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NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(3)-018 (naca633018-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.05 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633018-il-1000000.txt
Download as CSV file: xf-naca633018-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.3187   0.08328   0.07909  -0.0153   1.0000   0.0164
 -19.500  -1.3207   0.07963   0.07537  -0.0167   1.0000   0.0174
 -19.250  -1.3233   0.07597   0.07168  -0.0181   1.0000   0.0187
 -19.000  -1.3227   0.07281   0.06847  -0.0192   1.0000   0.0200
 -18.750  -1.3203   0.06994   0.06554  -0.0201   1.0000   0.0211
 -18.500  -1.3196   0.06688   0.06245  -0.0211   1.0000   0.0222
 -18.250  -1.3158   0.06424   0.05978  -0.0219   1.0000   0.0234
 -18.000  -1.3099   0.06191   0.05740  -0.0225   1.0000   0.0243
 -17.750  -1.3025   0.05979   0.05521  -0.0231   1.0000   0.0250
 -17.500  -1.2996   0.05715   0.05253  -0.0237   1.0000   0.0258
 -17.250  -1.2962   0.05464   0.04998  -0.0242   1.0000   0.0266
 -17.000  -1.2890   0.05257   0.04789  -0.0246   1.0000   0.0277
 -16.750  -1.2801   0.05074   0.04603  -0.0249   1.0000   0.0286
 -16.500  -1.2713   0.04890   0.04414  -0.0252   1.0000   0.0293
 -16.250  -1.2638   0.04695   0.04213  -0.0254   1.0000   0.0297
 -16.000  -1.2498   0.04568   0.04082  -0.0256   1.0000   0.0302
 -15.750  -1.2490   0.04315   0.03823  -0.0257   1.0000   0.0311
 -15.500  -1.2439   0.04110   0.03615  -0.0257   1.0000   0.0319
 -15.250  -1.2362   0.03932   0.03435  -0.0257   1.0000   0.0327
 -15.000  -1.2271   0.03771   0.03271  -0.0256   1.0000   0.0335
 -14.750  -1.2171   0.03623   0.03119  -0.0254   1.0000   0.0341
 -14.500  -1.2061   0.03487   0.02979  -0.0253   1.0000   0.0349
 -14.250  -1.1947   0.03357   0.02845  -0.0250   1.0000   0.0355
 -14.000  -1.1822   0.03237   0.02721  -0.0248   1.0000   0.0360
 -13.750  -1.1698   0.03119   0.02599  -0.0245   1.0000   0.0363
 -13.500  -1.1677   0.02923   0.02397  -0.0238   1.0000   0.0372
 -13.250  -1.1613   0.02765   0.02236  -0.0231   1.0000   0.0383
 -13.000  -1.1516   0.02636   0.02106  -0.0225   1.0000   0.0393
 -12.750  -1.1404   0.02519   0.01988  -0.0219   1.0000   0.0401
 -12.500  -1.1272   0.02419   0.01886  -0.0214   1.0000   0.0410
 -12.250  -1.1138   0.02323   0.01787  -0.0208   1.0000   0.0419
 -12.000  -1.0942   0.02228   0.01687  -0.0214   0.9604   0.0426
 -11.750  -1.0612   0.02167   0.01610  -0.0240   0.9113   0.0434
 -11.500  -1.0595   0.02047   0.01474  -0.0217   0.8797   0.0448
 -11.250  -1.0528   0.01951   0.01370  -0.0198   0.8605   0.0462
 -11.000  -1.0430   0.01870   0.01281  -0.0181   0.8457   0.0474
 -10.750  -1.0319   0.01797   0.01202  -0.0165   0.8330   0.0486
 -10.500  -1.0199   0.01731   0.01129  -0.0150   0.8220   0.0496
 -10.250  -1.0061   0.01678   0.01068  -0.0135   0.8116   0.0508
 -10.000  -0.9926   0.01625   0.01008  -0.0119   0.8022   0.0514
  -9.750  -0.9846   0.01559   0.00934  -0.0094   0.7930   0.0533
  -9.500  -0.9767   0.01500   0.00873  -0.0067   0.7840   0.0556
  -9.250  -0.9655   0.01460   0.00829  -0.0042   0.7761   0.0577
  -9.000  -0.9474   0.01423   0.00788  -0.0030   0.7686   0.0599
  -8.750  -0.9288   0.01385   0.00746  -0.0017   0.7613   0.0634
  -8.500  -0.9101   0.01340   0.00703  -0.0006   0.7544   0.0690
  -8.250  -0.8903   0.01297   0.00661   0.0005   0.7474   0.0771
  -8.000  -0.8707   0.01249   0.00618   0.0014   0.7410   0.0903
  -7.750  -0.8503   0.01200   0.00576   0.0023   0.7343   0.1087
