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NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(3)-018 (naca633018-il)
Reynolds number: 200,000
Max Cl/Cd: 50.2 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633018-il-200000-n5.txt
Download as CSV file: xf-naca633018-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0705   0.12223   0.11730   0.0005   1.0000   0.0302
 -19.500  -1.0733   0.11775   0.11278  -0.0021   1.0000   0.0308
 -19.250  -1.0771   0.11308   0.10803  -0.0048   1.0000   0.0314
 -19.000  -1.0810   0.10842   0.10329  -0.0075   1.0000   0.0322
 -18.750  -1.0847   0.10387   0.09862  -0.0100   1.0000   0.0329
 -18.500  -1.0884   0.09939   0.09401  -0.0123   1.0000   0.0338
 -18.250  -1.0917   0.09504   0.08951  -0.0145   1.0000   0.0347
 -18.000  -1.0940   0.09095   0.08525  -0.0164   1.0000   0.0355
 -17.750  -1.0961   0.08692   0.08103  -0.0183   1.0000   0.0363
 -17.500  -1.0939   0.08380   0.07788  -0.0195   1.0000   0.0371
 -17.250  -1.0928   0.08050   0.07453  -0.0210   1.0000   0.0379
 -17.000  -1.0909   0.07734   0.07130  -0.0223   1.0000   0.0388
 -16.750  -1.0885   0.07429   0.06815  -0.0235   1.0000   0.0399
 -16.500  -1.0856   0.07135   0.06509  -0.0246   1.0000   0.0410
 -16.250  -1.0823   0.06850   0.06210  -0.0256   1.0000   0.0422
 -16.000  -1.0786   0.06576   0.05918  -0.0266   1.0000   0.0432
 -15.750  -1.0730   0.06344   0.05687  -0.0270   1.0000   0.0444
 -15.500  -1.0677   0.06105   0.05445  -0.0277   1.0000   0.0456
 -15.250  -1.0616   0.05879   0.05213  -0.0283   1.0000   0.0468
 -15.000  -1.0547   0.05666   0.04993  -0.0287   1.0000   0.0480
 -14.750  -1.0465   0.05470   0.04787  -0.0289   1.0000   0.0491
 -14.500  -1.0374   0.05287   0.04594  -0.0291   1.0000   0.0502
 -14.250  -1.0279   0.05109   0.04406  -0.0292   1.0000   0.0511
 -14.000  -1.0182   0.04941   0.04234  -0.0291   1.0000   0.0521
 -13.750  -1.0101   0.04763   0.04056  -0.0290   1.0000   0.0532
 -13.500  -1.0018   0.04587   0.03878  -0.0289   1.0000   0.0543
 -13.250  -0.9929   0.04419   0.03706  -0.0288   1.0000   0.0554
 -13.000  -0.9838   0.04258   0.03539  -0.0287   1.0000   0.0567
 -12.750  -0.9743   0.04103   0.03378  -0.0285   1.0000   0.0580
 -12.500  -0.9641   0.03955   0.03224  -0.0283   1.0000   0.0594
 -12.250  -0.9537   0.03811   0.03073  -0.0280   1.0000   0.0606
 -12.000  -0.9461   0.03647   0.02908  -0.0276   1.0000   0.0620
 -11.750  -0.9393   0.03479   0.02739  -0.0272   1.0000   0.0635
 -11.500  -0.9311   0.03325   0.02583  -0.0268   1.0000   0.0652
 -11.250  -0.9218   0.03181   0.02436  -0.0264   1.0000   0.0671
 -11.000  -0.9114   0.03048   0.02299  -0.0260   1.0000   0.0694
 -10.750  -0.9002   0.02921   0.02168  -0.0256   1.0000   0.0718
 -10.500  -0.8929   0.02774   0.02023  -0.0252   0.9601   0.0748
 -10.250  -0.8709   0.02639   0.01880  -0.0271   0.9201   0.0793
 -10.000  -0.8580   0.02534   0.01762  -0.0266   0.8950   0.0837
  -9.500  -0.8424   0.02321   0.01538  -0.0236   0.8610   0.0953
  -9.250  -0.8361   0.02216   0.01432  -0.0218   0.8476   0.1035
  -9.000  -0.8296   0.02122   0.01336  -0.0198   0.8357   0.1137
  -8.750  -0.8241   0.02032   0.01244  -0.0174   0.8251   0.1267
  -8.500  -0.8192   0.01946   0.01160  -0.0148   0.8146   0.1418
  -8.250  -0.8147   0.01872   0.01090  -0.0118   0.8054   0.1597
  -8.000  -0.8058   0.01798   0.01021  -0.0095   0.7968   0.1827
  -7.750  -0.7955   0.01720   0.00954  -0.0074   0.7888   0.2102
