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NACA 63 (naca633418-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 63 (naca633418-il)
Reynolds number: 200,000
Max Cl/Cd: 67.79 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633418-il-200000-n5.txt
Download as CSV file: xf-naca633418-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63                                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.7562   0.12045   0.11584  -0.0421   1.0000   0.0276
 -18.250  -0.7999   0.10742   0.10252  -0.0501   1.0000   0.0276
 -18.000  -0.8259   0.09869   0.09354  -0.0553   1.0000   0.0277
 -17.750  -0.8448   0.09158   0.08622  -0.0595   1.0000   0.0279
 -17.500  -0.8565   0.08604   0.08051  -0.0625   1.0000   0.0280
 -17.250  -0.8572   0.08251   0.07694  -0.0642   1.0000   0.0284
 -17.000  -0.8597   0.07872   0.07308  -0.0660   1.0000   0.0286
 -16.750  -0.8618   0.07507   0.06935  -0.0678   1.0000   0.0289
 -16.500  -0.8634   0.07158   0.06577  -0.0693   1.0000   0.0292
 -16.250  -0.8646   0.06823   0.06232  -0.0708   1.0000   0.0295
 -16.000  -0.8650   0.06505   0.05904  -0.0720   1.0000   0.0299
 -15.750  -0.8650   0.06203   0.05592  -0.0731   1.0000   0.0303
 -15.500  -0.8638   0.05922   0.05299  -0.0740   1.0000   0.0307
 -15.250  -0.8628   0.05645   0.05008  -0.0748   1.0000   0.0314
 -15.000  -0.8599   0.05399   0.04748  -0.0754   1.0000   0.0319
 -14.750  -0.8565   0.05165   0.04502  -0.0758   1.0000   0.0325
 -14.500  -0.8506   0.04972   0.04308  -0.0759   1.0000   0.0330
 -14.250  -0.8450   0.04782   0.04116  -0.0761   1.0000   0.0336
 -14.000  -0.8390   0.04600   0.03930  -0.0762   1.0000   0.0342
 -13.750  -0.8326   0.04424   0.03748  -0.0761   1.0000   0.0350
 -13.500  -0.8254   0.04258   0.03576  -0.0759   1.0000   0.0356
 -13.250  -0.8180   0.04100   0.03409  -0.0756   1.0000   0.0365
 -13.000  -0.8098   0.03951   0.03251  -0.0752   1.0000   0.0373
 -12.750  -0.8031   0.03800   0.03100  -0.0746   1.0000   0.0380
 -12.500  -0.7964   0.03656   0.02956  -0.0741   1.0000   0.0388
 -12.250  -0.7895   0.03522   0.02821  -0.0734   1.0000   0.0398
 -12.000  -0.7828   0.03396   0.02693  -0.0725   1.0000   0.0409
 -11.750  -0.7742   0.03276   0.02568  -0.0718   0.9987   0.0421
 -11.500  -0.7469   0.03113   0.02400  -0.0750   0.9658   0.0438
 -11.250  -0.7180   0.02962   0.02243  -0.0784   0.9451   0.0456
 -11.000  -0.6893   0.02829   0.02099  -0.0814   0.9270   0.0480
 -10.750  -0.6660   0.02704   0.01964  -0.0832   0.9095   0.0501
 -10.500  -0.6486   0.02588   0.01841  -0.0839   0.8930   0.0523
 -10.250  -0.6325   0.02490   0.01734  -0.0839   0.8789   0.0549
 -10.000  -0.6190   0.02397   0.01631  -0.0833   0.8662   0.0573
  -9.750  -0.6090   0.02302   0.01532  -0.0822   0.8541   0.0599
  -9.500  -0.5975   0.02222   0.01443  -0.0809   0.8436   0.0631
  -9.250  -0.5882   0.02143   0.01356  -0.0793   0.8335   0.0661
  -9.000  -0.5813   0.02072   0.01282  -0.0772   0.8239   0.0694
  -8.750  -0.5683   0.02014   0.01214  -0.0758   0.8156   0.0738
  -8.500  -0.5548   0.01948   0.01147  -0.0745   0.8075   0.0791
  -8.250  -0.5379   0.01895   0.01087  -0.0734   0.7999   0.0855
  -8.000  -0.5209   0.01836   0.01027  -0.0724   0.7934   0.0939
  -7.750  -0.5026   0.01780   0.00973  -0.0716   0.7858   0.1041
