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NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(3)-618 (naca633618-il)
Reynolds number: 500,000
Max Cl/Cd: 102.82 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633618-il-500000-n5.txt
Download as CSV file: xf-naca633618-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.7984   0.12008   0.11659  -0.0532   1.0000   0.0156
 -19.500  -0.8188   0.11255   0.10894  -0.0573   1.0000   0.0158
 -19.250  -0.8369   0.10558   0.10185  -0.0611   1.0000   0.0159
 -19.000  -0.8529   0.09914   0.09530  -0.0645   1.0000   0.0161
 -18.750  -0.8673   0.09309   0.08914  -0.0678   1.0000   0.0162
 -18.500  -0.8805   0.08737   0.08330  -0.0708   1.0000   0.0163
 -18.250  -0.8905   0.08230   0.07813  -0.0734   1.0000   0.0165
 -18.000  -0.8992   0.07750   0.07321  -0.0759   1.0000   0.0166
 -17.750  -0.9078   0.07284   0.06847  -0.0783   1.0000   0.0168
 -17.500  -0.9153   0.06847   0.06403  -0.0805   1.0000   0.0171
 -17.250  -0.9198   0.06461   0.06009  -0.0823   1.0000   0.0173
 -17.000  -0.9227   0.06108   0.05649  -0.0839   1.0000   0.0175
 -16.750  -0.9246   0.05780   0.05314  -0.0853   1.0000   0.0179
 -16.500  -0.9252   0.05476   0.05002  -0.0865   1.0000   0.0181
 -16.250  -0.9245   0.05197   0.04716  -0.0875   1.0000   0.0185
 -16.000  -0.9235   0.04933   0.04444  -0.0884   1.0000   0.0189
 -15.750  -0.9212   0.04690   0.04193  -0.0890   1.0000   0.0193
 -15.500  -0.9181   0.04467   0.03964  -0.0895   1.0000   0.0197
 -15.250  -0.9160   0.04244   0.03737  -0.0898   1.0000   0.0201
 -15.000  -0.9132   0.04039   0.03527  -0.0900   1.0000   0.0204
 -14.750  -0.9083   0.03864   0.03348  -0.0899   1.0000   0.0211
 -14.500  -0.9033   0.03697   0.03177  -0.0897   1.0000   0.0216
 -14.250  -0.8990   0.03537   0.03011  -0.0893   1.0000   0.0222
 -14.000  -0.8820   0.03366   0.02833  -0.0907   0.9845   0.0230
 -13.750  -0.8554   0.03180   0.02643  -0.0947   0.9665   0.0237
 -13.500  -0.8186   0.03019   0.02475  -0.1000   0.9535   0.0248
 -13.250  -0.7780   0.02868   0.02312  -0.1058   0.9399   0.0261
 -12.750  -0.7112   0.02596   0.02018  -0.1142   0.9034   0.0281
 -12.500  -0.6933   0.02502   0.01911  -0.1147   0.8844   0.0291
 -12.250  -0.6791   0.02416   0.01813  -0.1144   0.8687   0.0300
 -12.000  -0.6660   0.02334   0.01718  -0.1137   0.8550   0.0307
 -11.750  -0.6566   0.02233   0.01611  -0.1128   0.8428   0.0314
 -11.250  -0.6333   0.02070   0.01433  -0.1108   0.8216   0.0330
 -11.000  -0.6204   0.02000   0.01354  -0.1097   0.8125   0.0339
 -10.750  -0.6077   0.01930   0.01277  -0.1086   0.8038   0.0347
 -10.500  -0.5955   0.01866   0.01204  -0.1073   0.7953   0.0355
 -10.250  -0.5883   0.01794   0.01127  -0.1053   0.7874   0.0363
 -10.000  -0.5762   0.01734   0.01062  -0.1040   0.7796   0.0372
  -9.750  -0.5590   0.01684   0.01005  -0.1033   0.7727   0.0382
  -9.500  -0.5393   0.01641   0.00956  -0.1027   0.7658   0.0395
  -9.250  -0.5184   0.01603   0.00909  -0.1021   0.7592   0.0405
  -9.000  -0.4983   0.01554   0.00858  -0.1016   0.7534   0.0419
  -8.750  -0.4759   0.01515   0.00816  -0.1013   0.7470   0.0435
  -8.500  -0.4526   0.01481   0.00775  -0.1009   0.7406   0.0451
  -8.250  -0.4287   0.01447   0.00736  -0.1007   0.7350   0.0467
  -8.000  -0.4047   0.01409   0.00696  -0.1006   0.7291   0.0486
  -7.750  -0.3798   0.01377   0.00660  -0.1005   0.7232   0.0507
