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DF 101 AIRFOIL (df101-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DF 101 AIRFOIL (df101-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.2 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-df101-il-1000000-n5.txt
Download as CSV file: xf-df101-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DF 101 AIRFOIL                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.7215   0.10930   0.10723  -0.0240   1.0000   0.0036
 -15.000  -0.7454   0.10025   0.09810  -0.0284   1.0000   0.0035
 -14.750  -0.7732   0.09093   0.08870  -0.0332   1.0000   0.0035
 -14.500  -0.8059   0.08129   0.07898  -0.0384   1.0000   0.0034
 -14.250  -0.8350   0.07255   0.07015  -0.0434   1.0000   0.0034
 -14.000  -0.8806   0.06114   0.05861  -0.0504   1.0000   0.0034
 -13.750  -0.9132   0.05131   0.04863  -0.0571   1.0000   0.0034
 -13.500  -0.9361   0.04172   0.03885  -0.0657   1.0000   0.0034
 -13.250  -0.9540   0.03509   0.03201  -0.0720   1.0000   0.0034
 -13.000  -0.9731   0.03142   0.02815  -0.0721   1.0000   0.0034
 -12.750  -0.9777   0.02980   0.02643  -0.0697   1.0000   0.0034
 -12.500  -0.9821   0.02837   0.02488  -0.0664   1.0000   0.0034
 -12.250  -0.9812   0.02679   0.02316  -0.0638   1.0000   0.0034
 -12.000  -0.9756   0.02554   0.02180  -0.0614   1.0000   0.0034
 -11.750  -0.9684   0.02443   0.02057  -0.0589   1.0000   0.0035
 -11.500  -0.9507   0.02280   0.01876  -0.0589   0.9967   0.0035
 -11.250  -0.9305   0.02102   0.01678  -0.0593   0.9906   0.0036
 -11.000  -0.9057   0.01971   0.01531  -0.0601   0.9864   0.0037
 -10.750  -0.8776   0.01868   0.01417  -0.0612   0.9834   0.0039
 -10.500  -0.8511   0.01777   0.01316  -0.0617   0.9785   0.0040
 -10.250  -0.8228   0.01697   0.01227  -0.0625   0.9738   0.0041
 -10.000  -0.7934   0.01629   0.01149  -0.0635   0.9695   0.0042
  -9.750  -0.7676   0.01570   0.01083  -0.0635   0.9627   0.0044
  -9.500  -0.7408   0.01513   0.01018  -0.0637   0.9566   0.0046
  -9.250  -0.7166   0.01462   0.00960  -0.0632   0.9494   0.0048
  -9.000  -0.6921   0.01413   0.00902  -0.0628   0.9426   0.0050
  -8.750  -0.6680   0.01369   0.00850  -0.0622   0.9358   0.0052
  -8.500  -0.6441   0.01322   0.00794  -0.0616   0.9289   0.0053
  -8.250  -0.6196   0.01282   0.00746  -0.0611   0.9225   0.0055
  -8.000  -0.5957   0.01232   0.00687  -0.0604   0.9156   0.0057
  -7.750  -0.5715   0.01183   0.00631  -0.0598   0.9092   0.0061
  -7.500  -0.5465   0.01146   0.00588  -0.0593   0.9025   0.0064
  -7.250  -0.5211   0.01113   0.00549  -0.0588   0.8962   0.0068
  -7.000  -0.4954   0.01082   0.00513  -0.0584   0.8894   0.0073
  -6.750  -0.4696   0.01054   0.00478  -0.0579   0.8828   0.0077
  -6.500  -0.4435   0.01026   0.00446  -0.0576   0.8758   0.0082
  -6.250  -0.4176   0.00998   0.00414  -0.0572   0.8687   0.0094
  -6.000  -0.3911   0.00975   0.00388  -0.0569   0.8614   0.0108
  -5.750  -0.3648   0.00952   0.00361  -0.0565   0.8536   0.0126
  -5.500  -0.3381   0.00931   0.00338  -0.0563   0.8457   0.0145
  -5.250  -0.3114   0.00913   0.00314  -0.0560   0.8376   0.0162
