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Fage & Collins 3 (fg3-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Fage & Collins 3 (fg3-il)
Reynolds number: 1,000,000
Max Cl/Cd: 111.88 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fg3-il-1000000.txt
Download as CSV file: xf-fg3-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Fage & Collins 3                                
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.3625   0.12702   0.12539  -0.0244   1.0000   0.0095
 -11.250  -0.3594   0.12319   0.12158  -0.0241   1.0000   0.0097
 -11.000  -0.3573   0.11980   0.11820  -0.0247   1.0000   0.0097
 -10.750  -0.3521   0.11761   0.11603  -0.0245   1.0000   0.0099
 -10.500  -0.3491   0.11489   0.11332  -0.0248   1.0000   0.0100
 -10.250  -0.3472   0.11202   0.11046  -0.0251   1.0000   0.0100
 -10.000  -0.3452   0.10953   0.10798  -0.0252   1.0000   0.0103
  -9.750  -0.3384   0.10609   0.10455  -0.0271   0.9996   0.0104
  -9.500  -0.3233   0.10199   0.10045  -0.0315   0.9983   0.0107
  -9.250  -0.3118   0.09635   0.09481  -0.0388   0.9963   0.0124
  -9.000  -0.2976   0.09133   0.08980  -0.0450   0.9945   0.0124
  -8.750  -0.2860   0.08678   0.08525  -0.0496   0.9917   0.0124
  -8.500  -0.2733   0.08183   0.08030  -0.0555   0.9883   0.0125
  -8.250  -0.2589   0.07684   0.07531  -0.0626   0.9852   0.0125
  -8.000  -0.2582   0.07290   0.07138  -0.0641   0.9762   0.0128
  -7.750  -0.2563   0.06864   0.06711  -0.0670   0.9556   0.0128
  -7.500  -0.2390   0.06515   0.06359  -0.0709   0.9467   0.0130
  -7.250  -0.2156   0.06059   0.05897  -0.0772   0.9398   0.0132
  -7.000  -0.1845   0.05658   0.05488  -0.0841   0.9351   0.0143
  -6.750  -0.1416   0.04799   0.04601  -0.0958   0.9285   0.0159
  -6.500  -0.1013   0.04151   0.03926  -0.1038   0.9219   0.0160
  -6.000  -0.0504   0.03207   0.02933  -0.1106   0.9054   0.0166
  -5.750  -0.0270   0.03120   0.02838  -0.1112   0.8971   0.0172
  -5.500  -0.0084   0.02954   0.02658  -0.1104   0.8883   0.0182
  -5.250   0.0125   0.02721   0.02385  -0.1075   0.8813   0.0203
  -5.000   0.0244   0.02494   0.02131  -0.1045   0.8748   0.0203
  -4.750   0.0233   0.02044   0.01642  -0.0994   0.8676   0.0209
  -4.500   0.0434   0.01966   0.01562  -0.0985   0.8617   0.0213
  -4.250   0.0611   0.01891   0.01481  -0.0967   0.8546   0.0219
  -4.000   0.0827   0.01842   0.01424  -0.0956   0.8480   0.0237
  -3.750   0.1064   0.01881   0.01438  -0.0934   0.8399   0.0258
  -3.500   0.1246   0.01777   0.01312  -0.0912   0.8325   0.0259
  -3.250   0.1346   0.01456   0.00957  -0.0875   0.8225   0.0267
  -3.000   0.1552   0.01359   0.00858  -0.0861   0.8119   0.0275
  -2.750   0.1761   0.01308   0.00801  -0.0847   0.7985   0.0287
  -2.500   0.1970   0.01273   0.00753  -0.0830   0.7816   0.0308
  -2.250   0.2184   0.01336   0.00801  -0.0812   0.7587   0.0328
  -2.000   0.2375   0.01320   0.00765  -0.0790   0.7330   0.0330
  -1.750   0.2559   0.01111   0.00533  -0.0770   0.7067   0.0352
  -1.500   0.2747   0.01079   0.00489  -0.0750   0.6733   0.0366
  -1.250   0.2922   0.01068   0.00460  -0.0727   0.6302   0.0386
  -1.000   0.3077   0.01082   0.00448  -0.0699   0.5740   0.0408
  -0.750   0.3237   0.01050   0.00393  -0.0675   0.5235   0.0466
  -0.500   0.3427   0.01046   0.00374  -0.0656   0.4852   0.0499
  -0.250   0.3647   0.01013   0.00315  -0.0637   0.4599   0.0342
   0.000   0.3863   0.01020   0.00312  -0.0623   0.4381   0.0335
   0.250   0.4070   0.01007   0.00292  -0.0607   0.4209   0.0335
   0.500   0.4273   0.00989   0.00268  -0.0590   0.4064   0.0328
   0.750   0.4471   0.00968   0.00241  -0.0573   0.3941   0.0325
   1.000   0.4684   0.00962   0.00229  -0.0558   0.3831   0.0327
   1.250   0.4902   0.00963   0.00224  -0.0545   0.3727   0.0331
   1.500   0.5115   0.00953   0.00209  -0.0531   0.3632   0.0336
   1.750   0.5334   0.00949   0.00200  -0.0518   0.3550   0.0346
   2.000   0.5558   0.00951   0.00197  -0.0506   0.3476   0.0352
   2.250   0.5782   0.00953   0.00196  -0.0495   0.3405   0.0359
   2.500   0.6009   0.00957   0.00197  -0.0484   0.3341   0.0376
   2.750   0.6230   0.00964   0.00201  -0.0473   0.3279   0.0393
