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NACA 63(2)-615 (naca632615-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(2)-615 (naca632615-il)
Reynolds number: 500,000
Max Cl/Cd: 104.5 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca632615-il-500000-n5.txt
Download as CSV file: xf-naca632615-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)-615                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.7272   0.10321   0.10014  -0.0555   1.0000   0.0124
 -16.750  -0.7732   0.09020   0.08693  -0.0628   1.0000   0.0123
 -16.500  -0.8023   0.08090   0.07748  -0.0683   1.0000   0.0123
 -16.250  -0.8275   0.07257   0.06899  -0.0734   1.0000   0.0124
 -16.000  -0.8454   0.06594   0.06219  -0.0774   1.0000   0.0124
 -15.750  -0.8588   0.06043   0.05656  -0.0807   1.0000   0.0123
 -15.500  -0.8700   0.05552   0.05150  -0.0834   1.0000   0.0125
 -15.250  -0.8800   0.05117   0.04704  -0.0857   1.0000   0.0126
 -15.000  -0.8870   0.04742   0.04318  -0.0875   1.0000   0.0126
 -14.750  -0.8926   0.04405   0.03974  -0.0889   1.0000   0.0128
 -14.500  -0.8957   0.04112   0.03673  -0.0898   1.0000   0.0129
 -14.250  -0.8967   0.03861   0.03414  -0.0904   1.0000   0.0131
 -14.000  -0.8971   0.03632   0.03177  -0.0906   1.0000   0.0133
 -13.750  -0.8939   0.03452   0.02992  -0.0905   1.0000   0.0136
 -13.500  -0.8942   0.03263   0.02795  -0.0899   1.0000   0.0137
 -13.250  -0.8932   0.03110   0.02636  -0.0889   1.0000   0.0139
 -13.000  -0.8833   0.02940   0.02457  -0.0896   0.9978   0.0143
 -12.750  -0.8640   0.02770   0.02276  -0.0918   0.9867   0.0147
 -12.500  -0.8422   0.02610   0.02103  -0.0942   0.9764   0.0150
 -12.250  -0.8165   0.02456   0.01935  -0.0972   0.9661   0.0154
 -12.000  -0.7873   0.02313   0.01786  -0.1006   0.9558   0.0159
 -11.750  -0.7547   0.02202   0.01666  -0.1039   0.9451   0.0164
 -11.500  -0.7239   0.02101   0.01554  -0.1066   0.9321   0.0170
 -11.250  -0.6971   0.02016   0.01455  -0.1082   0.9180   0.0177
 -11.000  -0.6743   0.01947   0.01372  -0.1085   0.9045   0.0183
 -10.750  -0.6542   0.01878   0.01294  -0.1083   0.8918   0.0189
 -10.250  -0.6119   0.01778   0.01178  -0.1076   0.8696   0.0203
 -10.000  -0.5903   0.01729   0.01118  -0.1072   0.8602   0.0210
  -9.750  -0.5682   0.01681   0.01060  -0.1068   0.8506   0.0218
  -9.500  -0.5460   0.01630   0.01001  -0.1064   0.8420   0.0225
  -9.250  -0.5227   0.01588   0.00954  -0.1061   0.8335   0.0234
  -9.000  -0.4985   0.01552   0.00911  -0.1059   0.8260   0.0245
  -8.750  -0.4739   0.01517   0.00867  -0.1058   0.8181   0.0256
  -8.500  -0.4494   0.01478   0.00819  -0.1056   0.8110   0.0266
  -8.250  -0.4247   0.01436   0.00774  -0.1055   0.8038   0.0277
  -8.000  -0.3992   0.01404   0.00735  -0.1054   0.7968   0.0289
  -7.750  -0.3732   0.01373   0.00698  -0.1054   0.7901   0.0303
  -7.500  -0.3471   0.01342   0.00659  -0.1054   0.7832   0.0315
  -7.250  -0.3212   0.01304   0.00618  -0.1054   0.7768   0.0331
  -7.000  -0.2943   0.01275   0.00586  -0.1056   0.7701   0.0347
  -6.750  -0.2674   0.01251   0.00553  -0.1056   0.7636   0.0363
  -6.500  -0.2403   0.01220   0.00518  -0.1058   0.7575   0.0381
  -6.250  -0.2130   0.01191   0.00487  -0.1060   0.7509   0.0401
  -6.000  -0.1854   0.01169   0.00459  -0.1061   0.7448   0.0424
