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NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(3)-018 (naca633018-il)
Reynolds number: 500,000
Max Cl/Cd: 61.38 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633018-il-500000-n5.txt
Download as CSV file: xf-naca633018-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2070   0.10046   0.09601  -0.0076   1.0000   0.0186
 -19.500  -1.2093   0.09639   0.09186  -0.0096   1.0000   0.0195
 -19.250  -1.2104   0.09255   0.08793  -0.0114   1.0000   0.0204
 -19.000  -1.2117   0.08875   0.08405  -0.0131   1.0000   0.0211
 -18.750  -1.2127   0.08506   0.08030  -0.0147   1.0000   0.0220
 -18.500  -1.2121   0.08164   0.07681  -0.0161   1.0000   0.0227
 -18.250  -1.2105   0.07841   0.07351  -0.0174   1.0000   0.0236
 -18.000  -1.2075   0.07543   0.07044  -0.0185   1.0000   0.0245
 -17.750  -1.2036   0.07264   0.06755  -0.0194   1.0000   0.0252
 -17.500  -1.2026   0.06950   0.06436  -0.0205   1.0000   0.0258
 -17.250  -1.1996   0.06665   0.06147  -0.0215   1.0000   0.0265
 -17.000  -1.1954   0.06400   0.05876  -0.0223   1.0000   0.0273
 -16.750  -1.1904   0.06151   0.05620  -0.0230   1.0000   0.0281
 -16.500  -1.1836   0.05927   0.05390  -0.0235   1.0000   0.0291
 -16.250  -1.1767   0.05708   0.05163  -0.0240   1.0000   0.0298
 -16.000  -1.1701   0.05488   0.04936  -0.0245   1.0000   0.0303
 -15.750  -1.1664   0.05241   0.04684  -0.0249   1.0000   0.0311
 -15.500  -1.1613   0.05015   0.04453  -0.0253   1.0000   0.0317
 -15.250  -1.1542   0.04813   0.04248  -0.0256   1.0000   0.0326
 -15.000  -1.1471   0.04615   0.04045  -0.0258   1.0000   0.0333
 -14.750  -1.1387   0.04435   0.03859  -0.0259   1.0000   0.0342
 -14.500  -1.1302   0.04260   0.03678  -0.0259   1.0000   0.0349
 -14.250  -1.1210   0.04093   0.03505  -0.0259   1.0000   0.0356
 -14.000  -1.1103   0.03944   0.03349  -0.0259   1.0000   0.0362
 -13.750  -1.1053   0.03751   0.03154  -0.0257   1.0000   0.0374
 -13.500  -1.0981   0.03582   0.02983  -0.0254   1.0000   0.0384
 -13.250  -1.0897   0.03426   0.02823  -0.0252   1.0000   0.0392
 -13.000  -1.0793   0.03288   0.02683  -0.0249   1.0000   0.0405
 -12.750  -1.0686   0.03156   0.02547  -0.0245   1.0000   0.0415
 -12.500  -1.0569   0.03034   0.02420  -0.0242   1.0000   0.0425
 -12.250  -1.0475   0.02912   0.02292  -0.0234   0.9639   0.0430
 -12.000  -1.0179   0.02754   0.02122  -0.0272   0.9123   0.0446
 -11.750  -1.0095   0.02636   0.01991  -0.0262   0.8808   0.0456
 -11.500  -1.0016   0.02526   0.01871  -0.0249   0.8606   0.0465
 -11.250  -0.9926   0.02423   0.01758  -0.0236   0.8450   0.0475
 -11.000  -0.9823   0.02328   0.01654  -0.0224   0.8318   0.0487
 -10.750  -0.9711   0.02239   0.01556  -0.0212   0.8205   0.0499
 -10.500  -0.9594   0.02157   0.01464  -0.0200   0.8097   0.0510
 -10.250  -0.9478   0.02074   0.01374  -0.0187   0.7996   0.0521
 -10.000  -0.9381   0.01985   0.01279  -0.0171   0.7908   0.0540
  -9.750  -0.9269   0.01907   0.01197  -0.0156   0.7815   0.0558
  -9.500  -0.9151   0.01838   0.01121  -0.0140   0.7733   0.0579
  -9.250  -0.9025   0.01776   0.01053  -0.0124   0.7650   0.0601
  -9.000  -0.8910   0.01716   0.00988  -0.0105   0.7577   0.0629
  -8.750  -0.8813   0.01657   0.00927  -0.0082   0.7497   0.0671
  -8.500  -0.8687   0.01616   0.00881  -0.0061   0.7429   0.0715
  -8.250  -0.8537   0.01565   0.00831  -0.0045   0.7358   0.0788
  -8.000  -0.8364   0.01518   0.00784  -0.0032   0.7292   0.0877
