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NACA 63(2)-615 (naca632615-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(2)-615 (naca632615-il)
Reynolds number: 500,000
Max Cl/Cd: 112.16 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca632615-il-500000.txt
Download as CSV file: xf-naca632615-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.6398   0.07428   0.07144  -0.0739   1.0000   0.0194
 -14.000  -0.6825   0.06347   0.06040  -0.0816   1.0000   0.0193
 -13.750  -0.7111   0.05628   0.05303  -0.0861   1.0000   0.0191
 -13.500  -0.7340   0.05065   0.04722  -0.0892   1.0000   0.0192
 -13.250  -0.7556   0.04582   0.04219  -0.0911   1.0000   0.0192
 -13.000  -0.7711   0.04226   0.03845  -0.0917   1.0000   0.0193
 -12.750  -0.7883   0.03911   0.03513  -0.0911   1.0000   0.0195
 -12.500  -0.8045   0.03695   0.03284  -0.0890   1.0000   0.0196
 -12.250  -0.8190   0.03523   0.03100  -0.0868   0.9987   0.0197
 -12.000  -0.8040   0.03173   0.02717  -0.0916   0.9904   0.0202
 -11.750  -0.7771   0.02981   0.02521  -0.0950   0.9848   0.0207
 -11.500  -0.7482   0.02857   0.02391  -0.0980   0.9787   0.0213
 -11.250  -0.7193   0.02713   0.02234  -0.1007   0.9732   0.0220
 -11.000  -0.6890   0.02547   0.02048  -0.1034   0.9689   0.0227
 -10.750  -0.6612   0.02401   0.01881  -0.1053   0.9611   0.0235
 -10.500  -0.6296   0.02224   0.01684  -0.1078   0.9563   0.0243
 -10.250  -0.6018   0.02121   0.01580  -0.1090   0.9467   0.0251
 -10.000  -0.5706   0.02051   0.01503  -0.1108   0.9388   0.0261
  -9.750  -0.5437   0.01980   0.01420  -0.1114   0.9283   0.0272
  -9.500  -0.5185   0.01928   0.01351  -0.1115   0.9176   0.0282
  -9.250  -0.4957   0.01808   0.01223  -0.1115   0.9082   0.0294
  -9.000  -0.4736   0.01754   0.01166  -0.1110   0.8975   0.0304
  -8.750  -0.4497   0.01704   0.01108  -0.1107   0.8886   0.0316
  -8.500  -0.4261   0.01659   0.01052  -0.1103   0.8794   0.0330
  -8.250  -0.4036   0.01586   0.00970  -0.1098   0.8710   0.0344
  -8.000  -0.3804   0.01533   0.00916  -0.1095   0.8625   0.0360
  -7.750  -0.3555   0.01493   0.00869  -0.1093   0.8549   0.0378
  -7.500  -0.3304   0.01457   0.00825  -0.1090   0.8469   0.0394
  -7.250  -0.3069   0.01385   0.00747  -0.1088   0.8398   0.0413
  -7.000  -0.2816   0.01347   0.00708  -0.1087   0.8320   0.0436
  -6.750  -0.2552   0.01316   0.00668  -0.1086   0.8254   0.0458
  -6.500  -0.2296   0.01267   0.00614  -0.1086   0.8181   0.0481
  -6.250  -0.2033   0.01225   0.00571  -0.1087   0.8112   0.0512
  -6.000  -0.1761   0.01199   0.00538  -0.1088   0.8048   0.0543
  -5.750  -0.1492   0.01155   0.00492  -0.1089   0.7978   0.0582
  -5.500  -0.1214   0.01128   0.00459  -0.1091   0.7916   0.0632
  -5.250  -0.0938   0.01091   0.00423  -0.1094   0.7849   0.0706
  -5.000  -0.0658   0.01055   0.00390  -0.1097   0.7785   0.0853
