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NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(3)-618 (naca633618-il)
Reynolds number: 100,000
Max Cl/Cd: 41.61 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633618-il-100000.txt
Download as CSV file: xf-naca633618-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(3)-618                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.4586   0.09079   0.08570  -0.0754   1.0000   0.0961
 -12.250  -0.4570   0.08790   0.08287  -0.0747   1.0000   0.0969
 -12.000  -0.6602   0.07058   0.06532  -0.0806   1.0000   0.0839
 -11.750  -0.6895   0.06915   0.06395  -0.0763   1.0000   0.0835
 -11.500  -0.7218   0.06785   0.06268  -0.0720   1.0000   0.0832
 -11.250  -0.7543   0.06663   0.06147  -0.0677   1.0000   0.0828
 -11.000  -0.7752   0.06278   0.05738  -0.0695   0.9936   0.0826
 -10.750  -0.7789   0.05752   0.05167  -0.0735   0.9837   0.0827
 -10.500  -0.7772   0.05298   0.04662  -0.0761   0.9738   0.0832
 -10.250  -0.7674   0.04897   0.04204  -0.0785   0.9658   0.0845
 -10.000  -0.7391   0.04675   0.03997  -0.0801   0.9594   0.0877
  -9.750  -0.7104   0.04405   0.03695  -0.0831   0.9540   0.0906
  -9.500  -0.6968   0.04194   0.03445  -0.0830   0.9447   0.0930
  -9.250  -0.6679   0.03938   0.03139  -0.0855   0.9390   0.0964
  -9.000  -0.6436   0.03777   0.02981  -0.0859   0.9320   0.0997
  -8.750  -0.6147   0.03636   0.02823  -0.0871   0.9253   0.1040
  -8.500  -0.5755   0.03458   0.02608  -0.0900   0.9213   0.1087
  -8.250  -0.5562   0.03347   0.02510  -0.0891   0.9130   0.1128
  -8.000  -0.5230   0.03236   0.02385  -0.0906   0.9073   0.1188
  -7.750  -0.4803   0.03088   0.02240  -0.0934   0.9040   0.1260
  -7.500  -0.4651   0.03034   0.02185  -0.0918   0.8949   0.1323
  -7.250  -0.4316   0.02923   0.02082  -0.0930   0.8896   0.1418
  -7.000  -0.3903   0.02801   0.01974  -0.0957   0.8864   0.1582
  -6.750  -0.3825   0.02755   0.01939  -0.0930   0.8766   0.1718
  -6.500  -0.3539   0.02621   0.01838  -0.0942   0.8710   0.2074
  -6.250  -0.3203   0.02408   0.01720  -0.0974   0.8675   0.3252
  -6.000  -0.3143   0.02427   0.01774  -0.0944   0.8568   0.4055
  -5.750  -0.2779   0.02478   0.01827  -0.0952   0.8520   0.4632
  -5.500  -0.2356   0.02542   0.01884  -0.0965   0.8489   0.4984
  -5.250  -0.2303   0.02629   0.01970  -0.0926   0.8379   0.5152
  -5.000  -0.1969   0.02713   0.02050  -0.0920   0.8333   0.5361
  -4.750  -0.1584   0.02798   0.02132  -0.0918   0.8304   0.5555
  -4.500  -0.1573   0.02885   0.02215  -0.0875   0.8192   0.5682
  -4.250  -0.1246   0.02948   0.02272  -0.0868   0.8148   0.5848
  -4.000  -0.0883   0.03024   0.02345  -0.0858   0.8121   0.5977
  -3.750  -0.0927   0.03110   0.02431  -0.0810   0.8007   0.6063
  -3.500  -0.0590   0.03119   0.02427  -0.0815   0.7965   0.6209
  -3.250  -0.0249   0.03176   0.02483  -0.0798   0.7938   0.6286
  -3.000  -0.0290   0.03233   0.02534  -0.0765   0.7823   0.6406
  -2.750  -0.0036   0.03286   0.02587  -0.0741   0.7782   0.6484
  -2.500   0.0358   0.03253   0.02540  -0.0758   0.7757   0.6604
  -2.250   0.0247   0.03355   0.02647  -0.0703   0.7641   0.6659
  -2.000   0.0620   0.03311   0.02588  -0.0728   0.7602   0.6775
  -1.750   0.0947   0.03306   0.02580  -0.0720   0.7577   0.6829
  -1.500   0.0825   0.03415   0.02690  -0.0679   0.7463   0.6906
  -1.250   0.1162   0.03389   0.02655  -0.0690   0.7424   0.6985
  -1.000   0.1529   0.03361   0.02621  -0.0695   0.7399   0.7050
  -0.750   0.1424   0.03482   0.02740  -0.0670   0.7284   0.7142
  -0.500   0.1672   0.03488   0.02745  -0.0658   0.7245   0.7192
  -0.250   0.2080   0.03454   0.02704  -0.0675   0.7222   0.7269
   0.000   0.2445   0.03433   0.02676  -0.0693   0.7190   0.7344
   0.250   0.2171   0.03615   0.02865  -0.0631   0.7065   0.7399
   0.500   0.2612   0.03581   0.02824  -0.0658   0.7044   0.7482
   0.750   0.3045   0.03533   0.02772  -0.0676   0.7028   0.7542
   1.000   0.2668   0.03790   0.03036  -0.0612   0.6889   0.7605
   1.250   0.3115   0.03755   0.02995  -0.0640   0.6866   0.7689
   1.500   0.3498   0.03709   0.02949  -0.0644   0.6850   0.7746
   1.750   0.3186   0.04004   0.03249  -0.0601   0.6716   0.7820