  -7.750  -0.8180   0.01470   0.00739  -0.0020   0.7230   0.0993
  -7.500  -0.7991   0.01421   0.00694  -0.0010   0.7163   0.1142
  -7.250  -0.7794   0.01373   0.00650   0.0000   0.7103   0.1316
  -7.000  -0.7587   0.01325   0.00609   0.0007   0.7042   0.1515
  -6.750  -0.7383   0.01271   0.00566   0.0015   0.6981   0.1767
  -6.500  -0.7177   0.01216   0.00522   0.0023   0.6924   0.2078
  -6.250  -0.6963   0.01159   0.00480   0.0029   0.6863   0.2432
  -6.000  -0.6742   0.01108   0.00441   0.0035   0.6807   0.2782
  -5.750  -0.6510   0.01061   0.00408   0.0039   0.6756   0.3131
  -5.500  -0.6267   0.01021   0.00380   0.0042   0.6699   0.3464
  -5.250  -0.6012   0.00992   0.00358   0.0044   0.6641   0.3746
  -5.000  -0.5746   0.00971   0.00341   0.0045   0.6590   0.3968
  -4.750  -0.5473   0.00954   0.00327   0.0044   0.6536   0.4149
  -4.500  -0.5203   0.00936   0.00315   0.0044   0.6484   0.4378
  -4.250  -0.4929   0.00924   0.00305   0.0044   0.6435   0.4568
  -4.000  -0.4644   0.00915   0.00296   0.0042   0.6380   0.4682
  -3.750  -0.4359   0.00908   0.00287   0.0040   0.6325   0.4770
  -3.250  -0.3786   0.00898   0.00272   0.0036   0.6231   0.4967
  -3.000  -0.3498   0.00891   0.00266   0.0034   0.6178   0.5027
  -2.750  -0.3210   0.00888   0.00258   0.0031   0.6128   0.5084
  -2.250  -0.2628   0.00880   0.00247   0.0026   0.6033   0.5191
  -2.000  -0.2337   0.00877   0.00242   0.0023   0.5985   0.5247
  -1.750  -0.2045   0.00877   0.00237   0.0020   0.5940   0.5296
  -1.500  -0.1754   0.00872   0.00234   0.0018   0.5890   0.5342
  -1.250  -0.1462   0.00870   0.00231   0.0015   0.5843   0.5389
  -1.000  -0.1170   0.00870   0.00228   0.0012   0.5799   0.5438
  -0.750  -0.0877   0.00869   0.00226   0.0009   0.5755   0.5481
  -0.500  -0.0585   0.00866   0.00225   0.0006   0.5705   0.5524
  -0.250  -0.0293   0.00866   0.00224   0.0003   0.5660   0.5572
   0.000   0.0000   0.00869   0.00223   0.0000   0.5619   0.5619
   0.250   0.0293   0.00866   0.00224  -0.0003   0.5572   0.5660
   0.500   0.0585   0.00866   0.00225  -0.0006   0.5524   0.5705
   0.750   0.0877   0.00869   0.00226  -0.0009   0.5481   0.5755
   1.000   0.1170   0.00870   0.00228  -0.0012   0.5438   0.5799
   1.250   0.1462   0.00870   0.00231  -0.0015   0.5389   0.5843
   1.500   0.1754   0.00872   0.00234  -0.0018   0.5342   0.5890
   1.750   0.2045   0.00877   0.00237  -0.0020   0.5296   0.5940
   2.000   0.2337   0.00877   0.00242  -0.0023   0.5247   0.5985
   2.250   0.2628   0.00880   0.00247  -0.0026   0.5191   0.6033
   2.750   0.3210   0.00888   0.00258  -0.0031   0.5084   0.6128
   3.000   0.3498   0.00891   0.00266  -0.0034   0.5027   0.6178
   3.250   0.3786   0.00898   0.00272  -0.0036   0.4967   0.6231
   3.750   0.4359   0.00908   0.00287  -0.0040   0.4770   0.6325
   4.000   0.4644   0.00915   0.00296  -0.0042   0.4682   0.6380
   4.250   0.4929   0.00924   0.00305  -0.0044   0.4568   0.6435
   4.500   0.5203   0.00936   0.00315  -0.0044   0.4378   0.6484
   4.750   0.5473   0.00954   0.00327  -0.0044   0.4148   0.6536
   5.000   0.5747   0.00971   0.00341  -0.0045   0.3968   0.6590
   5.250   0.6013   0.00991   0.00358  -0.0044   0.3755   0.6642
   5.500   0.6267   0.01021   0.00380  -0.0042   0.3468   0.6699
   5.750   0.6511   0.01061   0.00408  -0.0039   0.3132   0.6756
   6.000   0.6742   0.01107   0.00441  -0.0035   0.2783   0.6807
