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NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(3)-018 (naca633018-il)
Reynolds number: 200,000
Max Cl/Cd: 53.25 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633018-il-200000.txt
Download as CSV file: xf-naca633018-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(3)-018                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.0786   0.09164   0.08685  -0.0227   1.0000   0.0476
 -17.500  -1.0941   0.08604   0.08106  -0.0255   1.0000   0.0484
 -17.250  -1.1099   0.08066   0.07546  -0.0279   1.0000   0.0492
 -17.000  -1.1254   0.07570   0.07027  -0.0299   1.0000   0.0501
 -16.750  -1.1405   0.07116   0.06548  -0.0316   1.0000   0.0509
 -16.500  -1.1550   0.06715   0.06122  -0.0329   1.0000   0.0515
 -16.250  -1.1434   0.06453   0.05861  -0.0329   1.0000   0.0534
 -16.000  -1.1369   0.06256   0.05665  -0.0333   1.0000   0.0550
 -15.750  -1.1360   0.06002   0.05401  -0.0337   1.0000   0.0562
 -15.500  -1.1357   0.05754   0.05139  -0.0341   1.0000   0.0576
 -15.250  -1.1379   0.05501   0.04870  -0.0343   1.0000   0.0590
 -15.000  -1.1412   0.05256   0.04605  -0.0343   1.0000   0.0602
 -14.500  -1.1195   0.04860   0.04200  -0.0340   1.0000   0.0640
 -14.250  -1.1102   0.04702   0.04038  -0.0338   1.0000   0.0658
 -14.000  -1.1028   0.04535   0.03860  -0.0335   1.0000   0.0676
 -13.750  -1.0934   0.04373   0.03687  -0.0332   1.0000   0.0692
 -13.500  -1.0843   0.04214   0.03512  -0.0327   1.0000   0.0706
 -13.250  -1.0746   0.04067   0.03348  -0.0322   1.0000   0.0716
 -13.000  -1.0427   0.03944   0.03233  -0.0320   1.0000   0.0744
 -12.750  -1.0253   0.03832   0.03121  -0.0317   1.0000   0.0764
 -12.500  -1.0088   0.03718   0.03004  -0.0313   1.0000   0.0783
 -12.250  -0.9919   0.03607   0.02887  -0.0308   1.0000   0.0802
 -12.000  -0.9764   0.03495   0.02765  -0.0303   1.0000   0.0821
 -11.750  -0.9575   0.03393   0.02661  -0.0297   1.0000   0.0845
 -11.500  -0.9406   0.03285   0.02561  -0.0291   1.0000   0.0874
 -11.250  -0.9264   0.03172   0.02450  -0.0285   1.0000   0.0901
 -11.000  -0.9121   0.03062   0.02337  -0.0280   1.0000   0.0932
 -10.750  -0.8977   0.02954   0.02223  -0.0274   1.0000   0.0963
 -10.500  -0.8890   0.02807   0.02090  -0.0266   1.0000   0.1007
 -10.250  -0.8778   0.02681   0.01966  -0.0260   1.0000   0.1057
 -10.000  -0.8681   0.02545   0.01832  -0.0255   1.0000   0.1119
  -9.750  -0.8603   0.02400   0.01696  -0.0250   1.0000   0.1198
  -9.500  -0.8550   0.02249   0.01556  -0.0244   1.0000   0.1304
  -9.250  -0.8396   0.02071   0.01391  -0.0263   0.9681   0.1535
  -9.000  -0.8302   0.01882   0.01224  -0.0269   0.9406   0.1898
  -8.750  -0.8375   0.01779   0.01136  -0.0226   0.9178   0.2245
  -8.500  -0.8422   0.01691   0.01066  -0.0181   0.9009   0.2656
  -8.250  -0.8411   0.01615   0.01011  -0.0143   0.8877   0.3119
  -8.000  -0.8328   0.01565   0.00976  -0.0114   0.8768   0.3560
  -7.750  -0.8174   0.01535   0.00955  -0.0095   0.8663   0.3910
  -7.500  -0.7995   0.01522   0.00937  -0.0078   0.8580   0.4176
  -7.250  -0.7782   0.01514   0.00928  -0.0067   0.8486   0.4382
  -7.000  -0.7565   0.01513   0.00921  -0.0055   0.8413   0.4562
  -6.750  -0.7328   0.01513   0.00917  -0.0048   0.8327   0.4720
  -6.500  -0.7097   0.01516   0.00909  -0.0037   0.8261   0.4855
  -6.250  -0.6849   0.01517   0.00900  -0.0033   0.8176   0.4984