  -5.750  -0.1575   0.01145   0.00431  -0.1063   0.7387   0.0449
  -5.500  -0.1297   0.01121   0.00405  -0.1065   0.7322   0.0483
  -5.250  -0.1016   0.01102   0.00381  -0.1067   0.7264   0.0524
  -5.000  -0.0733   0.01078   0.00358  -0.1071   0.7203   0.0587
  -4.750  -0.0450   0.01055   0.00336  -0.1074   0.7141   0.0688
  -4.500  -0.0167   0.01031   0.00315  -0.1077   0.7084   0.0854
  -4.250   0.0120   0.01003   0.00295  -0.1082   0.7022   0.1111
  -4.000   0.0406   0.00971   0.00274  -0.1087   0.6964   0.1493
  -3.750   0.0696   0.00934   0.00254  -0.1093   0.6908   0.2015
  -3.500   0.0989   0.00891   0.00234  -0.1101   0.6847   0.2711
  -3.250   0.1282   0.00855   0.00217  -0.1108   0.6787   0.3404
  -3.000   0.1577   0.00831   0.00210  -0.1115   0.6734   0.3980
  -2.750   0.1872   0.00820   0.00205  -0.1119   0.6675   0.4323
  -2.500   0.2163   0.00813   0.00203  -0.1122   0.6617   0.4669
  -2.250   0.2457   0.00807   0.00204  -0.1126   0.6561   0.4980
  -2.000   0.2749   0.00806   0.00204  -0.1129   0.6504   0.5158
  -1.750   0.3038   0.00807   0.00203  -0.1131   0.6450   0.5293
  -1.500   0.3330   0.00808   0.00204  -0.1134   0.6395   0.5428
  -1.250   0.3621   0.00810   0.00204  -0.1136   0.6335   0.5525
  -1.000   0.3909   0.00813   0.00204  -0.1138   0.6282   0.5598
  -0.750   0.4200   0.00815   0.00206  -0.1141   0.6231   0.5674
  -0.500   0.4490   0.00818   0.00208  -0.1143   0.6173   0.5744
  -0.250   0.4777   0.00822   0.00210  -0.1145   0.6118   0.5809
   0.000   0.5067   0.00826   0.00213  -0.1147   0.6067   0.5876
   0.250   0.5356   0.00830   0.00217  -0.1149   0.6012   0.5934
   0.500   0.5641   0.00835   0.00221  -0.1151   0.5958   0.5997
   0.750   0.5930   0.00841   0.00226  -0.1153   0.5906   0.6061
   1.000   0.6217   0.00845   0.00232  -0.1155   0.5851   0.6117
   1.250   0.6501   0.00852   0.00238  -0.1157   0.5796   0.6178
   1.500   0.6788   0.00859   0.00245  -0.1158   0.5743   0.6244
   1.750   0.7073   0.00864   0.00253  -0.1160   0.5685   0.6305
   2.000   0.7354   0.00873   0.00262  -0.1161   0.5627   0.6368
   2.500   0.7921   0.00887   0.00281  -0.1164   0.5511   0.6493
   2.750   0.8200   0.00898   0.00291  -0.1164   0.5454   0.6563
   3.000   0.8483   0.00905   0.00303  -0.1166   0.5396   0.6625
   3.250   0.8762   0.00914   0.00315  -0.1166   0.5331   0.6689
   3.500   0.9037   0.00926   0.00328  -0.1167   0.5259   0.6760
   3.750   0.9311   0.00936   0.00341  -0.1166   0.5164   0.6826
   4.000   0.9582   0.00949   0.00355  -0.1165   0.5068   0.6896
   4.250   0.9850   0.00964   0.00370  -0.1164   0.4972   0.6963
   4.500   1.0118   0.00976   0.00387  -0.1163   0.4865   0.7032
   4.750   1.0377   0.00995   0.00404  -0.1160   0.4714   0.7107
   5.000   1.0628   0.01017   0.00423  -0.1156   0.4534   0.7173
   5.250   1.0867   0.01045   0.00446  -0.1151   0.4320   0.7246
   5.500   1.1096   0.01081   0.00472  -0.1143   0.4024   0.7319
   5.750   1.1303   0.01130   0.00507  -0.1132   0.3668   0.7393
   6.000   1.1509   0.01181   0.00546  -0.1122   0.3337   0.7469
   6.250   1.1693   0.01244   0.00594  -0.1108   0.2957   0.7543
   6.500   1.1859   0.01318   0.00649  -0.1092   0.2556   0.7626
   6.750   1.2014   0.01394   0.00709  -0.1074   0.2173   0.7703