  -7.500  -0.8303   0.01147   0.00533   0.0032   0.7278   0.1325
  -7.250  -0.8090   0.01093   0.00493   0.0039   0.7217   0.1587
  -7.000  -0.7874   0.01040   0.00453   0.0046   0.7156   0.1893
  -6.750  -0.7656   0.00986   0.00413   0.0052   0.7098   0.2262
  -6.500  -0.7430   0.00929   0.00375   0.0057   0.7038   0.2657
  -6.250  -0.7196   0.00880   0.00341   0.0061   0.6977   0.3064
  -6.000  -0.6951   0.00837   0.00313   0.0064   0.6921   0.3438
  -5.750  -0.6689   0.00806   0.00293   0.0065   0.6865   0.3739
  -5.500  -0.6419   0.00784   0.00276   0.0064   0.6808   0.3983
  -5.250  -0.6140   0.00770   0.00264   0.0063   0.6754   0.4158
  -5.000  -0.5856   0.00756   0.00253   0.0061   0.6697   0.4291
  -4.750  -0.5572   0.00747   0.00242   0.0059   0.6640   0.4401
  -4.500  -0.5283   0.00741   0.00234   0.0057   0.6589   0.4504
  -4.250  -0.4995   0.00731   0.00226   0.0054   0.6537   0.4609
  -4.000  -0.4707   0.00724   0.00218   0.0052   0.6482   0.4718
  -3.750  -0.4417   0.00721   0.00212   0.0049   0.6429   0.4831
  -3.500  -0.4126   0.00713   0.00208   0.0047   0.6377   0.4931
  -3.250  -0.3832   0.00710   0.00201   0.0043   0.6326   0.4997
  -3.000  -0.3543   0.00707   0.00197   0.0041   0.6275   0.5068
  -2.750  -0.3245   0.00705   0.00193   0.0037   0.6227   0.5144
  -2.500  -0.2954   0.00699   0.00189   0.0034   0.6174   0.5212
  -2.250  -0.2660   0.00699   0.00185   0.0031   0.6123   0.5265
  -2.000  -0.2363   0.00698   0.00182   0.0027   0.6079   0.5310
  -1.750  -0.2069   0.00692   0.00178   0.0024   0.6029   0.5362
  -1.500  -0.1775   0.00692   0.00175   0.0021   0.5979   0.5415
  -1.250  -0.1477   0.00694   0.00174   0.0017   0.5932   0.5461
  -1.000  -0.1183   0.00688   0.00172   0.0014   0.5886   0.5512
  -0.750  -0.0888   0.00687   0.00170   0.0011   0.5838   0.5561
  -0.500  -0.0593   0.00692   0.00169   0.0007   0.5787   0.5606
  -0.250  -0.0295   0.00688   0.00168   0.0003   0.5746   0.5651
   0.000   0.0000   0.00686   0.00168   0.0000   0.5699   0.5699
   0.250   0.0295   0.00688   0.00168  -0.0003   0.5652   0.5746
   0.500   0.0593   0.00692   0.00169  -0.0007   0.5606   0.5788
   0.750   0.0888   0.00687   0.00170  -0.0011   0.5561   0.5838
   1.000   0.1183   0.00688   0.00172  -0.0014   0.5512   0.5887
   1.250   0.1477   0.00694   0.00174  -0.0017   0.5461   0.5932
   1.500   0.1775   0.00692   0.00175  -0.0021   0.5415   0.5979
   1.750   0.2069   0.00692   0.00178  -0.0024   0.5363   0.6029
   2.000   0.2363   0.00698   0.00182  -0.0027   0.5310   0.6079
   2.250   0.2660   0.00699   0.00185  -0.0031   0.5264   0.6123
   2.500   0.2954   0.00699   0.00189  -0.0034   0.5212   0.6174
   2.750   0.3245   0.00705   0.00193  -0.0037   0.5144   0.6227
   3.000   0.3543   0.00707   0.00197  -0.0041   0.5068   0.6275
   3.250   0.3832   0.00710   0.00201  -0.0043   0.4997   0.6326
   3.500   0.4126   0.00713   0.00208  -0.0047   0.4933   0.6377
   3.750   0.4417   0.00721   0.00212  -0.0049   0.4831   0.6429
   4.000   0.4707   0.00724   0.00218  -0.0052   0.4718   0.6482
   4.250   0.4995   0.00731   0.00226  -0.0054   0.4610   0.6537
   4.500   0.5283   0.00741   0.00234  -0.0057   0.4505   0.6589
   4.750   0.5572   0.00747   0.00242  -0.0059   0.4401   0.6640
   5.000   0.5857   0.00756   0.00253  -0.0061   0.4291   0.6697
   5.250   0.6140   0.00770   0.00264  -0.0063   0.4157   0.6755
   5.500   0.6419   0.00784   0.00276  -0.0064   0.3980   0.6808
   5.750   0.6689   0.00806   0.00293  -0.0065   0.3741   0.6865
