0.0854   0.6209   0.0565
  -3.000   0.1602   0.02701   0.01862  -0.0847   0.6193   0.0588
  -2.750   0.1837   0.02668   0.01825  -0.0840   0.6178   0.0617
  -2.500   0.2081   0.02630   0.01780  -0.0835   0.6165   0.0663
  -2.250   0.2318   0.02580   0.01733  -0.0829   0.6153   0.0736
  -2.000   0.2556   0.02538   0.01690  -0.0823   0.6143   0.0855
  -1.750   0.2604   0.02630   0.01805  -0.0800   0.6108   0.1030
  -1.500   0.2699   0.02657   0.01877  -0.0785   0.6072   0.1789
  -1.250   0.2559   0.02540   0.02002  -0.0708   0.6049   0.7560
  -1.000   0.2641   0.02651   0.02111  -0.0659   0.6032   0.8466
  -0.750   0.2727   0.02717   0.02170  -0.0605   0.6017   0.8771
  -0.500   0.2807   0.02759   0.02204  -0.0545   0.6005   0.9058
  -0.250   0.2401   0.03088   0.02559  -0.0481   0.5911   0.9102
   0.000   0.2607   0.03122   0.02584  -0.0446   0.5889   0.9421
   0.250   0.4564   0.03041   0.02455  -0.0722   0.5896   0.9617
   0.500   0.5254   0.02981   0.02376  -0.0795   0.5881   0.9674
   0.750   0.5894   0.02918   0.02295  -0.0860   0.5867   0.9756
   1.000   0.6348   0.02875   0.02237  -0.0893   0.5856   0.9795
   1.250   0.6698   0.02851   0.02200  -0.0907   0.5847   0.9828
   1.500   0.6651   0.03156   0.02531  -0.0899   0.5751   0.9906
   1.750   0.7003   0.03133   0.02500  -0.0915   0.5734   0.9936
   2.000   0.7396   0.03097   0.02456  -0.0939   0.5721   0.9959
   2.250   0.7786   0.03060   0.02410  -0.0960   0.5711   0.9981
   2.500   0.8164   0.03026   0.02369  -0.0980   0.5702   1.0000
   2.750   0.8431   0.03007   0.02343  -0.0978   0.5695   1.0000
   3.000   0.6445   0.03931   0.03315  -0.0703   0.5454   1.0000
   3.250   0.6677   0.03899   0.03278  -0.0693   0.5439   1.0000
   3.500   0.6301   0.04068   0.03446  -0.0610   0.5373   1.0000
   3.750   0.6762   0.03953   0.03326  -0.0624   0.5381   1.0000
   4.000   0.7223   0.03850   0.03217  -0.0641   0.5386   1.0000
   4.250   0.7693   0.03758   0.03121  -0.0664   0.5391   1.0000
   4.500   0.8151   0.03659   0.03018  -0.0684   0.5395   1.0000
   4.750   0.8598   0.03558   0.02912  -0.0702   0.5400   1.0000
   5.000   0.6246   0.04448   0.03814  -0.0406   0.5108   1.0000
   5.250   0.6636   0.04354   0.03717  -0.0412   0.5115   1.0000
   5.500   0.6050   0.04909   0.04277  -0.0370   0.4910   1.0000
   5.750   0.6296   0.04931   0.04298  -0.0372   0.4885   1.0000
   6.000   0.6585   0.04921   0.04287  -0.0375   0.4870   1.0000
   6.250   0.6891   0.04900   0.04265  -0.0379   0.4860   1.0000
   6.500   0.6755   0.05245   0.04612  -0.0369   0.4751   1.0000
   6.750   0.7026   0.05255   0.04624  -0.0373   0.4734   1.0000
   7.000   0.7327   0.05239   0.04608  -0.0378   0.4724   1.0000
   7.250   0.7641   0.05210   0.04580  -0.0383   0.4717   1.0000
   7.500   0.7963   0.05173   0.04546  -0.0388   0.4711   1.0000
   7.750   0.8283   0.05134   0.04509  -0.0393   0.4705   1.0000
   8.000   0.7534   0.06108   0.05489  -0.0371   0.4483   1.0000
   8.250   0.7758   0.06170   0.05553  -0.0374   0.4462   1.0000
   8.500   0.8032   0.06177   0.05563  -0.0378   0.4450   1.0000
   8.750   0.7813   0.06704   0.06094  -0.0374   0.4351   1.0000
   9.000   0.7999   0.06811   0.06205  -0.0377   0.4327   1.0000
   9.250   0.8250   0.06845   0.06244  -0.0380   0.4313   1.0000
   9.500   0.8053   0.07380   0.06784  -0.0379   0.4227   1.0000
   9.750   0.8189   0.07542   0.06951  -0.0382   0.4193   1.0000
  10.000   0.8441   0.07569   0.06983  -0.0385   0.4176   1.0000
  10.250   0.8712   0.07576   0.06995  -0.0388   0.4165   1.0000
  10.500   0.9007   0.07551   0.06978  -0.0392   0.4157   1.0000
  10.750   0.9322   0.07499   0.06933  -0.0395   0.4151   1.0000
  11.250   1.0410   0.06660   0.06111  -0.0399   0.4146   1.0000
  11.500   1.1687   0.05241   0.04705  -0.0413   0.4170   1.0000
  11.750   1.2408   0.04652   0.04124  -0.0426   0.4098   1.0000
  12.000   1.2762   0.04491   0.03965  -0.0429   0.3957   1.0000
  12.250   1.2975   0.04456   0.03913  -0.0425   0.3696   1.0000
  12.500   1.2961   0.04679   0.04129  -0.0417   0.3487   1.0000
  12.750   1.2909   0.04943   0.04378  -0.0407   0.3221   1.0000
  13.000   1.2792   0.05295   0.04717  -0.0398   0.2918   1.0000
  13.250   1.2627   0.05709   0.05109  -0.0389   0.2487   1.0000
  13.500   1.2380   0.06230   0.05598  -0.0381   0.2073   1.0000
  13.750   1.2077   0.06843   0.06181  -0.0376   0.1639   1.0000
  14.000   1.1840   0.07412   0.06726  -0.0374   0.1249   1.0000
  14.250   1.1573   0.08039   0.07322  -0.0375   0.0782   1.0000
  14.500   1.1369   0.08613   0.07871  -0.0379   0.0442   1.0000
  14.750   1.1306   0.09028   0.08282  -0.0383   0.0306   1.0000
  15.000   1.1278   0.09408   0.08663  -0.0389   0.0250   1.0000
  15.250   1.1293   0.09737   0.09002  -0.0395   0.0229   1.0000
  15.500   1.1301   0.10081   0.09354  -0.0402   0.0215   1.0000
  15.750   1.1300   0.10441   0.09725  -0.0410   0.0205   1.0000
  16.000   1.1275   0.10838   0.10133  -0.0419   0.0195   1.0000
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