   7.000   1.2170   0.01467   0.00768  -0.1056   0.1860   0.7789
   7.250   1.2313   0.01538   0.00829  -0.1037   0.1578   0.7874
   7.500   1.2431   0.01613   0.00891  -0.1013   0.1318   0.7971
   7.750   1.2519   0.01688   0.00958  -0.0983   0.1090   0.8068
   8.000   1.2612   0.01765   0.01029  -0.0956   0.0894   0.8175
   8.500   1.2793   0.01925   0.01183  -0.0904   0.0615   0.8423
   8.750   1.2886   0.02006   0.01265  -0.0879   0.0522   0.8567
   9.000   1.2972   0.02089   0.01352  -0.0855   0.0453   0.8744
   9.250   1.3053   0.02167   0.01436  -0.0829   0.0406   0.8994
   9.500   1.3109   0.02237   0.01517  -0.0800   0.0377   0.9765
   9.750   1.3237   0.02333   0.01615  -0.0787   0.0349   1.0000
  10.000   1.3353   0.02441   0.01725  -0.0774   0.0324   1.0000
  10.250   1.3479   0.02545   0.01833  -0.0762   0.0307   1.0000
  10.500   1.3595   0.02660   0.01951  -0.0750   0.0291   1.0000
  10.750   1.3694   0.02791   0.02085  -0.0738   0.0276   1.0000
  11.000   1.3808   0.02914   0.02213  -0.0728   0.0264   1.0000
  11.250   1.3916   0.03045   0.02350  -0.0718   0.0252   1.0000
  11.500   1.4011   0.03190   0.02500  -0.0708   0.0240   1.0000
  11.750   1.4089   0.03354   0.02667  -0.0698   0.0228   1.0000
  12.000   1.4187   0.03504   0.02824  -0.0690   0.0219   1.0000
  12.250   1.4280   0.03663   0.02989  -0.0682   0.0208   1.0000
  12.500   1.4359   0.03839   0.03170  -0.0675   0.0198   1.0000
  12.750   1.4419   0.04035   0.03371  -0.0667   0.0189   1.0000
  13.000   1.4499   0.04218   0.03561  -0.0662   0.0181   1.0000
  13.250   1.4571   0.04414   0.03764  -0.0656   0.0173   1.0000
  13.500   1.4635   0.04622   0.03979  -0.0652   0.0165   1.0000
  13.750   1.4688   0.04847   0.04209  -0.0648   0.0159   1.0000
  14.000   1.4732   0.05090   0.04458  -0.0645   0.0153   1.0000
  14.250   1.4785   0.05329   0.04707  -0.0643   0.0148   1.0000
  14.500   1.4834   0.05579   0.04965  -0.0642   0.0143   1.0000
  14.750   1.4875   0.05843   0.05236  -0.0642   0.0139   1.0000
  15.000   1.4909   0.06121   0.05523  -0.0643   0.0134   1.0000
  15.250   1.4936   0.06416   0.05825  -0.0646   0.0131   1.0000
  15.500   1.4953   0.06731   0.06146  -0.0649   0.0128   1.0000
  15.750   1.4959   0.07064   0.06488  -0.0653   0.0125   1.0000
  16.000   1.4974   0.07393   0.06828  -0.0659   0.0123   1.0000
  16.250   1.4981   0.07742   0.07187  -0.0665   0.0121   1.0000
  16.500   1.4984   0.08103   0.07558  -0.0673   0.0119   1.0000
  16.750   1.4982   0.08475   0.07940  -0.0682   0.0117   1.0000
  17.000   1.4975   0.08862   0.08338  -0.0693   0.0115   1.0000
  17.250   1.4962   0.09265   0.08750  -0.0704   0.0113   1.0000
  17.500   1.4946   0.09679   0.09175  -0.0718   0.0112   1.0000
  17.750   1.4927   0.10104   0.09609  -0.0732   0.0110   1.0000
  18.000   1.4903   0.10540   0.10055  -0.0748   0.0109   1.0000
  18.250   1.4872   0.10992   0.10519  -0.0765   0.0108   1.0000
  18.500   1.4837   0.11461   0.10997  -0.0785   0.0106   1.0000
  18.750   1.4796   0.11943   0.11489  -0.0806   0.0105   1.0000
  19.000   1.4749   0.12440   0.11996  -0.0829   0.0104   1.0000
  19.250   1.4697   0.12949   0.12514  -0.0853   0.0103   1.0000
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