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NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(3)-618 (naca633618-il)
Reynolds number: 200,000
Max Cl/Cd: 73.37 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633618-il-200000-n5.txt
Download as CSV file: xf-naca633618-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(3)-618                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.6652   0.10265   0.09802  -0.0671   1.0000   0.0263
 -17.000  -0.7052   0.09128   0.08638  -0.0739   1.0000   0.0264
 -16.750  -0.7357   0.08237   0.07720  -0.0793   1.0000   0.0266
 -16.500  -0.7434   0.07779   0.07254  -0.0818   1.0000   0.0269
 -16.250  -0.7495   0.07362   0.06829  -0.0839   1.0000   0.0271
 -16.000  -0.7526   0.07003   0.06465  -0.0857   1.0000   0.0275
 -15.750  -0.7578   0.06626   0.06080  -0.0875   1.0000   0.0279
 -15.500  -0.7630   0.06265   0.05709  -0.0892   1.0000   0.0283
 -15.250  -0.7680   0.05923   0.05354  -0.0905   1.0000   0.0287
 -15.000  -0.7730   0.05598   0.05016  -0.0917   1.0000   0.0294
 -14.750  -0.7783   0.05287   0.04688  -0.0925   1.0000   0.0301
 -14.500  -0.7827   0.05002   0.04383  -0.0929   1.0000   0.0307
 -14.250  -0.7807   0.04803   0.04183  -0.0929   1.0000   0.0312
 -14.000  -0.7782   0.04620   0.03998  -0.0927   1.0000   0.0317
 -13.750  -0.7763   0.04442   0.03817  -0.0923   1.0000   0.0322
 -13.500  -0.7749   0.04271   0.03641  -0.0917   1.0000   0.0329
 -13.250  -0.7750   0.04109   0.03472  -0.0908   1.0000   0.0337
 -12.750  -0.7509   0.03745   0.03085  -0.0929   0.9834   0.0357
 -12.500  -0.7275   0.03582   0.02920  -0.0957   0.9718   0.0368
 -12.250  -0.7022   0.03422   0.02751  -0.0987   0.9605   0.0381
 -12.000  -0.6753   0.03267   0.02581  -0.1016   0.9492   0.0397
 -11.750  -0.6466   0.03120   0.02424  -0.1046   0.9387   0.0412
 -11.500  -0.6189   0.02989   0.02287  -0.1074   0.9265   0.0427
 -11.250  -0.5923   0.02870   0.02157  -0.1096   0.9143   0.0444
 -11.000  -0.5668   0.02764   0.02033  -0.1112   0.9025   0.0461
 -10.750  -0.5471   0.02657   0.01924  -0.1119   0.8899   0.0475
 -10.500  -0.5302   0.02567   0.01828  -0.1119   0.8777   0.0491
 -10.250  -0.5133   0.02484   0.01734  -0.1117   0.8669   0.0509
 -10.000  -0.4986   0.02409   0.01647  -0.1108   0.8558   0.0523
  -9.750  -0.4870   0.02322   0.01556  -0.1097   0.8460   0.0539
  -9.500  -0.4762   0.02248   0.01477  -0.1083   0.8361   0.0554
  -9.250  -0.4656   0.02184   0.01406  -0.1067   0.8274   0.0571
  -9.000  -0.4517   0.02122   0.01334  -0.1056   0.8187   0.0590
  -8.750  -0.4366   0.02054   0.01258  -0.1046   0.8116   0.0608
  -8.500  -0.4210   0.01991   0.01193  -0.1037   0.8035   0.0630
  -8.250  -0.4023   0.01938   0.01131  -0.1030   0.7966   0.0659
  -8.000  -0.3832   0.01883   0.01071  -0.1023   0.7899   0.0691
  -7.750  -0.3636   0.01828   0.01013  -0.1018   0.7828   0.0729
  -7.500  -0.3417   0.01780   0.00958  -0.1014   0.7769   0.0778
  -7.250  -0.3201   0.01728   0.00906  -0.1010   0.7706   0.0847
  -7.000  -0.2977   0.01678   0.00856  -0.1008   0.7639   0.0941