  -7.500  -0.7834   0.01646   0.00891  -0.0056   0.7811   0.2424
  -7.250  -0.7697   0.01575   0.00833  -0.0038   0.7741   0.2786
  -7.000  -0.7540   0.01510   0.00785  -0.0024   0.7665   0.3180
  -6.750  -0.7353   0.01464   0.00748  -0.0012   0.7605   0.3539
  -6.500  -0.7133   0.01431   0.00723  -0.0005   0.7532   0.3828
  -6.250  -0.6899   0.01408   0.00699   0.0001   0.7470   0.4054
  -6.000  -0.6654   0.01390   0.00680   0.0006   0.7408   0.4247
  -5.750  -0.6402   0.01375   0.00664   0.0009   0.7341   0.4432
  -5.500  -0.6153   0.01365   0.00650   0.0014   0.7286   0.4635
  -5.250  -0.5894   0.01358   0.00641   0.0017   0.7223   0.4814
  -5.000  -0.5628   0.01351   0.00633   0.0019   0.7160   0.4929
  -4.750  -0.5359   0.01345   0.00618   0.0021   0.7110   0.5019
  -4.500  -0.5086   0.01339   0.00607   0.0020   0.7047   0.5124
  -4.250  -0.4811   0.01335   0.00602   0.0022   0.6989   0.5213
  -3.750  -0.4257   0.01323   0.00579   0.0021   0.6877   0.5353
  -3.500  -0.3977   0.01317   0.00566   0.0021   0.6822   0.5415
  -3.250  -0.3699   0.01311   0.00550   0.0020   0.6777   0.5475
  -3.000  -0.3415   0.01306   0.00546   0.0019   0.6718   0.5526
  -2.750  -0.3133   0.01300   0.00535   0.0018   0.6661   0.5584
  -2.500  -0.2852   0.01295   0.00520   0.0017   0.6615   0.5637
  -2.250  -0.2566   0.01291   0.00518   0.0015   0.6561   0.5681
  -2.000  -0.2282   0.01287   0.00511   0.0014   0.6507   0.5733
  -1.750  -0.1999   0.01283   0.00497   0.0012   0.6460   0.5788
  -1.500  -0.1713   0.01279   0.00496   0.0011   0.6409   0.5828
  -1.250  -0.1428   0.01277   0.00493   0.0009   0.6355   0.5875
  -1.000  -0.1143   0.01274   0.00485   0.0007   0.6309   0.5929
  -0.750  -0.0858   0.01272   0.00480   0.0006   0.6265   0.5973
  -0.500  -0.0571   0.01271   0.00483   0.0004   0.6208   0.6016
  -0.250  -0.0286   0.01270   0.00480   0.0002   0.6160   0.6068
   0.000   0.0000   0.01270   0.00474   0.0000   0.6120   0.6120
   0.250   0.0286   0.01270   0.00480  -0.0002   0.6068   0.6160
   0.500   0.0571   0.01271   0.00483  -0.0004   0.6016   0.6209
   0.750   0.0858   0.01272   0.00480  -0.0006   0.5973   0.6265
   1.000   0.1143   0.01274   0.00485  -0.0007   0.5929   0.6309
   1.250   0.1428   0.01277   0.00493  -0.0009   0.5875   0.6355
   1.500   0.1713   0.01279   0.00496  -0.0011   0.5828   0.6409
   1.750   0.1999   0.01283   0.00497  -0.0012   0.5788   0.6460
   2.000   0.2282   0.01287   0.00511  -0.0014   0.5733   0.6507
   2.250   0.2566   0.01291   0.00518  -0.0015   0.5681   0.6561
   2.500   0.2852   0.01295   0.00520  -0.0017   0.5637   0.6615
   2.750   0.3133   0.01300   0.00535  -0.0018   0.5583   0.6661
   3.000   0.3415   0.01306   0.00546  -0.0019   0.5526   0.6718
   3.250   0.3699   0.01311   0.00550  -0.0020   0.5475   0.6777
   3.500   0.3977   0.01317   0.00566  -0.0021   0.5415   0.6822
   3.750   0.4257   0.01323   0.00578  -0.0021   0.5353   0.6877
   4.250   0.4811   0.01335   0.00602  -0.0022   0.5213   0.6989
   4.500   0.5086   0.01339   0.00607  -0.0020   0.5124   0.7047
   4.750   0.5359   0.01344   0.00617  -0.0021   0.5019   0.7109
   5.000   0.5628   0.01351   0.00633  -0.0019   0.4929   0.7160
   5.250   0.5894   0.01358   0.00641  -0.0017   0.4815   0.7223
   5.500   0.6153   0.01365   0.00650  -0.0014   0.4636   0.7286
   5.750   0.6402   0.01375   0.00664  -0.0009   0.4431   0.7341
   6.000   0.6654   0.01390   0.00680  -0.0006   0.4245   0.7408