   6.000   0.6951   0.00837   0.00313  -0.0064   0.3438   0.6921
   6.250   0.7196   0.00879   0.00341  -0.0061   0.3065   0.6977
   6.500   0.7430   0.00929   0.00375  -0.0057   0.2656   0.7038
   6.750   0.7656   0.00986   0.00413  -0.0052   0.2259   0.7097
   7.000   0.7874   0.01040   0.00453  -0.0046   0.1893   0.7156
   7.250   0.8090   0.01093   0.00493  -0.0039   0.1587   0.7217
   7.500   0.8304   0.01147   0.00533  -0.0032   0.1324   0.7277
   7.750   0.8503   0.01200   0.00576  -0.0023   0.1085   0.7343
   8.000   0.8707   0.01249   0.00618  -0.0015   0.0904   0.7410
   8.250   0.8904   0.01297   0.00661  -0.0005   0.0771   0.7474
   8.500   0.9101   0.01340   0.00702   0.0006   0.0690   0.7543
   8.750   0.9288   0.01386   0.00746   0.0017   0.0633   0.7613
   9.000   0.9474   0.01423   0.00788   0.0029   0.0600   0.7686
   9.250   0.9656   0.01460   0.00829   0.0042   0.0578   0.7761
   9.500   0.9770   0.01500   0.00873   0.0066   0.0556   0.7840
   9.750   0.9849   0.01558   0.00934   0.0094   0.0532   0.7930
  10.000   0.9927   0.01625   0.01008   0.0119   0.0514   0.8023
  10.250   1.0068   0.01676   0.01065   0.0134   0.0507   0.8115
  10.500   1.0197   0.01733   0.01131   0.0150   0.0498   0.8219
  10.750   1.0322   0.01796   0.01201   0.0165   0.0487   0.8329
  11.000   1.0434   0.01868   0.01280   0.0181   0.0474   0.8457
  11.500   1.0596   0.02047   0.01474   0.0216   0.0447   0.8797
  11.750   1.0618   0.02164   0.01607   0.0239   0.0434   0.9112
  12.000   1.0945   0.02233   0.01692   0.0212   0.0427   0.9612
  12.250   1.1158   0.02312   0.01774   0.0206   0.0417   1.0000
  12.500   1.1279   0.02417   0.01884   0.0213   0.0411   1.0000
  12.750   1.1411   0.02517   0.01985   0.0218   0.0400   1.0000
  13.000   1.1527   0.02632   0.02101   0.0224   0.0392   1.0000
  13.250   1.1619   0.02765   0.02236   0.0230   0.0381   1.0000
  13.500   1.1689   0.02919   0.02393   0.0236   0.0373   1.0000
  13.750   1.1711   0.03115   0.02594   0.0243   0.0362   1.0000
  14.000   1.1842   0.03228   0.02711   0.0246   0.0359   1.0000
  14.250   1.1981   0.03335   0.02822   0.0248   0.0353   1.0000
  14.500   1.2077   0.03480   0.02972   0.0251   0.0349   1.0000
  14.750   1.2187   0.03616   0.03111   0.0253   0.0341   1.0000
  15.000   1.2290   0.03761   0.03260   0.0254   0.0334   1.0000
  15.250   1.2378   0.03925   0.03428   0.0255   0.0327   1.0000
  15.500   1.2460   0.04097   0.03601   0.0255   0.0318   1.0000
  15.750   1.2507   0.04307   0.03814   0.0255   0.0309   1.0000
  16.000   1.2522   0.04553   0.04065   0.0254   0.0302   1.0000
  16.250   1.2647   0.04695   0.04213   0.0252   0.0298   1.0000
  16.500   1.2750   0.04861   0.04383   0.0250   0.0291   1.0000
  16.750   1.2843   0.05038   0.04566   0.0248   0.0283   1.0000
  17.000   1.2912   0.05244   0.04776   0.0244   0.0277   1.0000
  17.250   1.2977   0.05458   0.04992   0.0240   0.0267   1.0000
  17.500   1.3019   0.05701   0.05237   0.0235   0.0257   1.0000
  17.750   1.3054   0.05955   0.05497   0.0229   0.0249   1.0000
  18.000   1.3127   0.06170   0.05718   0.0224   0.0242   1.0000
  18.250   1.3184   0.06405   0.05958   0.0217   0.0233   1.0000
  18.500   1.3217   0.06673   0.06230   0.0209   0.0222   1.0000
  18.750   1.3223   0.06980   0.06539   0.0200   0.0211   1.0000
  19.000   1.3253   0.07261   0.06827   0.0190   0.0199   1.0000
  19.250   1.3256   0.07580   0.07150   0.0179   0.0186   1.0000
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