   6.250   0.6964   0.01159   0.00480  -0.0030   0.2434   0.6863
   6.500   0.7177   0.01216   0.00522  -0.0023   0.2077   0.6924
   6.750   0.7383   0.01272   0.00566  -0.0015   0.1764   0.6981
   7.000   0.7587   0.01325   0.00609  -0.0007   0.1515   0.7042
   7.250   0.7795   0.01374   0.00650   0.0000   0.1315   0.7103
   7.500   0.7991   0.01421   0.00695   0.0010   0.1140   0.7163
   7.750   0.8180   0.01471   0.00739   0.0020   0.0990   0.7230
   8.000   0.8365   0.01518   0.00784   0.0031   0.0877   0.7292
   8.250   0.8538   0.01565   0.00831   0.0045   0.0787   0.7357
   8.500   0.8688   0.01616   0.00881   0.0061   0.0715   0.7429
   8.750   0.8814   0.01657   0.00927   0.0082   0.0670   0.7499
   9.000   0.8914   0.01715   0.00987   0.0105   0.0631   0.7577
   9.250   0.9027   0.01776   0.01053   0.0124   0.0601   0.7650
   9.500   0.9154   0.01837   0.01120   0.0140   0.0579   0.7732
   9.750   0.9273   0.01906   0.01196   0.0155   0.0559   0.7815
  10.000   0.9385   0.01984   0.01278   0.0171   0.0540   0.7906
  10.250   0.9482   0.02072   0.01372   0.0186   0.0521   0.7997
  10.500   0.9598   0.02156   0.01463   0.0199   0.0509   0.8098
  10.750   0.9716   0.02237   0.01554   0.0212   0.0499   0.8204
  11.000   0.9827   0.02326   0.01652   0.0224   0.0487   0.8318
  11.250   0.9928   0.02422   0.01758   0.0236   0.0476   0.8451
  11.500   1.0020   0.02525   0.01869   0.0249   0.0466   0.8609
  11.750   1.0101   0.02633   0.01988   0.0262   0.0456   0.8811
  12.000   1.0185   0.02752   0.02120   0.0272   0.0446   0.9130
  12.250   1.0470   0.02920   0.02299   0.0233   0.0433   0.9655
  12.750   1.0686   0.03160   0.02551   0.0245   0.0417   1.0000
  13.000   1.0809   0.03279   0.02674   0.0247   0.0403   1.0000
  13.250   1.0900   0.03428   0.02826   0.0251   0.0395   1.0000
  13.500   1.0993   0.03577   0.02977   0.0253   0.0382   1.0000
  13.750   1.1063   0.03749   0.03151   0.0256   0.0372   1.0000
  14.000   1.1116   0.03940   0.03344   0.0257   0.0362   1.0000
  14.250   1.1223   0.04088   0.03500   0.0258   0.0356   1.0000
  14.500   1.1317   0.04252   0.03670   0.0258   0.0349   1.0000
  14.750   1.1406   0.04423   0.03847   0.0258   0.0340   1.0000
  15.000   1.1481   0.04613   0.04043   0.0256   0.0334   1.0000
  15.250   1.1559   0.04803   0.04238   0.0254   0.0326   1.0000
  15.500   1.1627   0.05007   0.04446   0.0252   0.0318   1.0000
  15.750   1.1681   0.05231   0.04673   0.0248   0.0311   1.0000
  16.000   1.1721   0.05474   0.04921   0.0244   0.0302   1.0000
  16.250   1.1794   0.05686   0.05140   0.0239   0.0297   1.0000
  16.500   1.1853   0.05917   0.05379   0.0234   0.0291   1.0000
  16.750   1.1922   0.06139   0.05608   0.0228   0.0282   1.0000
  17.000   1.1976   0.06385   0.05860   0.0221   0.0272   1.0000
  17.250   1.2011   0.06656   0.06138   0.0213   0.0267   1.0000
  17.500   1.2046   0.06935   0.06420   0.0204   0.0258   1.0000
  17.750   1.2061   0.07242   0.06733   0.0193   0.0250   1.0000
  18.000   1.2100   0.07523   0.07023   0.0183   0.0243   1.0000
  18.250   1.2127   0.07824   0.07333   0.0172   0.0235   1.0000
  18.500   1.2141   0.08148   0.07665   0.0160   0.0227   1.0000
  18.750   1.2147   0.08489   0.08012   0.0145   0.0218   1.0000
  19.000   1.2138   0.08857   0.08386   0.0129   0.0210   1.0000
  19.250   1.2126   0.09236   0.08774   0.0113   0.0203   1.0000
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