  -7.500  -0.4832   0.01725   0.00917  -0.0708   0.7793   0.1172
  -7.250  -0.4631   0.01670   0.00866  -0.0702   0.7729   0.1347
  -7.000  -0.4426   0.01612   0.00815  -0.0697   0.7661   0.1570
  -6.750  -0.4217   0.01551   0.00763  -0.0693   0.7604   0.1870
  -6.500  -0.4005   0.01487   0.00714  -0.0689   0.7542   0.2254
  -6.250  -0.3787   0.01422   0.00669  -0.0687   0.7476   0.2724
  -6.000  -0.3556   0.01368   0.00632  -0.0685   0.7421   0.3228
  -5.750  -0.3306   0.01333   0.00611  -0.0684   0.7365   0.3681
  -5.500  -0.3042   0.01313   0.00597  -0.0684   0.7302   0.4019
  -5.250  -0.2771   0.01300   0.00585  -0.0683   0.7247   0.4269
  -5.000  -0.2495   0.01293   0.00575  -0.0683   0.7194   0.4470
  -4.750  -0.2217   0.01287   0.00568  -0.0684   0.7134   0.4635
  -4.500  -0.1937   0.01284   0.00559  -0.0684   0.7080   0.4781
  -4.250  -0.1654   0.01282   0.00549  -0.0685   0.7031   0.4919
  -4.000  -0.1372   0.01282   0.00546  -0.0686   0.6970   0.5050
  -3.750  -0.1091   0.01283   0.00546  -0.0686   0.6917   0.5161
  -3.500  -0.0805   0.01283   0.00536  -0.0687   0.6871   0.5266
  -3.250  -0.0523   0.01284   0.00537  -0.0688   0.6814   0.5348
  -3.000  -0.0236   0.01282   0.00527  -0.0690   0.6758   0.5428
  -2.750   0.0048   0.01282   0.00525  -0.0690   0.6711   0.5486
  -2.500   0.0335   0.01282   0.00518  -0.0692   0.6666   0.5552
  -2.250   0.0622   0.01280   0.00512  -0.0694   0.6609   0.5612
  -2.000   0.0905   0.01280   0.00511  -0.0695   0.6557   0.5661
  -1.750   0.1193   0.01281   0.00504  -0.0696   0.6514   0.5716
  -1.500   0.1482   0.01281   0.00499  -0.0700   0.6464   0.5776
  -1.250   0.1764   0.01281   0.00502  -0.0700   0.6414   0.5818
  -1.000   0.2050   0.01283   0.00501  -0.0701   0.6368   0.5866
  -0.750   0.2339   0.01285   0.00496  -0.0704   0.6326   0.5921
  -0.500   0.2624   0.01287   0.00497  -0.0706   0.6271   0.5971
  -0.250   0.2906   0.01289   0.00502  -0.0707   0.6223   0.6013
   0.000   0.3193   0.01293   0.00504  -0.0708   0.6182   0.6064
   0.250   0.3482   0.01298   0.00503  -0.0711   0.6141   0.6119
   0.500   0.3764   0.01301   0.00511  -0.0713   0.6088   0.6163
   0.750   0.4044   0.01306   0.00518  -0.0713   0.6040   0.6209
   1.000   0.4331   0.01312   0.00521  -0.0715   0.6000   0.6263
   1.250   0.4619   0.01318   0.00526  -0.0718   0.5959   0.6319
   1.500   0.4896   0.01324   0.00538  -0.0718   0.5908   0.6359
   1.750   0.5176   0.01331   0.00548  -0.0719   0.5861   0.6408
   2.000   0.5462   0.01339   0.00553  -0.0721   0.5821   0.6465
   2.250   0.5745   0.01348   0.00564  -0.0723   0.5776   0.6520
   2.500   0.6018   0.01356   0.00581  -0.0722   0.5725   0.6564
   2.750   0.6297   0.01364   0.00592  -0.0723   0.5678   0.6615
   3.000   0.6584   0.01374   0.00598  -0.0725   0.5638   0.6675
   3.250   0.6853   0.01384   0.00618  -0.0724   0.5585   0.6725
   3.500   0.7124   0.01394   0.00635  -0.0723   0.5531   0.6777
   3.750   0.7403   0.01404   0.00645  -0.0724   0.5484   0.6835
   4.000   0.7680   0.01416   0.00661  -0.0725   0.5434   0.6891
   4.250   0.7942   0.01427   0.00683  -0.0723   0.5376   0.6940
   4.500   0.8213   0.01438   0.00698  -0.0722   0.5322   0.7001
   4.750   0.8489   0.01451   0.00712  -0.0723   0.5269   0.7066