  -6.750  -0.2742   0.01629   0.00807  -0.1007   0.7583   0.1080
  -6.500  -0.2502   0.01582   0.00763  -0.1006   0.7526   0.1266
  -6.250  -0.2261   0.01530   0.00720  -0.1007   0.7463   0.1524
  -6.000  -0.2013   0.01475   0.00675  -0.1009   0.7407   0.1858
  -5.750  -0.1761   0.01415   0.00632  -0.1013   0.7354   0.2319
  -5.500  -0.1504   0.01359   0.00597  -0.1017   0.7293   0.2861
  -5.250  -0.1236   0.01315   0.00573  -0.1021   0.7238   0.3424
  -5.000  -0.0954   0.01293   0.00559  -0.1024   0.7192   0.3883
  -4.750  -0.0675   0.01282   0.00555  -0.1026   0.7130   0.4208
  -4.500  -0.0390   0.01277   0.00549  -0.1029   0.7075   0.4479
  -4.250  -0.0101   0.01276   0.00544  -0.1031   0.7028   0.4695
  -4.000   0.0187   0.01277   0.00542  -0.1033   0.6975   0.4865
  -3.750   0.0471   0.01279   0.00542  -0.1034   0.6917   0.4999
  -3.500   0.0758   0.01280   0.00538  -0.1035   0.6867   0.5100
  -3.250   0.1053   0.01283   0.00529  -0.1038   0.6824   0.5212
  -3.000   0.1331   0.01287   0.00537  -0.1038   0.6768   0.5313
  -2.750   0.1622   0.01290   0.00532  -0.1041   0.6715   0.5413
  -2.500   0.1907   0.01291   0.00529  -0.1041   0.6668   0.5469
  -2.250   0.2196   0.01293   0.00526  -0.1043   0.6621   0.5534
  -2.000   0.2485   0.01294   0.00522  -0.1046   0.6569   0.5599
  -1.750   0.2768   0.01296   0.00523  -0.1047   0.6521   0.5648
  -1.500   0.3059   0.01299   0.00519  -0.1049   0.6479   0.5707
  -1.250   0.3349   0.01302   0.00517  -0.1052   0.6428   0.5769
  -1.000   0.3629   0.01304   0.00521  -0.1053   0.6376   0.5816
  -0.750   0.3914   0.01307   0.00522  -0.1054   0.6332   0.5864
  -0.500   0.4207   0.01312   0.00520  -0.1058   0.6294   0.5920
  -0.250   0.4495   0.01317   0.00523  -0.1061   0.6246   0.5975
   0.000   0.4772   0.01320   0.00531  -0.1061   0.6195   0.6014
   0.250   0.5057   0.01325   0.00534  -0.1062   0.6150   0.6062
   0.500   0.5349   0.01332   0.00534  -0.1065   0.6112   0.6120
   0.750   0.5632   0.01339   0.00544  -0.1068   0.6066   0.6172
   1.000   0.5908   0.01346   0.00556  -0.1068   0.6019   0.6214
   1.250   0.6191   0.01353   0.00563  -0.1069   0.5976   0.6263
   1.500   0.6482   0.01361   0.00566  -0.1072   0.5937   0.6319
   1.750   0.6759   0.01370   0.00580  -0.1073   0.5890   0.6372
   2.000   0.7032   0.01380   0.00596  -0.1073   0.5844   0.6421
   2.250   0.7313   0.01389   0.00607  -0.1074   0.5801   0.6476
   2.500   0.7603   0.01400   0.00612  -0.1078   0.5762   0.6534
   2.750   0.7872   0.01411   0.00632  -0.1077   0.5715   0.6581
   3.000   0.8141   0.01423   0.00651  -0.1076   0.5666   0.6634
   3.250   0.8419   0.01434   0.00663  -0.1077   0.5620   0.6698
   3.750   0.8961   0.01460   0.00699  -0.1076   0.5528   0.6806
   4.000   0.9228   0.01474   0.00719  -0.1076   0.5477   0.6866
   4.250   0.9507   0.01487   0.00733  -0.1077   0.5432   0.6933
   4.500   0.9772   0.01502   0.00753  -0.1075   0.5388   0.6986
   4.750   1.0027   0.01518   0.00780  -0.1072   0.5334   0.7050
   5.000   1.0294   0.01534   0.00800  -0.1072   0.5281   0.7118
