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NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(3)-018 (naca633018-il)
Reynolds number: 1,000,000
Max Cl/Cd: 65.4 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633018-il-1000000-n5.txt
Download as CSV file: xf-naca633018-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2926   0.08680   0.08241  -0.0137   1.0000   0.0091
 -19.500  -1.2972   0.08270   0.07824  -0.0154   1.0000   0.0094
 -19.250  -1.3010   0.07879   0.07425  -0.0170   1.0000   0.0099
 -19.000  -1.3034   0.07516   0.07056  -0.0183   1.0000   0.0105
 -18.500  -1.3065   0.06834   0.06362  -0.0206   1.0000   0.0118
 -18.250  -1.3084   0.06499   0.06022  -0.0216   1.0000   0.0131
 -18.000  -1.3074   0.06207   0.05725  -0.0224   1.0000   0.0141
 -17.750  -1.3071   0.05914   0.05427  -0.0231   1.0000   0.0151
 -17.500  -1.3051   0.05643   0.05152  -0.0237   1.0000   0.0163
 -17.250  -1.3010   0.05401   0.04905  -0.0242   1.0000   0.0171
 -17.000  -1.2987   0.05146   0.04649  -0.0246   1.0000   0.0191
 -16.750  -1.2939   0.04921   0.04419  -0.0249   1.0000   0.0203
 -16.500  -1.2878   0.04713   0.04207  -0.0251   1.0000   0.0210
 -16.250  -1.2816   0.04509   0.03998  -0.0253   1.0000   0.0213
 -16.000  -1.2760   0.04305   0.03793  -0.0254   1.0000   0.0229
 -15.750  -1.2683   0.04125   0.03610  -0.0254   1.0000   0.0238
 -15.500  -1.2602   0.03952   0.03431  -0.0254   1.0000   0.0245
 -15.250  -1.2515   0.03787   0.03261  -0.0253   1.0000   0.0250
 -15.000  -1.2438   0.03618   0.03089  -0.0251   1.0000   0.0258
 -14.750  -1.2357   0.03459   0.02927  -0.0248   1.0000   0.0266
 -14.500  -1.2271   0.03307   0.02773  -0.0245   1.0000   0.0275
 -14.250  -1.2175   0.03167   0.02630  -0.0242   1.0000   0.0283
 -14.000  -1.2071   0.03035   0.02494  -0.0238   1.0000   0.0290
 -13.500  -1.1717   0.02784   0.02232  -0.0256   0.9473   0.0301
 -13.250  -1.1524   0.02671   0.02101  -0.0266   0.8914   0.0311
 -13.000  -1.1449   0.02562   0.01981  -0.0253   0.8638   0.0321
 -12.750  -1.1357   0.02458   0.01868  -0.0242   0.8459   0.0330
 -12.500  -1.1249   0.02363   0.01766  -0.0231   0.8306   0.0339
 -12.250  -1.1134   0.02272   0.01668  -0.0221   0.8184   0.0347
 -12.000  -1.1013   0.02187   0.01575  -0.0210   0.8077   0.0353
 -11.750  -1.0879   0.02110   0.01491  -0.0200   0.7972   0.0360
 -11.500  -1.0757   0.02028   0.01403  -0.0189   0.7878   0.0368
 -11.250  -1.0648   0.01943   0.01312  -0.0175   0.7783   0.0379
 -11.000  -1.0529   0.01865   0.01231  -0.0162   0.7702   0.0391
 -10.750  -1.0405   0.01796   0.01156  -0.0148   0.7616   0.0401
 -10.500  -1.0272   0.01732   0.01087  -0.0134   0.7540   0.0410
 -10.250  -1.0135   0.01676   0.01026  -0.0120   0.7459   0.0422
 -10.000  -0.9995   0.01624   0.00968  -0.0104   0.7390   0.0429
  -9.750  -0.9861   0.01575   0.00914  -0.0087   0.7315   0.0437
  -9.500  -0.9754   0.01525   0.00860  -0.0064   0.7248   0.0453
  -9.250  -0.9632   0.01486   0.00818  -0.0041   0.7178   0.0468
  -9.000  -0.9457   0.01451   0.00780  -0.0027   0.7113   0.0484
  -8.750  -0.9257   0.01418   0.00744  -0.0018   0.7054   0.0502
  -8.500  -0.9044   0.01389   0.00711  -0.0010   0.6987   0.0517
  -8.250  -0.8835   0.01354   0.00675  -0.0001   0.6928   0.0551
  -8.000  -0.8615   0.01322   0.00642   0.0006   0.6869   0.0588