  -5.000  -0.2847   0.00893   0.00291  -0.0557   0.8287   0.0185
  -4.750  -0.2578   0.00878   0.00272  -0.0554   0.8200   0.0203
  -4.500  -0.2312   0.00858   0.00250  -0.0551   0.8102   0.0244
  -4.250  -0.2045   0.00839   0.00231  -0.0548   0.8004   0.0317
  -4.000  -0.1783   0.00812   0.00208  -0.0545   0.7903   0.0503
  -3.750  -0.1527   0.00780   0.00187  -0.0541   0.7795   0.0849
  -3.500  -0.1266   0.00754   0.00170  -0.0538   0.7682   0.1175
  -3.250  -0.1000   0.00737   0.00157  -0.0535   0.7565   0.1409
  -3.000  -0.0732   0.00724   0.00146  -0.0532   0.7445   0.1629
  -2.750  -0.0465   0.00713   0.00137  -0.0530   0.7319   0.1834
  -2.500  -0.0197   0.00705   0.00130  -0.0527   0.7183   0.2035
  -2.250   0.0070   0.00696   0.00123  -0.0524   0.7041   0.2261
  -2.000   0.0339   0.00690   0.00117  -0.0522   0.6890   0.2447
  -1.750   0.0608   0.00688   0.00113  -0.0519   0.6730   0.2588
  -1.500   0.0877   0.00688   0.00108  -0.0517   0.6550   0.2700
  -1.250   0.1144   0.00690   0.00105  -0.0514   0.6347   0.2831
  -1.000   0.1412   0.00691   0.00102  -0.0511   0.6167   0.2963
  -0.750   0.1682   0.00691   0.00100  -0.0509   0.6014   0.3117
  -0.500   0.1952   0.00690   0.00099  -0.0507   0.5866   0.3289
  -0.250   0.2221   0.00689   0.00098  -0.0504   0.5720   0.3489
   0.000   0.2490   0.00688   0.00099  -0.0502   0.5571   0.3699
   0.250   0.2757   0.00686   0.00099  -0.0500   0.5422   0.3975
   0.500   0.3023   0.00684   0.00101  -0.0497   0.5262   0.4276
   0.750   0.3286   0.00682   0.00103  -0.0494   0.5095   0.4637
   1.000   0.3545   0.00677   0.00107  -0.0491   0.4925   0.5105
   1.250   0.3803   0.00676   0.00112  -0.0487   0.4739   0.5556
   1.500   0.4058   0.00675   0.00117  -0.0482   0.4538   0.6033
   1.750   0.4311   0.00673   0.00124  -0.0477   0.4350   0.6538
   2.000   0.4557   0.00673   0.00131  -0.0470   0.4139   0.7066
   2.250   0.4788   0.00670   0.00141  -0.0461   0.3892   0.7739
   2.500   0.5002   0.00664   0.00153  -0.0446   0.3674   0.8586
   2.750   0.5244   0.00672   0.00168  -0.0436   0.3462   0.9150
   3.000   0.5521   0.00692   0.00182  -0.0435   0.3218   0.9427
   3.250   0.5833   0.00713   0.00195  -0.0443   0.2993   0.9589
   3.500   0.6148   0.00735   0.00209  -0.0452   0.2806   0.9699
   3.750   0.6489   0.00758   0.00223  -0.0467   0.2603   0.9766
   4.000   0.6799   0.00779   0.00237  -0.0475   0.2452   0.9830
   4.250   0.7146   0.00801   0.00253  -0.0491   0.2295   0.9868
   4.500   0.7503   0.00823   0.00269  -0.0510   0.2168   0.9939
   4.750   0.7936   0.00846   0.00287  -0.0545   0.2041   1.0000
   5.250   0.8389   0.00882   0.00318  -0.0525   0.1867   1.0000
   5.500   0.8616   0.00902   0.00335  -0.0515   0.1788   1.0000
   5.750   0.8844   0.00922   0.00352  -0.0505   0.1703   1.0000
   6.000   0.9072   0.00943   0.00371  -0.0496   0.1616   1.0000
   6.250   0.9291   0.00971   0.00392  -0.0485   0.1476   1.0000
   6.500   0.9512   0.00998   0.00414  -0.0475   0.1360   1.0000
   6.750   0.9733   0.01027   0.00437  -0.0464   0.1251   1.0000
   7.000   0.9953   0.01057   0.00463  -0.0454   0.1131   1.0000
   7.250   1.0170   0.01090   0.00490  -0.0444   0.1007   1.0000