   2.000   0.3565   0.03975   0.03219  -0.0613   0.6690   0.7893
   2.250   0.3436   0.04197   0.03445  -0.0582   0.6595   0.7966
   2.500   0.3700   0.04243   0.03490  -0.0590   0.6543   0.8048
   2.750   0.4019   0.04220   0.03469  -0.0589   0.6514   0.8117
   3.000   0.4486   0.04167   0.03414  -0.0611   0.6496   0.8207
   3.250   0.4135   0.04494   0.03749  -0.0562   0.6368   0.8283
   3.500   0.4522   0.04477   0.03733  -0.0576   0.6339   0.8380
   3.750   0.4391   0.04692   0.03955  -0.0544   0.6245   0.8461
   4.000   0.4617   0.04752   0.04017  -0.0546   0.6191   0.8559
   4.250   0.4941   0.04712   0.03980  -0.0541   0.6161   0.8662
   4.500   0.5357   0.04633   0.03905  -0.0545   0.6142   0.8767
   4.750   0.5052   0.04992   0.04270  -0.0515   0.6010   0.8886
   5.000   0.5415   0.04929   0.04210  -0.0514   0.5982   0.9017
   5.250   0.5212   0.05208   0.04497  -0.0486   0.5865   0.9166
   5.500   0.5506   0.05169   0.04464  -0.0480   0.5824   0.9344
   5.750   0.5950   0.05070   0.04373  -0.0488   0.5801   0.9562
   6.000   0.5898   0.05390   0.04702  -0.0500   0.5665   1.0000
   6.250   0.6453   0.05323   0.04638  -0.0533   0.5636   1.0000
   6.500   0.6458   0.05637   0.04957  -0.0547   0.5507   1.0000
   6.750   0.6985   0.05562   0.04886  -0.0574   0.5472   1.0000
   7.000   0.7016   0.05860   0.05188  -0.0586   0.5349   1.0000
   7.250   0.7517   0.05771   0.05104  -0.0607   0.5307   1.0000
   7.500   0.8114   0.05580   0.04920  -0.0627   0.5286   1.0000
   7.750   0.8056   0.05923   0.05267  -0.0629   0.5142   1.0000
   8.000   0.8144   0.06144   0.05492  -0.0633   0.5026   1.0000
   8.250   0.8599   0.06015   0.05370  -0.0642   0.4977   1.0000
   8.500   0.8737   0.06173   0.05533  -0.0643   0.4872   1.0000
   8.750   0.9150   0.06043   0.05411  -0.0647   0.4814   1.0000
   9.000   0.9756   0.05688   0.05067  -0.0651   0.4795   1.0000
   9.250   1.0463   0.05178   0.04569  -0.0654   0.4793   1.0000
   9.500   1.1361   0.04487   0.03893  -0.0665   0.4800   1.0000
   9.750   1.3197   0.03242   0.02652  -0.0759   0.4761   1.0000
  10.000   1.3344   0.03207   0.02620  -0.0738   0.4615   1.0000
  10.250   1.3372   0.03255   0.02674  -0.0708   0.4468   1.0000
  10.500   1.3464   0.03276   0.02699  -0.0686   0.4311   1.0000
  10.750   1.3540   0.03320   0.02746  -0.0664   0.4145   1.0000
  11.000   1.3601   0.03385   0.02812  -0.0643   0.3965   1.0000
  11.250   1.3649   0.03471   0.02895  -0.0623   0.3768   1.0000
  11.500   1.3567   0.03677   0.03104  -0.0598   0.3560   1.0000
  11.750   1.3548   0.03849   0.03268  -0.0578   0.3325   1.0000
  12.000   1.3502   0.04063   0.03471  -0.0560   0.3077   1.0000
  12.250   1.3442   0.04305   0.03694  -0.0543   0.2822   1.0000
  12.500   1.3345   0.04606   0.03984  -0.0528   0.2572   1.0000
  12.750   1.3260   0.04909   0.04264  -0.0514   0.2334   1.0000
  13.000   1.3158   0.05260   0.04602  -0.0505   0.2104   1.0000
  13.250   1.3075   0.05605   0.04927  -0.0497   0.1895   1.0000
  13.500   1.3019   0.05935   0.05234  -0.0490   0.1703   1.0000
  13.750   1.2985   0.06262   0.05549  -0.0485   0.1532   1.0000
  14.000   1.2994   0.06550   0.05823  -0.0480   0.1387   1.0000
  14.250   1.3046   0.06795   0.06054  -0.0475   0.1267   1.0000
  14.500   1.3119   0.07024   0.06274  -0.0472   0.1170   1.0000
  14.750   1.3204   0.07256   0.06513  -0.0468   0.1090   1.0000
  15.000   1.3373   0.07391   0.06632  -0.0462   0.1019   1.0000
  15.250   1.3430   0.07661   0.06917  -0.0462   0.0965   1.0000
  15.500   1.3661   0.07750   0.06988  -0.0455   0.0907   1.0000
  15.750   1.3673   0.08076   0.07340  -0.0457   0.0871   1.0000
  16.000   1.3803   0.08266   0.07528  -0.0456   0.0829   1.0000
  16.250   1.3953   0.08472   0.07738  -0.0454   0.0792   1.0000
  16.500   1.3942   0.08832   0.08123  -0.0459   0.0766   1.0000
  16.750   1.4002   0.09111   0.08412  -0.0462   0.0738   1.0000
  17.000   1.4227   0.09255   0.08546  -0.0458   0.0705   1.0000
  17.250   1.4100   0.09751   0.09078  -0.0470   0.0693   1.0000
  17.500   1.3995   0.10246   0.09602  -0.0483   0.0679   1.0000
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