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NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(3)-018 (naca633018-il)
Reynolds number: 500,000
Max Cl/Cd: 72.96 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633018-il-500000.txt
Download as CSV file: xf-naca633018-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1912   0.10230   0.09809  -0.0077   1.0000   0.0263
 -19.500  -1.1928   0.09821   0.09394  -0.0099   1.0000   0.0271
 -19.250  -1.1929   0.09439   0.09005  -0.0118   1.0000   0.0281
 -19.000  -1.1924   0.09070   0.08626  -0.0137   1.0000   0.0290
 -18.750  -1.1913   0.08711   0.08254  -0.0154   1.0000   0.0298
 -18.500  -1.1914   0.08358   0.07892  -0.0169   1.0000   0.0307
 -18.250  -1.1915   0.08018   0.07549  -0.0182   1.0000   0.0316
 -18.000  -1.1894   0.07697   0.07224  -0.0196   1.0000   0.0324
 -17.750  -1.1862   0.07397   0.06918  -0.0209   1.0000   0.0332
 -17.500  -1.1821   0.07115   0.06629  -0.0220   1.0000   0.0341
 -17.250  -1.1777   0.06840   0.06345  -0.0230   1.0000   0.0350
 -17.000  -1.1726   0.06577   0.06071  -0.0240   1.0000   0.0357
 -16.750  -1.1668   0.06323   0.05806  -0.0250   1.0000   0.0362
 -16.500  -1.1644   0.06071   0.05555  -0.0252   1.0000   0.0375
 -16.250  -1.1593   0.05833   0.05314  -0.0258   1.0000   0.0385
 -16.000  -1.1530   0.05609   0.05085  -0.0264   1.0000   0.0392
 -15.750  -1.1459   0.05397   0.04868  -0.0268   1.0000   0.0401
 -15.500  -1.1382   0.05197   0.04662  -0.0272   1.0000   0.0409
 -15.250  -1.1298   0.05003   0.04461  -0.0276   1.0000   0.0419
 -15.000  -1.1209   0.04822   0.04272  -0.0278   1.0000   0.0426
 -14.750  -1.1109   0.04648   0.04090  -0.0281   1.0000   0.0433
 -14.500  -1.1058   0.04455   0.03894  -0.0276   1.0000   0.0444
 -14.250  -1.1004   0.04259   0.03697  -0.0275   1.0000   0.0455
 -14.000  -1.0923   0.04087   0.03522  -0.0274   1.0000   0.0464
 -13.750  -1.0828   0.03929   0.03361  -0.0273   1.0000   0.0475
 -13.500  -1.0727   0.03781   0.03209  -0.0272   1.0000   0.0488
 -13.250  -1.0621   0.03640   0.03064  -0.0270   1.0000   0.0498
 -13.000  -1.0496   0.03516   0.02932  -0.0269   1.0000   0.0510
 -12.750  -1.0386   0.03383   0.02794  -0.0265   1.0000   0.0518
 -12.500  -1.0359   0.03194   0.02604  -0.0257   1.0000   0.0534
 -12.250  -1.0292   0.03034   0.02442  -0.0251   1.0000   0.0545
 -12.000  -1.0193   0.02900   0.02308  -0.0246   1.0000   0.0561
 -11.750  -1.0092   0.02770   0.02174  -0.0240   1.0000   0.0572
 -11.500  -0.9983   0.02647   0.02048  -0.0234   1.0000   0.0584
 -11.250  -0.9866   0.02530   0.01928  -0.0229   1.0000   0.0595
 -11.000  -0.9732   0.02425   0.01818  -0.0225   1.0000   0.0606
 -10.750  -0.9525   0.02267   0.01654  -0.0246   0.9474   0.0628
 -10.250  -0.9321   0.02060   0.01425  -0.0225   0.8862   0.0673
 -10.000  -0.9235   0.01979   0.01334  -0.0206   0.8699   0.0694
  -9.750  -0.9131   0.01910   0.01252  -0.0188   0.8564   0.0714
  -9.500  -0.9094   0.01811   0.01148  -0.0162   0.8439   0.0752
  -9.250  -0.9026   0.01730   0.01064  -0.0139   0.8324   0.0796
  -9.000  -0.8943   0.01665   0.00993  -0.0114   0.8227   0.0848
  -8.750  -0.8904   0.01598   0.00926  -0.0080   0.8129   0.0935
  -8.500  -0.8804   0.01532   0.00865  -0.0057   0.8043   0.1083
  -8.250  -0.8695   0.01457   0.00800  -0.0035   0.7963   0.1316
  -8.000  -0.8560   0.01382   0.00738  -0.0018   0.7886   0.1611
  -7.750  -0.8410   0.01308   0.00679  -0.0002   0.7812   0.1956