   5.000   0.8742   0.01463   0.00737  -0.0719   0.5202   0.7114
   5.250   0.9006   0.01474   0.00751  -0.0716   0.5138   0.7172
   5.500   0.9264   0.01488   0.00771  -0.0714   0.5059   0.7240
   5.750   0.9513   0.01499   0.00788  -0.0709   0.4976   0.7294
   6.000   0.9759   0.01513   0.00811  -0.0704   0.4894   0.7356
   6.250   1.0009   0.01528   0.00829  -0.0701   0.4802   0.7424
   6.500   1.0236   0.01542   0.00853  -0.0692   0.4692   0.7481
   6.750   1.0455   0.01559   0.00873  -0.0682   0.4555   0.7550
   7.000   1.0666   0.01579   0.00894  -0.0672   0.4400   0.7621
   7.250   1.0860   0.01602   0.00921  -0.0658   0.4244   0.7684
   7.500   1.1054   0.01631   0.00952  -0.0646   0.4086   0.7761
   7.750   1.1226   0.01662   0.00986  -0.0629   0.3910   0.7832
   8.000   1.1375   0.01701   0.01026  -0.0610   0.3704   0.7913
   8.250   1.1477   0.01752   0.01071  -0.0584   0.3468   0.7995
   8.500   1.1516   0.01811   0.01126  -0.0547   0.3222   0.8088
   8.750   1.1522   0.01896   0.01202  -0.0509   0.2972   0.8189
   9.000   1.1528   0.01997   0.01295  -0.0475   0.2716   0.8306
   9.250   1.1507   0.02117   0.01408  -0.0440   0.2476   0.8431
   9.500   1.1496   0.02245   0.01532  -0.0409   0.2240   0.8578
   9.750   1.1476   0.02387   0.01670  -0.0380   0.2028   0.8765
  10.000   1.1457   0.02536   0.01816  -0.0353   0.1833   0.9032
  10.250   1.1464   0.02680   0.01962  -0.0334   0.1650   1.0000
  10.500   1.1496   0.02864   0.02138  -0.0323   0.1473   1.0000
  10.750   1.1532   0.03052   0.02318  -0.0314   0.1321   1.0000
  11.000   1.1567   0.03245   0.02506  -0.0305   0.1186   1.0000
  11.250   1.1604   0.03442   0.02699  -0.0297   0.1069   1.0000
  11.500   1.1642   0.03643   0.02898  -0.0290   0.0972   1.0000
  11.750   1.1673   0.03855   0.03107  -0.0284   0.0890   1.0000
  12.000   1.1726   0.04053   0.03306  -0.0279   0.0818   1.0000
  12.250   1.1764   0.04272   0.03525  -0.0275   0.0759   1.0000
  12.500   1.1811   0.04488   0.03744  -0.0272   0.0708   1.0000
  12.750   1.1851   0.04717   0.03975  -0.0270   0.0665   1.0000
  13.000   1.1901   0.04942   0.04204  -0.0269   0.0625   1.0000
  13.250   1.1927   0.05199   0.04462  -0.0268   0.0594   1.0000
  13.500   1.1986   0.05425   0.04695  -0.0268   0.0565   1.0000
  13.750   1.2028   0.05674   0.04950  -0.0270   0.0539   1.0000
  14.000   1.2044   0.05960   0.05237  -0.0272   0.0516   1.0000
  14.250   1.2103   0.06201   0.05487  -0.0274   0.0494   1.0000
  14.500   1.2143   0.06468   0.05761  -0.0277   0.0474   1.0000
  14.750   1.2169   0.06758   0.06055  -0.0282   0.0458   1.0000
  15.000   1.2191   0.07056   0.06356  -0.0287   0.0443   1.0000
  15.250   1.2238   0.07330   0.06641  -0.0292   0.0427   1.0000
  15.500   1.2278   0.07616   0.06935  -0.0298   0.0411   1.0000
  15.750   1.2302   0.07927   0.07252  -0.0306   0.0399   1.0000
  16.000   1.2313   0.08259   0.07586  -0.0314   0.0389   1.0000
  16.250   1.2354   0.08555   0.07892  -0.0322   0.0377   1.0000
  16.500   1.2393   0.08857   0.08203  -0.0330   0.0366   1.0000
  16.750   1.2422   0.09177   0.08532  -0.0340   0.0355   1.0000
  17.000   1.2446   0.09506   0.08867  -0.0351   0.0346   1.0000
  17.250   1.2461   0.09852   0.09217  -0.0363   0.0338   1.0000
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