  -6.000  -0.6597   0.01525   0.00904  -0.0025   0.8115   0.5092
  -5.750  -0.6333   0.01535   0.00912  -0.0022   0.8037   0.5205
  -5.500  -0.6083   0.01551   0.00922  -0.0014   0.7970   0.5336
  -5.250  -0.5830   0.01571   0.00933  -0.0008   0.7904   0.5466
  -5.000  -0.5545   0.01587   0.00955  -0.0006   0.7835   0.5545
  -4.750  -0.5294   0.01584   0.00936   0.0000   0.7782   0.5634
  -4.500  -0.5003   0.01599   0.00957   0.0000   0.7708   0.5703
  -4.250  -0.4747   0.01598   0.00943   0.0004   0.7646   0.5796
  -4.000  -0.4461   0.01610   0.00957   0.0007   0.7593   0.5854
  -3.750  -0.4189   0.01606   0.00947   0.0006   0.7523   0.5925
  -3.500  -0.3915   0.01598   0.00933   0.0008   0.7469   0.5979
  -3.250  -0.3633   0.01602   0.00935   0.0008   0.7412   0.6030
  -3.000  -0.3363   0.01593   0.00918   0.0008   0.7345   0.6098
  -2.750  -0.3083   0.01586   0.00907   0.0009   0.7296   0.6145
  -2.500  -0.2800   0.01590   0.00910   0.0009   0.7241   0.6194
  -2.250  -0.2526   0.01581   0.00896   0.0007   0.7177   0.6257
  -2.000  -0.2248   0.01572   0.00881   0.0008   0.7128   0.6304
  -1.750  -0.1964   0.01575   0.00886   0.0007   0.7075   0.6348
  -1.500  -0.1685   0.01572   0.00880   0.0005   0.7014   0.6405
  -1.250  -0.1408   0.01561   0.00862   0.0005   0.6966   0.6459
  -1.000  -0.1124   0.01564   0.00866   0.0005   0.6916   0.6499
  -0.750  -0.0843   0.01564   0.00868   0.0003   0.6855   0.6552
  -0.500  -0.0565   0.01556   0.00851   0.0001   0.6808   0.6614
  -0.250  -0.0280   0.01557   0.00853   0.0002   0.6766   0.6652
   0.000   0.0000   0.01561   0.00864   0.0000   0.6701   0.6701
   0.250   0.0280   0.01557   0.00853  -0.0002   0.6652   0.6766
   0.500   0.0565   0.01555   0.00851  -0.0001   0.6614   0.6808
   0.750   0.0843   0.01564   0.00868  -0.0003   0.6552   0.6855
   1.000   0.1124   0.01564   0.00866  -0.0005   0.6499   0.6917
   1.250   0.1408   0.01561   0.00862  -0.0005   0.6459   0.6966
   1.500   0.1685   0.01572   0.00880  -0.0005   0.6405   0.7014
   1.750   0.1964   0.01575   0.00886  -0.0007   0.6348   0.7075
   2.000   0.2248   0.01572   0.00882  -0.0008   0.6304   0.7128
   2.250   0.2526   0.01581   0.00896  -0.0007   0.6256   0.7177
   2.500   0.2800   0.01589   0.00910  -0.0009   0.6194   0.7241
   2.750   0.3083   0.01586   0.00907  -0.0009   0.6145   0.7296
   3.000   0.3363   0.01593   0.00918  -0.0008   0.6098   0.7345
   3.250   0.3633   0.01601   0.00935  -0.0008   0.6030   0.7412
   3.500   0.3915   0.01599   0.00933  -0.0008   0.5979   0.7469
   3.750   0.4189   0.01606   0.00947  -0.0006   0.5925   0.7523
   4.000   0.4461   0.01610   0.00957  -0.0007   0.5854   0.7593
   4.250   0.4747   0.01598   0.00943  -0.0004   0.5796   0.7646
   4.500   0.5003   0.01599   0.00957   0.0000   0.5703   0.7708
   4.750   0.5294   0.01584   0.00936   0.0000   0.5634   0.7782
   5.000   0.5545   0.01587   0.00955   0.0006   0.5546   0.7835
   5.250   0.5831   0.01571   0.00933   0.0008   0.5467   0.7904
   5.500   0.6083   0.01551   0.00922   0.0014   0.5336   0.7970
   5.750   0.6333   0.01535   0.00912   0.0022   0.5204   0.8037
   6.000   0.6598   0.01525   0.00904   0.0025   0.5091   0.8115
   6.250   0.6849   0.01517   0.00900   0.0033   0.4984   0.8176
   6.500   0.7097   0.01516   0.00909   0.0037   0.4855   0.8261