  -7.500  -0.8252   0.01232   0.00622   0.0012   0.7743   0.2362
  -7.250  -0.8075   0.01159   0.00569   0.0024   0.7670   0.2802
  -7.000  -0.7882   0.01099   0.00524   0.0034   0.7610   0.3243
  -6.750  -0.7661   0.01050   0.00492   0.0040   0.7540   0.3631
  -6.500  -0.7418   0.01020   0.00467   0.0044   0.7476   0.3928
  -6.250  -0.7159   0.01001   0.00449   0.0046   0.7417   0.4154
  -6.000  -0.6889   0.00985   0.00434   0.0046   0.7353   0.4325
  -5.750  -0.6620   0.00973   0.00419   0.0047   0.7295   0.4462
  -5.500  -0.6344   0.00963   0.00407   0.0047   0.7236   0.4580
  -5.250  -0.6064   0.00954   0.00395   0.0046   0.7173   0.4690
  -5.000  -0.5785   0.00950   0.00384   0.0045   0.7118   0.4794
  -4.750  -0.5503   0.00942   0.00376   0.0044   0.7061   0.4883
  -4.500  -0.5220   0.00938   0.00370   0.0043   0.7002   0.5005
  -4.250  -0.4940   0.00940   0.00365   0.0042   0.6949   0.5123
  -4.000  -0.4655   0.00933   0.00360   0.0041   0.6891   0.5202
  -3.750  -0.4366   0.00930   0.00353   0.0039   0.6833   0.5273
  -3.500  -0.4082   0.00928   0.00347   0.0038   0.6784   0.5348
  -3.250  -0.3792   0.00928   0.00345   0.0035   0.6729   0.5425
  -3.000  -0.3502   0.00923   0.00337   0.0033   0.6673   0.5483
  -2.750  -0.3214   0.00920   0.00331   0.0031   0.6622   0.5532
  -2.500  -0.2922   0.00919   0.00327   0.0028   0.6571   0.5587
  -2.250  -0.2630   0.00915   0.00320   0.0025   0.6517   0.5639
  -2.000  -0.2340   0.00911   0.00316   0.0023   0.6467   0.5688
  -1.750  -0.2048   0.00912   0.00313   0.0020   0.6417   0.5739
  -1.500  -0.1754   0.00911   0.00308   0.0017   0.6363   0.5789
  -1.250  -0.1464   0.00905   0.00305   0.0015   0.6316   0.5834
  -1.000  -0.1172   0.00907   0.00303   0.0012   0.6269   0.5882
  -0.750  -0.0877   0.00905   0.00301   0.0009   0.6216   0.5933
  -0.500  -0.0585   0.00901   0.00298   0.0006   0.6167   0.5978
  -0.250  -0.0294   0.00903   0.00298   0.0003   0.6123   0.6023
   0.000   0.0000   0.00903   0.00299   0.0000   0.6074   0.6074
   0.250   0.0294   0.00903   0.00298  -0.0003   0.6023   0.6123
   0.500   0.0585   0.00901   0.00298  -0.0006   0.5978   0.6167
   0.750   0.0877   0.00905   0.00301  -0.0009   0.5933   0.6217
   1.000   0.1172   0.00907   0.00303  -0.0012   0.5882   0.6269
   1.250   0.1464   0.00905   0.00305  -0.0015   0.5834   0.6316
   1.500   0.1754   0.00911   0.00308  -0.0017   0.5789   0.6363
   1.750   0.2048   0.00912   0.00313  -0.0020   0.5740   0.6417
   2.000   0.2340   0.00911   0.00316  -0.0023   0.5687   0.6467
   2.250   0.2630   0.00915   0.00320  -0.0025   0.5639   0.6517
   2.500   0.2922   0.00919   0.00327  -0.0028   0.5587   0.6571
   2.750   0.3214   0.00920   0.00331  -0.0031   0.5532   0.6622
   3.000   0.3502   0.00923   0.00337  -0.0033   0.5482   0.6673
   3.250   0.3792   0.00928   0.00345  -0.0035   0.5425   0.6729
   3.500   0.4082   0.00928   0.00347  -0.0038   0.5348   0.6784
   3.750   0.4366   0.00930   0.00353  -0.0039   0.5273   0.6834
   4.000   0.4655   0.00933   0.00360  -0.0041   0.5203   0.6891
   4.250   0.4940   0.00940   0.00365  -0.0042   0.5123   0.6949
   4.500   0.5220   0.00938   0.00370  -0.0043   0.5005   0.7002
   4.750   0.5503   0.00942   0.00376  -0.0044   0.4882   0.7061
   5.000   0.5785   0.00950   0.00384  -0.0045   0.4794   0.7118
   5.250   0.6065   0.00954   0.00396  -0.0046   0.4692   0.7173
   5.500   0.6344   0.00963   0.00407  -0.0047   0.4580   0.7236
   5.750   0.6620   0.00973   0.00419  -0.0047   0.4462   0.7295
