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NACA 63(2)-615 (naca632615-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(2)-615 (naca632615-il)
Reynolds number: 100,000
Max Cl/Cd: 55.59 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca632615-il-100000-n5.txt
Download as CSV file: xf-naca632615-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)-615                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.4633   0.08418   0.07881  -0.0694   1.0000   0.0368
 -11.750  -0.4953   0.07516   0.06976  -0.0749   1.0000   0.0365
 -11.500  -0.5250   0.06837   0.06293  -0.0788   1.0000   0.0362
 -11.250  -0.5573   0.06292   0.05741  -0.0810   1.0000   0.0361
 -11.000  -0.5844   0.05950   0.05395  -0.0806   1.0000   0.0359
 -10.750  -0.6149   0.05741   0.05186  -0.0777   1.0000   0.0358
 -10.500  -0.6373   0.05374   0.04798  -0.0792   0.9913   0.0358
 -10.250  -0.6395   0.04810   0.04178  -0.0849   0.9765   0.0364
 -10.000  -0.6329   0.04359   0.03667  -0.0881   0.9651   0.0370
  -9.750  -0.6077   0.04132   0.03429  -0.0906   0.9594   0.0381
  -9.500  -0.5861   0.03950   0.03232  -0.0921   0.9509   0.0395
  -9.250  -0.5588   0.03701   0.02945  -0.0948   0.9459   0.0415
  -9.000  -0.5391   0.03463   0.02658  -0.0955   0.9368   0.0432
  -8.750  -0.5095   0.03262   0.02439  -0.0974   0.9319   0.0448
  -8.500  -0.4838   0.03139   0.02307  -0.0982   0.9246   0.0469
  -8.250  -0.4555   0.02997   0.02141  -0.0992   0.9182   0.0495
  -8.000  -0.4229   0.02840   0.01956  -0.1007   0.9140   0.0518
  -7.750  -0.3998   0.02738   0.01859  -0.1006   0.9054   0.0541
  -7.500  -0.3695   0.02635   0.01744  -0.1016   0.8998   0.0574
  -7.250  -0.3416   0.02540   0.01629  -0.1019   0.8934   0.0604
  -7.000  -0.3167   0.02446   0.01543  -0.1020   0.8858   0.0636
  -6.750  -0.2861   0.02360   0.01450  -0.1029   0.8808   0.0679
  -6.500  -0.2642   0.02293   0.01376  -0.1022   0.8721   0.0716
  -6.250  -0.2368   0.02216   0.01300  -0.1027   0.8660   0.0769
  -6.000  -0.2116   0.02156   0.01231  -0.1026   0.8588   0.0827
  -5.750  -0.1869   0.02085   0.01162  -0.1027   0.8515   0.0906
  -5.500  -0.1574   0.02011   0.01087  -0.1035   0.8465   0.1031
  -5.250  -0.1352   0.01952   0.01034  -0.1031   0.8377   0.1210
  -5.000  -0.1074   0.01866   0.00965  -0.1039   0.8318   0.1625
  -4.750  -0.0820   0.01768   0.00909  -0.1046   0.8251   0.2486
  -4.500  -0.0567   0.01694   0.00889  -0.1050   0.8180   0.3679
  -4.250  -0.0270   0.01673   0.00885  -0.1053   0.8129   0.4450
  -4.000  -0.0015   0.01678   0.00893  -0.1048   0.8053   0.4899
  -3.750   0.0264   0.01686   0.00899  -0.1045   0.7991   0.5255
  -3.500   0.0559   0.01697   0.00901  -0.1044   0.7941   0.5561
  -3.250   0.0799   0.01718   0.00922  -0.1034   0.7863   0.5764
  -3.000   0.1079   0.01728   0.00924  -0.1030   0.7807   0.5943
