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WORTMANN FX 80-080 (fx80080-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 80-080 (fx80080-il)
Reynolds number: 500,000
Max Cl/Cd: 90.46 at α=2.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx80080-il-500000-n5.txt
Download as CSV file: xf-fx80080-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 80-080                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.4656   0.10050   0.09815  -0.0266   1.0000   0.0060
  -9.500  -0.4651   0.09644   0.09411  -0.0282   1.0000   0.0059
  -9.250  -0.4643   0.09260   0.09030  -0.0297   1.0000   0.0057
  -9.000  -0.4645   0.08855   0.08628  -0.0314   1.0000   0.0057
  -8.750  -0.4671   0.08416   0.08192  -0.0332   1.0000   0.0057
  -8.500  -0.4717   0.07973   0.07754  -0.0350   1.0000   0.0058
  -8.250  -0.4788   0.07602   0.07388  -0.0362   1.0000   0.0057
  -8.000  -0.4905   0.07297   0.07089  -0.0365   1.0000   0.0056
  -7.750  -0.4761   0.06296   0.06082  -0.0512   0.9854   0.0057
  -7.500  -0.4611   0.05456   0.05230  -0.0604   0.9720   0.0057
  -7.250  -0.4419   0.04535   0.04281  -0.0684   0.9610   0.0058
  -7.000  -0.4179   0.03522   0.03220  -0.0745   0.9530   0.0061
  -6.750  -0.3943   0.02444   0.02052  -0.0788   0.9444   0.0064
  -6.500  -0.3604   0.02296   0.01879  -0.0819   0.9393   0.0073
  -6.250  -0.3288   0.02025   0.01567  -0.0839   0.9320   0.0076
  -6.000  -0.2966   0.01717   0.01208  -0.0857   0.9252   0.0078
  -5.750  -0.2668   0.01522   0.00976  -0.0865   0.9173   0.0080
  -5.500  -0.2358   0.01385   0.00813  -0.0875   0.9109   0.0084
  -5.250  -0.2081   0.01285   0.00693  -0.0877   0.9035   0.0089
  -4.750  -0.1525   0.01143   0.00519  -0.0880   0.8909   0.0103
  -4.500  -0.1248   0.01095   0.00460  -0.0881   0.8851   0.0108
  -4.250  -0.0993   0.01030   0.00383  -0.0878   0.8793   0.0118
  -4.000  -0.0730   0.00985   0.00333  -0.0877   0.8737   0.0139
  -3.750  -0.0457   0.00955   0.00295  -0.0877   0.8693   0.0159
  -3.500  -0.0195   0.00928   0.00261  -0.0874   0.8645   0.0178
  -3.250   0.0072   0.00899   0.00227  -0.0872   0.8599   0.0240
  -3.000   0.0344   0.00879   0.00205  -0.0872   0.8558   0.0346
  -2.750   0.0604   0.00858   0.00190  -0.0869   0.8509   0.0534
  -2.500   0.0870   0.00839   0.00175  -0.0868   0.8464   0.0758
  -2.000   0.1380   0.00763   0.00149  -0.0864   0.8382   0.2391
  -1.750   0.1628   0.00720   0.00139  -0.0862   0.8341   0.3529
  -1.500   0.1866   0.00664   0.00129  -0.0857   0.8303   0.5118
  -1.250   0.2090   0.00620   0.00136  -0.0847   0.8266   0.6713
  -1.000   0.2344   0.00613   0.00141  -0.0841   0.8225   0.7224
  -0.750   0.2607   0.00612   0.00144  -0.0837   0.8185   0.7506
  -0.500   0.2873   0.00615   0.00147  -0.0833   0.8149   0.7769
  -0.250   0.3125   0.00615   0.00154  -0.0826   0.8101   0.8026
   0.000   0.3384   0.00617   0.00158  -0.0820   0.8050   0.8181
   0.250   0.3651   0.00619   0.00159  -0.0817   0.7993   0.8270
   0.500   0.3914   0.00619   0.00159  -0.0813   0.7921   0.8327
   0.750   0.4179   0.00621   0.00160  -0.0810   0.7848   0.8381
   1.250   0.4701   0.00622   0.00162  -0.0801   0.7641   0.8472