   6.250   0.6900   0.01408   0.00699  -0.0001   0.4053   0.7469
   6.500   0.7134   0.01431   0.00723   0.0005   0.3828   0.7532
   6.750   0.7354   0.01465   0.00748   0.0012   0.3537   0.7605
   7.000   0.7541   0.01510   0.00785   0.0024   0.3183   0.7665
   7.250   0.7698   0.01574   0.00833   0.0038   0.2788   0.7741
   7.500   0.7835   0.01646   0.00891   0.0055   0.2424   0.7811
   7.750   0.7955   0.01721   0.00954   0.0074   0.2100   0.7888
   8.000   0.8059   0.01798   0.01021   0.0095   0.1827   0.7969
   8.250   0.8149   0.01872   0.01090   0.0118   0.1598   0.8055
   8.500   0.8194   0.01946   0.01160   0.0148   0.1418   0.8146
   8.750   0.8241   0.02032   0.01244   0.0174   0.1263   0.8251
   9.000   0.8299   0.02122   0.01335   0.0197   0.1138   0.8357
   9.250   0.8363   0.02216   0.01432   0.0218   0.1034   0.8476
   9.500   0.8427   0.02320   0.01537   0.0236   0.0954   0.8611
  10.000   0.8584   0.02533   0.01761   0.0265   0.0837   0.8951
  10.250   0.8715   0.02637   0.01877   0.0270   0.0794   0.9200
  10.500   0.8935   0.02773   0.02022   0.0250   0.0746   0.9606
  10.750   0.9008   0.02920   0.02167   0.0255   0.0718   1.0000
  11.000   0.9122   0.03044   0.02295   0.0259   0.0693   1.0000
  11.250   0.9225   0.03179   0.02434   0.0263   0.0671   1.0000
  11.500   0.9320   0.03322   0.02580   0.0267   0.0652   1.0000
  11.750   0.9401   0.03476   0.02736   0.0271   0.0635   1.0000
  12.000   0.9470   0.03644   0.02904   0.0275   0.0620   1.0000
  12.250   0.9547   0.03807   0.03068   0.0279   0.0606   1.0000
  12.500   0.9652   0.03950   0.03219   0.0282   0.0594   1.0000
  12.750   0.9752   0.04099   0.03374   0.0284   0.0579   1.0000
  13.000   0.9848   0.04254   0.03535   0.0286   0.0566   1.0000
  13.250   0.9939   0.04415   0.03702   0.0287   0.0554   1.0000
  13.500   1.0028   0.04583   0.03873   0.0288   0.0543   1.0000
  13.750   1.0113   0.04757   0.04049   0.0289   0.0532   1.0000
  14.000   1.0195   0.04935   0.04227   0.0290   0.0521   1.0000
  14.250   1.0291   0.05104   0.04400   0.0291   0.0511   1.0000
  14.500   1.0386   0.05280   0.04587   0.0290   0.0502   1.0000
  14.750   1.0477   0.05464   0.04782   0.0288   0.0491   1.0000
  15.000   1.0558   0.05660   0.04987   0.0286   0.0480   1.0000
  15.250   1.0630   0.05869   0.05204   0.0282   0.0468   1.0000
  15.500   1.0688   0.06099   0.05439   0.0276   0.0455   1.0000
  15.750   1.0743   0.06334   0.05677   0.0269   0.0444   1.0000
  16.000   1.0798   0.06568   0.05910   0.0264   0.0432   1.0000
  16.250   1.0837   0.06842   0.06201   0.0255   0.0421   1.0000
  16.500   1.0869   0.07128   0.06502   0.0245   0.0409   1.0000
  16.750   1.0900   0.07419   0.06804   0.0234   0.0398   1.0000
  17.000   1.0920   0.07730   0.07125   0.0221   0.0387   1.0000
  17.250   1.0942   0.08042   0.07444   0.0208   0.0378   1.0000
  17.500   1.0955   0.08370   0.07777   0.0194   0.0370   1.0000
  17.750   1.0974   0.08688   0.08097   0.0181   0.0362   1.0000
  18.000   1.0957   0.09085   0.08515   0.0163   0.0355   1.0000
  18.250   1.0932   0.09497   0.08944   0.0143   0.0346   1.0000
  18.500   1.0901   0.09927   0.09389   0.0122   0.0337   1.0000
  18.750   1.0865   0.10373   0.09848   0.0098   0.0329   1.0000
  19.000   1.0828   0.10831   0.10317   0.0073   0.0321   1.0000
  19.250   1.0790   0.11295   0.10790   0.0047   0.0314   1.0000
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