  -7.750  -0.8387   0.01292   0.00610   0.0012   0.6807   0.0632
  -7.500  -0.8161   0.01258   0.00578   0.0017   0.6751   0.0704
  -7.250  -0.7933   0.01221   0.00544   0.0023   0.6692   0.0801
  -7.000  -0.7701   0.01186   0.00512   0.0028   0.6637   0.0918
  -6.750  -0.7466   0.01150   0.00482   0.0032   0.6587   0.1061
  -6.500  -0.7224   0.01115   0.00452   0.0036   0.6531   0.1220
  -6.250  -0.6981   0.01081   0.00423   0.0039   0.6471   0.1392
  -6.000  -0.6737   0.01043   0.00394   0.0042   0.6422   0.1599
  -5.750  -0.6492   0.01003   0.00365   0.0044   0.6372   0.1858
  -5.500  -0.6252   0.00958   0.00334   0.0048   0.6320   0.2192
  -5.250  -0.6003   0.00918   0.00306   0.0050   0.6270   0.2518
  -5.000  -0.5747   0.00881   0.00281   0.0051   0.6219   0.2824
  -4.750  -0.5487   0.00847   0.00258   0.0051   0.6164   0.3137
  -4.250  -0.4951   0.00792   0.00223   0.0051   0.6074   0.3725
  -4.000  -0.4677   0.00769   0.00210   0.0050   0.6024   0.4006
  -3.750  -0.4399   0.00751   0.00199   0.0048   0.5972   0.4244
  -3.500  -0.4114   0.00740   0.00191   0.0046   0.5926   0.4413
  -3.250  -0.3822   0.00734   0.00185   0.0043   0.5881   0.4506
  -3.000  -0.3533   0.00726   0.00179   0.0040   0.5834   0.4608
  -2.750  -0.3244   0.00720   0.00173   0.0038   0.5787   0.4720
  -2.500  -0.2949   0.00716   0.00169   0.0034   0.5743   0.4801
  -2.250  -0.2656   0.00712   0.00164   0.0031   0.5694   0.4855
  -2.000  -0.2362   0.00709   0.00160   0.0028   0.5649   0.4910
  -1.750  -0.2067   0.00708   0.00157   0.0024   0.5608   0.4963
  -1.500  -0.1772   0.00704   0.00154   0.0021   0.5563   0.5016
  -1.250  -0.1478   0.00702   0.00152   0.0018   0.5514   0.5072
  -1.000  -0.1182   0.00703   0.00150   0.0014   0.5471   0.5119
  -0.750  -0.0887   0.00701   0.00148   0.0010   0.5432   0.5163
  -0.500  -0.0591   0.00698   0.00147   0.0007   0.5386   0.5210
  -0.250  -0.0296   0.00699   0.00146   0.0004   0.5340   0.5257
   0.000   0.0000   0.00701   0.00146   0.0000   0.5297   0.5297
   0.250   0.0296   0.00699   0.00146  -0.0004   0.5257   0.5340
   0.500   0.0591   0.00698   0.00147  -0.0007   0.5210   0.5387
   0.750   0.0887   0.00701   0.00148  -0.0011   0.5163   0.5432
   1.000   0.1182   0.00703   0.00150  -0.0014   0.5120   0.5471
   1.250   0.1478   0.00702   0.00152  -0.0018   0.5072   0.5514
   1.500   0.1772   0.00704   0.00154  -0.0021   0.5016   0.5563
   1.750   0.2067   0.00708   0.00157  -0.0024   0.4963   0.5608
   2.000   0.2362   0.00709   0.00160  -0.0028   0.4910   0.5649
   2.250   0.2656   0.00712   0.00164  -0.0031   0.4855   0.5694
   2.500   0.2949   0.00716   0.00169  -0.0034   0.4802   0.5743
   2.750   0.3244   0.00720   0.00173  -0.0038   0.4719   0.5787
   3.000   0.3533   0.00726   0.00179  -0.0040   0.4608   0.5834
   3.250   0.3822   0.00734   0.00185  -0.0043   0.4506   0.5881
   3.500   0.4114   0.00740   0.00191  -0.0046   0.4416   0.5926
   3.750   0.4399   0.00751   0.00199  -0.0048   0.4245   0.5972
   4.000   0.4677   0.00769   0.00210  -0.0050   0.4008   0.6024
   4.250   0.4952   0.00791   0.00223  -0.0051   0.3729   0.6074
   4.750   0.5487   0.00847   0.00258  -0.0051   0.3136   0.6165
   5.000   0.5747   0.00881   0.00281  -0.0051   0.2824   0.6219
   5.250   0.6004   0.00918   0.00306  -0.0050   0.2519   0.6270
   5.500   0.6251   0.00959   0.00334  -0.0047   0.2184   0.6320