  -7.500  -0.3543   0.01350   0.00626  -0.1004   0.7177   0.0529
  -7.250  -0.3286   0.01316   0.00592  -0.1005   0.7119   0.0562
  -7.000  -0.3024   0.01289   0.00562  -0.1005   0.7061   0.0603
  -6.750  -0.2762   0.01260   0.00531  -0.1006   0.7010   0.0660
  -6.500  -0.2493   0.01229   0.00502  -0.1008   0.6956   0.0734
  -6.250  -0.2223   0.01200   0.00474  -0.1010   0.6898   0.0838
  -6.000  -0.1953   0.01172   0.00447  -0.1012   0.6845   0.0979
  -5.750  -0.1679   0.01138   0.00421  -0.1016   0.6797   0.1179
  -5.500  -0.1401   0.01106   0.00396  -0.1020   0.6743   0.1415
  -5.250  -0.1123   0.01073   0.00371  -0.1024   0.6689   0.1677
  -5.000  -0.0843   0.01039   0.00345  -0.1029   0.6638   0.2010
  -4.750  -0.0557   0.00998   0.00321  -0.1036   0.6589   0.2457
  -4.500  -0.0269   0.00958   0.00298  -0.1042   0.6538   0.2953
  -4.250   0.0021   0.00927   0.00280  -0.1049   0.6488   0.3440
  -4.000   0.0315   0.00908   0.00270  -0.1054   0.6440   0.3801
  -3.750   0.0611   0.00895   0.00263  -0.1060   0.6388   0.4104
  -3.500   0.0906   0.00885   0.00260  -0.1064   0.6339   0.4389
  -3.250   0.1199   0.00883   0.00257  -0.1068   0.6294   0.4582
  -3.000   0.1496   0.00880   0.00254  -0.1072   0.6250   0.4707
  -2.750   0.1791   0.00879   0.00252  -0.1075   0.6199   0.4805
  -2.500   0.2084   0.00880   0.00250  -0.1078   0.6148   0.4894
  -2.250   0.2377   0.00882   0.00249  -0.1081   0.6104   0.5004
  -2.000   0.2673   0.00882   0.00250  -0.1085   0.6062   0.5084
  -1.750   0.2967   0.00883   0.00249  -0.1088   0.6016   0.5147
  -1.500   0.3260   0.00886   0.00248  -0.1091   0.5971   0.5204
  -1.250   0.3550   0.00889   0.00249  -0.1094   0.5927   0.5255
  -1.000   0.3845   0.00890   0.00251  -0.1097   0.5882   0.5312
  -0.750   0.4138   0.00893   0.00252  -0.1101   0.5835   0.5369
  -0.500   0.4429   0.00898   0.00254  -0.1103   0.5793   0.5420
  -0.250   0.4718   0.00902   0.00257  -0.1106   0.5754   0.5468
   0.000   0.5012   0.00905   0.00261  -0.1109   0.5714   0.5518
   0.250   0.5304   0.00909   0.00264  -0.1112   0.5669   0.5568
   0.500   0.5592   0.00915   0.00268  -0.1115   0.5623   0.5610
   0.750   0.5878   0.00921   0.00274  -0.1117   0.5582   0.5653
   1.000   0.6170   0.00925   0.00280  -0.1120   0.5545   0.5702
   1.250   0.6460   0.00930   0.00286  -0.1123   0.5502   0.5753
   1.500   0.6747   0.00937   0.00293  -0.1125   0.5457   0.5798
   1.750   0.7030   0.00945   0.00301  -0.1126   0.5414   0.5843
   2.000   0.7318   0.00951   0.00309  -0.1129   0.5374   0.5891
   2.250   0.7604   0.00958   0.00318  -0.1131   0.5327   0.5939
   2.500   0.7887   0.00966   0.00326  -0.1133   0.5278   0.5985
   2.750   0.8165   0.00977   0.00337  -0.1134   0.5233   0.6036
   3.000   0.8451   0.00983   0.00348  -0.1136   0.5190   0.6092
   3.250   0.8734   0.00992   0.00359  -0.1138   0.5143   0.6143
   3.500   0.9011   0.01002   0.00371  -0.1138   0.5095   0.6189
   3.750   0.9286   0.01014   0.00384  -0.1139   0.5051   0.6240
   4.000   0.9567   0.01022   0.00398  -0.1140   0.5004   0.6294
   4.250   0.9843   0.01033   0.00411  -0.1141   0.4950   0.6349
   4.500   1.0109   0.01047   0.00427  -0.1140   0.4893   0.6403
   4.750   1.0382   0.01057   0.00443  -0.1140   0.4825   0.6462
   5.000   1.0643   0.01072   0.00458  -0.1138   0.4743   0.6518
   5.250   1.0906   0.01087   0.00475  -0.1136   0.4668   0.6570