  -2.750   0.1349   0.01739   0.00928  -0.1026   0.7746   0.6100
  -2.500   0.1606   0.01749   0.00932  -0.1020   0.7677   0.6221
  -2.250   0.1893   0.01748   0.00922  -0.1019   0.7626   0.6310
  -2.000   0.2163   0.01751   0.00917  -0.1018   0.7560   0.6407
  -1.750   0.2427   0.01754   0.00915  -0.1014   0.7496   0.6481
  -1.500   0.2726   0.01750   0.00900  -0.1016   0.7449   0.6567
  -1.250   0.2981   0.01757   0.00905  -0.1013   0.7378   0.6641
  -1.000   0.3253   0.01758   0.00902  -0.1011   0.7318   0.6714
  -0.750   0.3561   0.01753   0.00886  -0.1016   0.7274   0.6795
  -0.500   0.3797   0.01766   0.00901  -0.1009   0.7201   0.6858
  -0.250   0.4087   0.01766   0.00895  -0.1012   0.7144   0.6941
   0.000   0.4373   0.01765   0.00890  -0.1011   0.7099   0.7004
   0.250   0.4615   0.01779   0.00907  -0.1006   0.7027   0.7079
   0.500   0.4898   0.01782   0.00907  -0.1007   0.6973   0.7153
   0.750   0.5175   0.01785   0.00907  -0.1005   0.6926   0.7222
   1.000   0.5431   0.01800   0.00925  -0.1004   0.6855   0.7307
   1.250   0.5694   0.01805   0.00932  -0.1000   0.6803   0.7372
   1.500   0.5983   0.01811   0.00935  -0.1002   0.6755   0.7456
   1.750   0.6213   0.01829   0.00960  -0.0994   0.6685   0.7527
   2.000   0.6493   0.01835   0.00968  -0.0994   0.6634   0.7610
   2.250   0.6762   0.01844   0.00978  -0.0992   0.6584   0.7687
   2.500   0.6998   0.01864   0.01006  -0.0986   0.6515   0.7773
   2.750   0.7270   0.01871   0.01016  -0.0984   0.6464   0.7854
   3.000   0.7532   0.01884   0.01033  -0.0981   0.6410   0.7943
   3.250   0.7762   0.01904   0.01062  -0.0974   0.6342   0.8029
   3.500   0.8041   0.01910   0.01071  -0.0973   0.6291   0.8125
   3.750   0.8268   0.01928   0.01099  -0.0964   0.6228   0.8214
   4.000   0.8513   0.01946   0.01125  -0.0959   0.6162   0.8319
   4.250   0.8779   0.01947   0.01129  -0.0954   0.6113   0.8416
   4.500   0.8976   0.01974   0.01171  -0.0941   0.6038   0.8525
   4.750   0.9222   0.01983   0.01187  -0.0934   0.5976   0.8644
   5.000   0.9451   0.01992   0.01206  -0.0924   0.5914   0.8767
   5.250   0.9641   0.02008   0.01235  -0.0908   0.5835   0.8906
   5.500   0.9896   0.01999   0.01230  -0.0900   0.5771   0.9059
   5.750   1.0059   0.02016   0.01265  -0.0881   0.5673   0.9266
   6.000   1.0322   0.02008   0.01264  -0.0877   0.5586   0.9536
   6.250   1.0615   0.02017   0.01282  -0.0883   0.5476   1.0000
   6.500   1.0875   0.02042   0.01318  -0.0884   0.5359   1.0000
   6.750   1.1143   0.02057   0.01338  -0.0885   0.5235   1.0000
   7.000   1.1398   0.02073   0.01358  -0.0884   0.5095   1.0000
   7.250   1.1628   0.02096   0.01386  -0.0878   0.4938   1.0000
   7.500   1.1818   0.02126   0.01423  -0.0866   0.4742   1.0000
   7.750   1.1988   0.02157   0.01452  -0.0850   0.4502   1.0000
   8.000   1.2120   0.02205   0.01498  -0.0830   0.4224   1.0000