   7.500   1.0388   0.01123   0.00519  -0.0433   0.0896   1.0000
   7.750   1.0601   0.01161   0.00551  -0.0423   0.0776   1.0000
   8.000   1.0804   0.01207   0.00589  -0.0410   0.0639   1.0000
   8.250   1.1006   0.01253   0.00629  -0.0398   0.0516   1.0000
   8.500   1.1202   0.01303   0.00672  -0.0385   0.0398   1.0000
   8.750   1.1393   0.01356   0.00720  -0.0372   0.0292   1.0000
   9.000   1.1577   0.01413   0.00772  -0.0357   0.0206   1.0000
   9.250   1.1766   0.01464   0.00821  -0.0344   0.0157   1.0000
   9.500   1.1962   0.01508   0.00868  -0.0331   0.0134   1.0000
   9.750   1.2151   0.01556   0.00916  -0.0317   0.0119   1.0000
  10.000   1.2336   0.01603   0.00966  -0.0303   0.0106   1.0000
  10.250   1.2521   0.01647   0.01014  -0.0289   0.0101   1.0000
  10.500   1.2685   0.01693   0.01064  -0.0271   0.0096   1.0000
  10.750   1.2831   0.01742   0.01117  -0.0250   0.0092   1.0000
  11.000   1.2971   0.01793   0.01173  -0.0229   0.0088   1.0000
  11.250   1.3099   0.01853   0.01238  -0.0207   0.0084   1.0000
  11.500   1.3215   0.01923   0.01313  -0.0184   0.0080   1.0000
  11.750   1.3339   0.01989   0.01386  -0.0164   0.0078   1.0000
  12.000   1.3474   0.02051   0.01453  -0.0146   0.0076   1.0000
  12.250   1.3599   0.02119   0.01527  -0.0128   0.0073   1.0000
  12.500   1.3725   0.02189   0.01602  -0.0111   0.0070   1.0000
  12.750   1.3848   0.02263   0.01680  -0.0095   0.0065   1.0000
  13.000   1.3936   0.02363   0.01790  -0.0075   0.0066   1.0000
  13.250   1.4030   0.02462   0.01893  -0.0058   0.0062   1.0000
  13.500   1.4114   0.02572   0.02009  -0.0042   0.0060   1.0000
  13.750   1.4181   0.02699   0.02144  -0.0025   0.0058   1.0000
  14.000   1.4222   0.02851   0.02303  -0.0009   0.0054   1.0000
  14.250   1.4288   0.02992   0.02453   0.0003   0.0054   1.0000
  14.500   1.4352   0.03141   0.02609   0.0014   0.0053   1.0000
  14.750   1.4406   0.03304   0.02781   0.0024   0.0052   1.0000
  15.000   1.4433   0.03501   0.02988   0.0033   0.0051   1.0000
  15.250   1.4483   0.03684   0.03178   0.0039   0.0050   1.0000
  15.500   1.4507   0.03902   0.03406   0.0043   0.0048   1.0000
  15.750   1.4514   0.04148   0.03662   0.0045   0.0047   1.0000
  16.000   1.4508   0.04418   0.03941   0.0046   0.0047   1.0000
  16.250   1.4481   0.04726   0.04260   0.0043   0.0046   1.0000
  16.500   1.4467   0.05033   0.04577   0.0038   0.0045   1.0000
  16.750   1.4397   0.05425   0.04981   0.0029   0.0045   1.0000
  17.000   1.4343   0.05813   0.05378   0.0018   0.0043   1.0000
  17.250   1.4256   0.06264   0.05841   0.0003   0.0043   1.0000
  17.500   1.4132   0.06788   0.06378  -0.0016   0.0043   1.0000
  17.750   1.4025   0.07305   0.06907  -0.0037   0.0042   1.0000
  18.000   1.3885   0.07897   0.07510  -0.0063   0.0041   1.0000
  18.250   1.3718   0.08551   0.08177  -0.0093   0.0041   1.0000
  18.500   1.3513   0.09295   0.08935  -0.0129   0.0041   1.0000
  18.750   1.3304   0.10068   0.09722  -0.0168   0.0040   1.0000
  19.000   1.3086   0.10876   0.10542  -0.0209   0.0040   1.0000
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