   5.250   1.0559   0.01548   0.00816  -0.1070   0.5234   0.7173
   5.500   1.0799   0.01565   0.00847  -0.1065   0.5169   0.7240
   5.750   1.1052   0.01581   0.00867  -0.1061   0.5101   0.7313
   6.000   1.1291   0.01596   0.00888  -0.1055   0.5031   0.7371
   6.250   1.1521   0.01613   0.00914  -0.1048   0.4946   0.7442
   6.500   1.1763   0.01631   0.00934  -0.1042   0.4873   0.7513
   6.750   1.1974   0.01650   0.00966  -0.1032   0.4785   0.7582
   7.000   1.2201   0.01671   0.00988  -0.1024   0.4699   0.7660
   7.250   1.2398   0.01692   0.01022  -0.1011   0.4601   0.7729
   7.500   1.2597   0.01717   0.01052  -0.0999   0.4506   0.7810
   7.750   1.2774   0.01744   0.01083  -0.0983   0.4389   0.7890
   8.000   1.2915   0.01775   0.01120  -0.0961   0.4240   0.7975
   8.250   1.3004   0.01813   0.01157  -0.0931   0.4061   0.8066
   8.500   1.3061   0.01864   0.01207  -0.0896   0.3858   0.8165
   8.750   1.3111   0.01929   0.01270  -0.0863   0.3634   0.8272
   9.000   1.3142   0.02012   0.01349  -0.0829   0.3415   0.8393
   9.250   1.3147   0.02110   0.01443  -0.0794   0.3210   0.8525
   9.500   1.3145   0.02220   0.01551  -0.0760   0.3004   0.8680
   9.750   1.3120   0.02347   0.01676  -0.0726   0.2802   0.8882
  10.000   1.3073   0.02482   0.01810  -0.0690   0.2609   0.9232
  10.250   1.3039   0.02645   0.01968  -0.0664   0.2412   1.0000
  10.500   1.3048   0.02839   0.02155  -0.0648   0.2208   1.0000
  10.750   1.3048   0.03049   0.02357  -0.0633   0.2015   1.0000
  11.000   1.3049   0.03267   0.02568  -0.0620   0.1842   1.0000
  11.250   1.3048   0.03496   0.02791  -0.0608   0.1679   1.0000
  11.500   1.3051   0.03728   0.03019  -0.0598   0.1533   1.0000
  11.750   1.3059   0.03966   0.03253  -0.0590   0.1399   1.0000
  12.000   1.3070   0.04209   0.03495  -0.0583   0.1277   1.0000
  12.250   1.3080   0.04462   0.03746  -0.0577   0.1162   1.0000
  12.500   1.3090   0.04724   0.04006  -0.0572   0.1059   1.0000
  12.750   1.3097   0.04997   0.04277  -0.0568   0.0961   1.0000
  13.000   1.3117   0.05263   0.04543  -0.0566   0.0872   1.0000
  13.250   1.3136   0.05539   0.04820  -0.0565   0.0793   1.0000
  13.500   1.3151   0.05825   0.05108  -0.0564   0.0729   1.0000
  13.750   1.3165   0.06119   0.05404  -0.0565   0.0674   1.0000
  14.000   1.3192   0.06405   0.05695  -0.0566   0.0626   1.0000
  14.500   1.3229   0.07014   0.06312  -0.0572   0.0550   1.0000
  14.750   1.3233   0.07345   0.06646  -0.0577   0.0520   1.0000
  15.000   1.3260   0.07652   0.06961  -0.0581   0.0492   1.0000
  15.250   1.3277   0.07977   0.07292  -0.0587   0.0467   1.0000
  15.500   1.3278   0.08330   0.07648  -0.0594   0.0447   1.0000
  15.750   1.3315   0.08638   0.07966  -0.0601   0.0425   1.0000
  16.000   1.3327   0.08984   0.08317  -0.0610   0.0407   1.0000
  16.250   1.3320   0.09361   0.08697  -0.0620   0.0393   1.0000
  16.500   1.3353   0.09685   0.09034  -0.0628   0.0378   1.0000
  16.750   1.3374   0.10029   0.09386  -0.0639   0.0365   1.0000
  17.000   1.3384   0.10392   0.09757  -0.0650   0.0354   1.0000
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