   3.000   0.6461   0.00967   0.00203  -0.0463   0.3229   0.0419
   3.250   0.8987   0.00869   0.00309  -0.0995   0.3043   1.0000
   3.500   0.9208   0.00885   0.00321  -0.0983   0.2993   1.0000
   3.750   0.9443   0.00894   0.00331  -0.0975   0.2958   1.0000
   4.000   0.9672   0.00905   0.00341  -0.0966   0.2916   1.0000
   4.250   0.9887   0.00924   0.00355  -0.0954   0.2843   1.0000
   4.500   1.0123   0.00932   0.00364  -0.0946   0.2792   1.0000
   4.750   1.0344   0.00947   0.00377  -0.0936   0.2729   1.0000
   5.000   1.0569   0.00961   0.00390  -0.0926   0.2675   1.0000
   5.250   1.0796   0.00974   0.00403  -0.0916   0.2620   1.0000
   5.500   1.1011   0.00993   0.00420  -0.0905   0.2562   1.0000
   5.750   1.1239   0.01005   0.00433  -0.0896   0.2501   1.0000
   6.000   1.1450   0.01026   0.00450  -0.0884   0.2414   1.0000
   6.250   1.1669   0.01043   0.00466  -0.0874   0.2314   1.0000
   6.500   1.1874   0.01067   0.00486  -0.0861   0.2182   1.0000
   6.750   1.2025   0.01125   0.00519  -0.0839   0.1779   1.0000
   7.250   1.2044   0.01435   0.00735  -0.0742   0.0183   1.0000
   7.500   1.2227   0.01471   0.00776  -0.0725   0.0164   1.0000
   7.750   1.2402   0.01510   0.00819  -0.0707   0.0152   1.0000
   8.000   1.2555   0.01561   0.00875  -0.0685   0.0137   1.0000
   8.250   1.2672   0.01619   0.00941  -0.0655   0.0126   1.0000
   8.500   1.2801   0.01658   0.00985  -0.0627   0.0122   1.0000
   8.750   1.2929   0.01698   0.01030  -0.0601   0.0117   1.0000
   9.000   1.3047   0.01744   0.01082  -0.0572   0.0111   1.0000
   9.250   1.3159   0.01796   0.01139  -0.0544   0.0104   1.0000
   9.500   1.3257   0.01858   0.01206  -0.0514   0.0098   1.0000
   9.750   1.3252   0.01974   0.01335  -0.0467   0.0092   1.0000
  10.000   1.3265   0.02081   0.01453  -0.0425   0.0090   1.0000
  10.250   1.3348   0.02157   0.01537  -0.0397   0.0090   1.0000
  10.500   1.3468   0.02216   0.01601  -0.0375   0.0087   1.0000
  10.750   1.3530   0.02310   0.01703  -0.0346   0.0085   1.0000
  11.000   1.3552   0.02429   0.01832  -0.0314   0.0085   1.0000
  11.250   1.3696   0.02485   0.01890  -0.0300   0.0077   1.0000
  11.500   1.3742   0.02602   0.02015  -0.0275   0.0076   1.0000
  11.750   1.3754   0.02748   0.02169  -0.0247   0.0073   1.0000
  12.000   1.3791   0.02885   0.02313  -0.0226   0.0071   1.0000
  12.250   1.3790   0.03058   0.02493  -0.0202   0.0069   1.0000
  12.500   1.3775   0.03252   0.02697  -0.0181   0.0069   1.0000
  12.750   1.3710   0.03505   0.02959  -0.0160   0.0068   1.0000
  13.000   1.3652   0.03772   0.03238  -0.0143   0.0068   1.0000
  13.250   1.3503   0.04153   0.03629  -0.0129   0.0065   1.0000
  13.500   1.3376   0.04540   0.04028  -0.0120   0.0065   1.0000
  13.750   1.3195   0.05008   0.04508  -0.0113   0.0064   1.0000
  14.000   1.3222   0.05277   0.04787  -0.0117   0.0062   1.0000
  14.250   1.3170   0.05642   0.05162  -0.0118   0.0061   1.0000
  14.500   1.3105   0.06017   0.05546  -0.0120   0.0062   1.0000
  14.750   1.3082   0.06369   0.05908  -0.0126   0.0061   1.0000
  15.000   1.3031   0.06738   0.06286  -0.0129   0.0061   1.0000
  15.250   1.3067   0.07079   0.06637  -0.0147   0.0056   1.0000
  15.500   1.2966   0.07467   0.07034  -0.0141   0.0059   1.0000
  15.750   1.2926   0.07820   0.07394  -0.0143   0.0059   1.0000
  16.000   1.2899   0.08215   0.07799  -0.0158   0.0057   1.0000
  16.250   1.2860   0.08562   0.08155  -0.0158   0.0058   1.0000
  16.500   1.2822   0.08978   0.08580  -0.0173   0.0055   1.0000
  16.750   1.2785   0.09338   0.08950  -0.0177   0.0055   1.0000
  17.000   1.2743   0.09752   0.09372  -0.0191   0.0053   1.0000
  17.250   1.2697   0.10149   0.09779  -0.0199   0.0052   1.0000
  17.500   1.2660   0.10572   0.10209  -0.0217   0.0051   1.0000
  17.750   1.2617   0.10976   0.10623  -0.0228   0.0051   1.0000
  18.000   1.2579   0.11422   0.11074  -0.0250   0.0049   1.0000
  18.250   1.2527   0.11825   0.11489  -0.0259   0.0050   1.0000
  18.500   1.2475   0.12292   0.11962  -0.0281   0.0048   1.0000
  18.750   1.2430   0.12743   0.12421  -0.0301   0.0047   1.0000
  19.000   1.2355   0.13218   0.12908  -0.0318   0.0047   1.0000
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