   1.500   0.4954   0.00624   0.00161  -0.0795   0.7489   0.8520
   1.750   0.5207   0.00629   0.00161  -0.0789   0.7316   0.8571
   2.000   0.5458   0.00632   0.00164  -0.0782   0.7140   0.8619
   2.250   0.5697   0.00641   0.00166  -0.0773   0.6842   0.8677
   2.500   0.5925   0.00655   0.00173  -0.0761   0.6462   0.8735
   2.750   0.6113   0.00689   0.00181  -0.0741   0.5755   0.8806
   3.000   0.6236   0.00770   0.00208  -0.0711   0.4501   0.8888
   3.250   0.6408   0.00836   0.00237  -0.0692   0.3578   0.8977
   3.500   0.6602   0.00888   0.00264  -0.0677   0.2871   0.9082
   3.750   0.6793   0.00947   0.00294  -0.0662   0.2103   0.9225
   4.000   0.7020   0.01007   0.00329  -0.0656   0.1401   0.9430
   4.250   0.7354   0.01059   0.00364  -0.0673   0.0956   0.9744
   4.500   0.7600   0.01098   0.00393  -0.0669   0.0736   1.0000
   4.750   0.7838   0.01133   0.00423  -0.0663   0.0584   1.0000
   5.000   0.8076   0.01168   0.00455  -0.0657   0.0467   1.0000
   5.250   0.8311   0.01206   0.00493  -0.0650   0.0363   1.0000
   5.500   0.8541   0.01249   0.00532  -0.0643   0.0268   1.0000
   5.750   0.8777   0.01286   0.00572  -0.0636   0.0225   1.0000
   6.000   0.8998   0.01338   0.00625  -0.0627   0.0178   1.0000
   6.250   0.9232   0.01376   0.00668  -0.0620   0.0158   1.0000
   6.500   0.9461   0.01417   0.00712  -0.0613   0.0135   1.0000
   6.750   0.9677   0.01474   0.00770  -0.0603   0.0107   1.0000
   7.000   0.9898   0.01524   0.00831  -0.0594   0.0092   1.0000
   7.250   1.0117   0.01576   0.00891  -0.0585   0.0079   1.0000
   7.500   1.0325   0.01640   0.00957  -0.0575   0.0060   1.0000
   7.750   1.0516   0.01730   0.01058  -0.0560   0.0051   1.0000
   8.000   1.0711   0.01812   0.01152  -0.0547   0.0046   1.0000
   8.250   1.0912   0.01884   0.01233  -0.0536   0.0041   1.0000
   8.500   1.1117   0.01949   0.01305  -0.0526   0.0037   1.0000
   8.750   1.1311   0.02027   0.01390  -0.0515   0.0033   1.0000
   9.000   1.1456   0.02174   0.01554  -0.0495   0.0029   1.0000
   9.250   1.1628   0.02281   0.01679  -0.0480   0.0028   1.0000
   9.500   1.1787   0.02406   0.01823  -0.0463   0.0027   1.0000
   9.750   1.1930   0.02549   0.01986  -0.0445   0.0026   1.0000
  10.000   1.2066   0.02690   0.02148  -0.0426   0.0025   1.0000
  10.250   1.2167   0.02859   0.02341  -0.0402   0.0024   1.0000
  10.500   1.2237   0.03043   0.02551  -0.0374   0.0023   1.0000
  10.750   1.2269   0.03253   0.02788  -0.0343   0.0023   1.0000
  11.000   1.2274   0.03472   0.03034  -0.0310   0.0022   1.0000
  11.250   1.2247   0.03710   0.03298  -0.0276   0.0021   1.0000
  11.500   1.2162   0.04001   0.03619  -0.0242   0.0021   1.0000
  11.750   1.2054   0.04316   0.03961  -0.0212   0.0020   1.0000
  12.000   1.1873   0.04721   0.04396  -0.0185   0.0020   1.0000
  12.250   1.1732   0.05101   0.04799  -0.0170   0.0019   1.0000
  12.500   1.1568   0.05536   0.05256  -0.0163   0.0019   1.0000
  12.750   1.1224   0.06276   0.06025  -0.0172   0.0020   1.0000
  13.000   1.1028   0.06893   0.06659  -0.0196   0.0019   1.0000
  13.250   1.0773   0.07754   0.07538  -0.0247   0.0020   1.0000
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