   6.000   0.6890   0.00985   0.00434  -0.0046   0.4325   0.7353
   6.250   0.7159   0.01001   0.00449  -0.0046   0.4155   0.7417
   6.500   0.7418   0.01020   0.00467  -0.0044   0.3928   0.7476
   6.750   0.7661   0.01050   0.00492  -0.0040   0.3629   0.7541
   7.000   0.7882   0.01100   0.00524  -0.0034   0.3242   0.7610
   7.250   0.8075   0.01160   0.00569  -0.0024   0.2800   0.7670
   7.500   0.8252   0.01233   0.00622  -0.0012   0.2360   0.7743
   7.750   0.8410   0.01309   0.00679   0.0002   0.1953   0.7812
   8.000   0.8561   0.01382   0.00738   0.0017   0.1612   0.7886
   8.250   0.8695   0.01457   0.00800   0.0035   0.1315   0.7963
   8.500   0.8805   0.01532   0.00865   0.0057   0.1081   0.8042
   8.750   0.8905   0.01598   0.00927   0.0080   0.0934   0.8130
   9.000   0.8947   0.01664   0.00992   0.0113   0.0849   0.8227
   9.250   0.9027   0.01730   0.01064   0.0138   0.0795   0.8324
   9.500   0.9097   0.01811   0.01147   0.0162   0.0752   0.8438
   9.750   0.9134   0.01909   0.01251   0.0187   0.0714   0.8564
  10.000   0.9238   0.01979   0.01333   0.0205   0.0695   0.8697
  10.250   0.9326   0.02058   0.01423   0.0224   0.0673   0.8861
  10.500   0.9395   0.02147   0.01522   0.0244   0.0653   0.9086
  10.750   0.9531   0.02263   0.01650   0.0245   0.0629   0.9471
  11.000   0.9741   0.02421   0.01813   0.0224   0.0606   1.0000
  11.250   0.9869   0.02530   0.01927   0.0228   0.0596   1.0000
  11.500   0.9990   0.02644   0.02046   0.0234   0.0584   1.0000
  11.750   1.0100   0.02767   0.02171   0.0239   0.0572   1.0000
  12.000   1.0206   0.02893   0.02300   0.0244   0.0559   1.0000
  12.250   1.0299   0.03031   0.02441   0.0250   0.0550   1.0000
  12.500   1.0367   0.03190   0.02599   0.0256   0.0533   1.0000
  12.750   1.0399   0.03376   0.02788   0.0264   0.0520   1.0000
  13.000   1.0512   0.03507   0.02924   0.0267   0.0509   1.0000
  13.250   1.0623   0.03642   0.03065   0.0270   0.0501   1.0000
  13.500   1.0739   0.03774   0.03202   0.0271   0.0487   1.0000
  13.750   1.0839   0.03923   0.03355   0.0272   0.0475   1.0000
  14.000   1.0932   0.04083   0.03518   0.0273   0.0464   1.0000
  14.250   1.1012   0.04255   0.03692   0.0274   0.0454   1.0000
  14.500   1.1072   0.04446   0.03885   0.0275   0.0444   1.0000
  14.750   1.1124   0.04641   0.04082   0.0279   0.0432   1.0000
  15.000   1.1220   0.04813   0.04262   0.0277   0.0427   1.0000
  15.250   1.1311   0.04994   0.04452   0.0274   0.0419   1.0000
  15.500   1.1394   0.05188   0.04653   0.0271   0.0410   1.0000
  15.750   1.1473   0.05388   0.04859   0.0267   0.0401   1.0000
  16.000   1.1546   0.05600   0.05076   0.0262   0.0391   1.0000
  16.250   1.1608   0.05826   0.05306   0.0256   0.0383   1.0000
  16.500   1.1659   0.06062   0.05545   0.0251   0.0375   1.0000
  16.750   1.1686   0.06310   0.05793   0.0248   0.0363   1.0000
  17.000   1.1745   0.06567   0.06062   0.0238   0.0356   1.0000
  17.250   1.1795   0.06826   0.06331   0.0230   0.0350   1.0000
  17.500   1.1839   0.07103   0.06617   0.0219   0.0341   1.0000
  17.750   1.1883   0.07385   0.06905   0.0207   0.0331   1.0000
  18.000   1.1915   0.07685   0.07211   0.0194   0.0323   1.0000
  18.250   1.1935   0.08004   0.07536   0.0181   0.0315   1.0000
  18.500   1.1930   0.08346   0.07878   0.0168   0.0306   1.0000
  18.750   1.1935   0.08694   0.08237   0.0152   0.0298   1.0000
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