   6.750   0.7329   0.01513   0.00917   0.0047   0.4719   0.8327
   7.000   0.7566   0.01513   0.00922   0.0055   0.4563   0.8413
   7.250   0.7783   0.01514   0.00928   0.0067   0.4383   0.8486
   7.500   0.7995   0.01522   0.00937   0.0078   0.4176   0.8580
   7.750   0.8174   0.01535   0.00955   0.0095   0.3909   0.8663
   8.000   0.8329   0.01565   0.00975   0.0114   0.3560   0.8768
   8.250   0.8412   0.01615   0.01011   0.0143   0.3119   0.8877
   8.500   0.8423   0.01691   0.01066   0.0181   0.2656   0.9009
   8.750   0.8375   0.01780   0.01136   0.0226   0.2241   0.9177
   9.000   0.8305   0.01882   0.01223   0.0269   0.1900   0.9406
   9.250   0.8398   0.02072   0.01392   0.0263   0.1533   0.9682
   9.500   0.8554   0.02248   0.01555   0.0243   0.1305   1.0000
   9.750   0.8608   0.02398   0.01694   0.0249   0.1199   1.0000
  10.000   0.8685   0.02544   0.01831   0.0254   0.1118   1.0000
  10.250   0.8784   0.02679   0.01964   0.0260   0.1057   1.0000
  10.500   0.8896   0.02805   0.02088   0.0265   0.1005   1.0000
  10.750   0.8983   0.02952   0.02222   0.0274   0.0963   1.0000
  11.000   0.9128   0.03060   0.02335   0.0279   0.0932   1.0000
  11.250   0.9271   0.03170   0.02448   0.0284   0.0901   1.0000
  11.500   0.9414   0.03282   0.02559   0.0290   0.0874   1.0000
  11.750   0.9582   0.03391   0.02659   0.0297   0.0845   1.0000
  12.000   0.9773   0.03493   0.02762   0.0302   0.0822   1.0000
  12.250   0.9926   0.03605   0.02884   0.0307   0.0802   1.0000
  12.500   1.0095   0.03716   0.03001   0.0312   0.0783   1.0000
  12.750   1.0259   0.03830   0.03119   0.0316   0.0763   1.0000
  13.000   1.0432   0.03942   0.03230   0.0319   0.0743   1.0000
  13.250   1.0756   0.04065   0.03347   0.0322   0.0716   1.0000
  13.500   1.0846   0.04212   0.03510   0.0327   0.0706   1.0000
  13.750   1.0941   0.04370   0.03684   0.0331   0.0692   1.0000
  14.000   1.1035   0.04532   0.03858   0.0334   0.0676   1.0000
  14.250   1.1111   0.04700   0.04035   0.0337   0.0657   1.0000
  14.500   1.1200   0.04854   0.04192   0.0339   0.0639   1.0000
  14.750   1.1456   0.05032   0.04360   0.0339   0.0610   1.0000
  15.000   1.1414   0.05253   0.04602   0.0342   0.0602   1.0000
  15.250   1.1385   0.05498   0.04867   0.0341   0.0590   1.0000
  15.500   1.1370   0.05751   0.05136   0.0340   0.0576   1.0000
  15.750   1.1372   0.05998   0.05396   0.0337   0.0562   1.0000
  16.000   1.1383   0.06236   0.05642   0.0332   0.0548   1.0000
  16.250   1.1460   0.06428   0.05833   0.0328   0.0532   1.0000
  16.500   1.1548   0.06714   0.06122   0.0327   0.0514   1.0000
  16.750   1.1412   0.07112   0.06544   0.0315   0.0508   1.0000
  17.000   1.1258   0.07566   0.07023   0.0298   0.0500   1.0000
  17.250   1.1109   0.08062   0.07541   0.0278   0.0492   1.0000
  17.500   1.0954   0.08594   0.08094   0.0254   0.0483   1.0000
  17.750   1.0809   0.09138   0.08658   0.0227   0.0475   1.0000
  18.000   1.0715   0.09625   0.09156   0.0201   0.0464   1.0000
  18.250   1.0604   0.10158   0.09701   0.0172   0.0456   1.0000
  18.500   1.0850   0.10127   0.09650   0.0182   0.0435   1.0000
  18.750   0.9950   0.12104   0.11696   0.0057   0.0452   1.0000
  19.000   0.9822   0.12760   0.12360   0.0016   0.0444   1.0000
  19.250   0.9647   0.13527   0.13134  -0.0030   0.0436   1.0000
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