   5.750   0.6493   0.01003   0.00365  -0.0045   0.1862   0.6372
   6.000   0.6737   0.01043   0.00394  -0.0042   0.1600   0.6422
   6.250   0.6981   0.01080   0.00423  -0.0039   0.1394   0.6472
   6.500   0.7225   0.01115   0.00452  -0.0036   0.1220   0.6531
   6.750   0.7466   0.01150   0.00482  -0.0032   0.1058   0.6587
   7.000   0.7702   0.01186   0.00513  -0.0028   0.0917   0.6637
   7.250   0.7934   0.01221   0.00544  -0.0023   0.0800   0.6692
   7.500   0.8162   0.01258   0.00578  -0.0018   0.0704   0.6750
   7.750   0.8387   0.01292   0.00610  -0.0012   0.0632   0.6807
   8.000   0.8615   0.01322   0.00642  -0.0006   0.0588   0.6869
   8.250   0.8837   0.01354   0.00675   0.0001   0.0552   0.6927
   8.500   0.9044   0.01389   0.00711   0.0009   0.0517   0.6987
   8.750   0.9258   0.01418   0.00744   0.0018   0.0501   0.7054
   9.000   0.9459   0.01451   0.00779   0.0027   0.0485   0.7114
   9.250   0.9634   0.01486   0.00818   0.0041   0.0468   0.7179
   9.500   0.9755   0.01525   0.00860   0.0064   0.0453   0.7248
   9.750   0.9863   0.01575   0.00914   0.0087   0.0436   0.7316
  10.000   0.9998   0.01623   0.00968   0.0104   0.0429   0.7391
  10.250   1.0139   0.01674   0.01024   0.0119   0.0420   0.7458
  10.500   1.0276   0.01731   0.01087   0.0134   0.0412   0.7536
  11.000   1.0534   0.01864   0.01229   0.0161   0.0391   0.7702
  11.250   1.0651   0.01943   0.01311   0.0175   0.0378   0.7784
  11.500   1.0762   0.02027   0.01401   0.0188   0.0367   0.7877
  11.750   1.0884   0.02109   0.01489   0.0200   0.0360   0.7971
  12.000   1.1017   0.02186   0.01574   0.0210   0.0354   0.8077
  12.250   1.1142   0.02268   0.01664   0.0220   0.0346   0.8185
  12.500   1.1257   0.02359   0.01762   0.0230   0.0340   0.8309
  12.750   1.1364   0.02456   0.01865   0.0241   0.0328   0.8456
  13.000   1.1458   0.02558   0.01977   0.0252   0.0321   0.8640
  13.500   1.1721   0.02786   0.02234   0.0255   0.0302   0.9476
  14.500   1.2285   0.03301   0.02766   0.0244   0.0275   1.0000
  14.750   1.2371   0.03453   0.02921   0.0247   0.0265   1.0000
  15.000   1.2451   0.03613   0.03084   0.0250   0.0257   1.0000
  15.250   1.2530   0.03779   0.03254   0.0251   0.0251   1.0000
  15.500   1.2619   0.03943   0.03422   0.0252   0.0243   1.0000
  15.750   1.2701   0.04115   0.03599   0.0252   0.0235   1.0000
  16.000   1.2776   0.04296   0.03784   0.0252   0.0228   1.0000
  16.250   1.2838   0.04495   0.03985   0.0251   0.0217   1.0000
  16.500   1.2893   0.04705   0.04198   0.0249   0.0207   1.0000
  16.750   1.2954   0.04913   0.04410   0.0247   0.0197   1.0000
  17.000   1.3006   0.05134   0.04637   0.0244   0.0190   1.0000
  17.250   1.3037   0.05380   0.04885   0.0240   0.0174   1.0000
  17.500   1.3068   0.05633   0.05142   0.0235   0.0161   1.0000
  17.750   1.3082   0.05910   0.05423   0.0229   0.0148   1.0000
  18.000   1.3089   0.06200   0.05717   0.0222   0.0138   1.0000
  18.250   1.3100   0.06491   0.06013   0.0214   0.0128   1.0000
  18.500   1.3087   0.06818   0.06346   0.0204   0.0119   1.0000
  18.750   1.3072   0.07156   0.06689   0.0193   0.0112   1.0000
  19.000   1.3056   0.07500   0.07040   0.0182   0.0105   1.0000
  19.250   1.3034   0.07859   0.07405   0.0168   0.0099   1.0000
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