   8.250   1.2219   0.02264   0.01550  -0.0805   0.3919   1.0000
   8.500   1.2294   0.02344   0.01618  -0.0778   0.3584   1.0000
   8.750   1.2334   0.02453   0.01708  -0.0749   0.3226   1.0000
   9.000   1.2343   0.02593   0.01829  -0.0720   0.2863   1.0000
   9.250   1.2333   0.02763   0.01980  -0.0693   0.2513   1.0000
   9.500   1.2310   0.02958   0.02158  -0.0668   0.2192   1.0000
   9.750   1.2288   0.03170   0.02356  -0.0647   0.1904   1.0000
  10.000   1.2267   0.03398   0.02570  -0.0628   0.1649   1.0000
  10.250   1.2258   0.03630   0.02792  -0.0613   0.1420   1.0000
  10.500   1.2246   0.03876   0.03029  -0.0599   0.1234   1.0000
  10.750   1.2246   0.04122   0.03270  -0.0588   0.1072   1.0000
  11.000   1.2248   0.04376   0.03520  -0.0578   0.0951   1.0000
  11.250   1.2253   0.04635   0.03779  -0.0570   0.0856   1.0000
  11.500   1.2275   0.04885   0.04033  -0.0563   0.0781   1.0000
  11.750   1.2276   0.05162   0.04308  -0.0557   0.0725   1.0000
  12.000   1.2312   0.05410   0.04566  -0.0552   0.0671   1.0000
  12.250   1.2317   0.05698   0.04854  -0.0549   0.0634   1.0000
  12.500   1.2363   0.05947   0.05113  -0.0545   0.0595   1.0000
  12.750   1.2396   0.06216   0.05389  -0.0544   0.0561   1.0000
  13.000   1.2418   0.06502   0.05677  -0.0543   0.0534   1.0000
  13.250   1.2477   0.06753   0.05942  -0.0542   0.0504   1.0000
  13.500   1.2516   0.07031   0.06226  -0.0543   0.0479   1.0000
  13.750   1.2546   0.07322   0.06516  -0.0544   0.0458   1.0000
  14.000   1.2613   0.07577   0.06789  -0.0544   0.0436   1.0000
  14.250   1.2665   0.07852   0.07075  -0.0546   0.0416   1.0000
  14.500   1.2707   0.08140   0.07369  -0.0549   0.0400   1.0000
  14.750   1.2765   0.08409   0.07639  -0.0550   0.0386   1.0000
  15.000   1.2826   0.08690   0.07942  -0.0553   0.0371   1.0000
  15.250   1.2872   0.08992   0.08259  -0.0557   0.0356   1.0000
  15.500   1.2910   0.09304   0.08582  -0.0563   0.0344   1.0000
  15.750   1.2952   0.09607   0.08889  -0.0570   0.0334   1.0000
  16.000   1.3003   0.09901   0.09189  -0.0575   0.0324   1.0000
  16.250   1.3011   0.10286   0.09602  -0.0585   0.0316   1.0000
  16.500   1.3014   0.10682   0.10021  -0.0597   0.0308   1.0000
  16.750   1.3003   0.11103   0.10462  -0.0612   0.0302   1.0000
  17.000   1.2979   0.11552   0.10932  -0.0630   0.0296   1.0000
  17.250   1.2944   0.12024   0.11422  -0.0650   0.0292   1.0000
  17.500   1.2897   0.12525   0.11942  -0.0675   0.0288   1.0000
  17.750   1.2839   0.13057   0.12491  -0.0703   0.0284   1.0000
  18.000   1.2768   0.13624   0.13077  -0.0735   0.0282   1.0000
  18.250   1.2685   0.14229   0.13698  -0.0771   0.0279   1.0000
  18.500   1.2577   0.14910   0.14398  -0.0814   0.0277   1.0000
  18.750   1.2422   0.15729   0.15238  -0.0870   0.0276   1.0000
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