   5.500   1.1165   0.01101   0.00494  -0.1134   0.4589   0.6628
   5.750   1.1418   0.01119   0.00513  -0.1131   0.4506   0.6692
   6.000   1.1666   0.01139   0.00533  -0.1127   0.4405   0.6751
   6.250   1.1907   0.01158   0.00556  -0.1122   0.4290   0.6808
   6.500   1.2133   0.01185   0.00581  -0.1114   0.4150   0.6872
   7.000   1.2518   0.01260   0.00645  -0.1088   0.3734   0.6997
   7.250   1.2659   0.01315   0.00690  -0.1067   0.3442   0.7064
   7.500   1.2754   0.01378   0.00740  -0.1038   0.3171   0.7126
   7.750   1.2840   0.01440   0.00795  -0.1007   0.2943   0.7193
   8.000   1.2908   0.01517   0.00864  -0.0976   0.2709   0.7268
   8.250   1.2971   0.01601   0.00939  -0.0946   0.2471   0.7337
   8.500   1.3022   0.01695   0.01026  -0.0915   0.2254   0.7410
   8.750   1.3079   0.01795   0.01119  -0.0888   0.2055   0.7486
   9.000   1.3134   0.01900   0.01222  -0.0862   0.1872   0.7563
   9.250   1.3190   0.02015   0.01332  -0.0839   0.1706   0.7649
   9.500   1.3243   0.02137   0.01452  -0.0816   0.1553   0.7731
   9.750   1.3291   0.02270   0.01583  -0.0795   0.1404   0.7820
  10.000   1.3341   0.02408   0.01720  -0.0775   0.1271   0.7907
  10.250   1.3378   0.02563   0.01873  -0.0756   0.1133   0.8009
  10.500   1.3414   0.02724   0.02033  -0.0738   0.1009   0.8113
  10.750   1.3454   0.02890   0.02198  -0.0722   0.0901   0.8228
  11.000   1.3491   0.03060   0.02370  -0.0706   0.0803   0.8351
  11.250   1.3527   0.03234   0.02547  -0.0691   0.0719   0.8490
  11.500   1.3558   0.03413   0.02731  -0.0676   0.0648   0.8664
  11.750   1.3574   0.03593   0.02917  -0.0659   0.0583   0.8924
  12.250   1.3655   0.03954   0.03289  -0.0637   0.0486   1.0000
  12.500   1.3704   0.04169   0.03504  -0.0631   0.0445   1.0000
  12.750   1.3768   0.04372   0.03711  -0.0627   0.0413   1.0000
  13.000   1.3826   0.04588   0.03929  -0.0623   0.0387   1.0000
  13.250   1.3890   0.04804   0.04149  -0.0620   0.0366   1.0000
  13.500   1.3943   0.05034   0.04381  -0.0617   0.0346   1.0000
  13.750   1.4007   0.05258   0.04611  -0.0616   0.0332   1.0000
  14.000   1.4068   0.05489   0.04847  -0.0615   0.0319   1.0000
  14.250   1.4123   0.05731   0.05094  -0.0615   0.0307   1.0000
  14.500   1.4163   0.05997   0.05364  -0.0615   0.0297   1.0000
  14.750   1.4224   0.06239   0.05613  -0.0617   0.0289   1.0000
  15.000   1.4276   0.06499   0.05880  -0.0619   0.0279   1.0000
  15.250   1.4324   0.06768   0.06154  -0.0621   0.0271   1.0000
  15.500   1.4358   0.07058   0.06451  -0.0625   0.0263   1.0000
  15.750   1.4381   0.07367   0.06764  -0.0629   0.0256   1.0000
  16.000   1.4430   0.07647   0.07052  -0.0634   0.0249   1.0000
  16.250   1.4469   0.07943   0.07356  -0.0639   0.0242   1.0000
  16.500   1.4503   0.08248   0.07668  -0.0645   0.0235   1.0000
  16.750   1.4524   0.08578   0.08004  -0.0653   0.0228   1.0000
  17.000   1.4539   0.08919   0.08351  -0.0661   0.0221   1.0000
  17.250   1.4554   0.09263   0.08702  -0.0670   0.0216   1.0000
  17.500   1.4589   0.09581   0.09029  -0.0679   0.0209   1.0000
  17.750   1.4607   0.09929   0.09386  -0.0689   0.0203   1.0000
  18.000   1.4624   0.10280   0.09744  -0.0700   0.0197   1.0000
  18.250   1.4626   0.10659   0.10130  -0.0713   0.0192   1.0000
  18.500   1.4619   0.11053   0.10530  -0.0727   0.0187   1.0000
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