  -4.750  -0.0378   0.01001   0.00354  -0.1102   0.7725   0.1327
  -4.500  -0.0096   0.00929   0.00318  -0.1111   0.7657   0.2230
  -4.250   0.0193   0.00858   0.00288  -0.1122   0.7598   0.3409
  -4.000   0.0486   0.00825   0.00277  -0.1128   0.7538   0.4163
  -3.750   0.0778   0.00813   0.00271  -0.1131   0.7473   0.4541
  -3.500   0.1070   0.00809   0.00266  -0.1134   0.7415   0.4806
  -3.250   0.1361   0.00806   0.00263  -0.1137   0.7353   0.5007
  -3.000   0.1653   0.00804   0.00260  -0.1139   0.7291   0.5162
  -2.750   0.1944   0.00807   0.00257  -0.1141   0.7234   0.5306
  -2.500   0.2234   0.00806   0.00259  -0.1143   0.7170   0.5479
  -2.250   0.2524   0.00811   0.00261  -0.1145   0.7111   0.5651
  -2.000   0.2815   0.00815   0.00262  -0.1147   0.7055   0.5767
  -1.750   0.3105   0.00817   0.00263  -0.1149   0.6991   0.5873
  -1.500   0.3393   0.00821   0.00265  -0.1150   0.6934   0.5976
  -1.250   0.3684   0.00826   0.00266  -0.1152   0.6876   0.6062
  -1.000   0.3972   0.00826   0.00267  -0.1154   0.6816   0.6131
  -0.750   0.4261   0.00832   0.00267  -0.1156   0.6761   0.6205
  -0.500   0.4551   0.00834   0.00269  -0.1158   0.6701   0.6275
  -0.250   0.4838   0.00836   0.00272  -0.1160   0.6642   0.6341
   0.000   0.5129   0.00845   0.00273  -0.1162   0.6589   0.6412
   0.250   0.5414   0.00844   0.00278  -0.1164   0.6530   0.6474
   0.500   0.5701   0.00849   0.00282  -0.1165   0.6471   0.6541
   0.750   0.5991   0.00858   0.00286  -0.1168   0.6419   0.6608
   1.000   0.6275   0.00859   0.00293  -0.1169   0.6360   0.6670
   1.250   0.6562   0.00866   0.00298  -0.1171   0.6302   0.6741
   1.500   0.6847   0.00874   0.00305  -0.1172   0.6248   0.6804
   1.750   0.7130   0.00877   0.00314  -0.1173   0.6187   0.6871
   2.000   0.7417   0.00886   0.00320  -0.1175   0.6130   0.6945
   2.250   0.7698   0.00893   0.00331  -0.1176   0.6074   0.7007
   2.500   0.7981   0.00899   0.00340  -0.1177   0.6012   0.7079
   2.750   0.8262   0.00908   0.00348  -0.1178   0.5956   0.7146
   3.000   0.8542   0.00916   0.00362  -0.1178   0.5898   0.7218
   3.250   0.8823   0.00923   0.00372  -0.1179   0.5834   0.7293
   3.500   0.9098   0.00935   0.00383  -0.1179   0.5770   0.7359
   3.750   0.9374   0.00940   0.00395  -0.1179   0.5690   0.7438
   4.250   0.9917   0.00958   0.00419  -0.1177   0.5535   0.7586
   4.500   1.0183   0.00971   0.00432  -0.1175   0.5454   0.7657
   4.750   1.0450   0.00977   0.00446  -0.1173   0.5356   0.7736
   5.000   1.0710   0.00988   0.00459  -0.1170   0.5248   0.7814
   5.250   1.0962   0.01002   0.00473  -0.1165   0.5119   0.7894
   5.500   1.1212   0.01017   0.00488  -0.1160   0.4972   0.7975
   5.750   1.1464   0.01030   0.00506  -0.1155   0.4838   0.8059
   6.000   1.1714   0.01046   0.00526  -0.1151   0.4706   0.8144
   6.250   1.1956   0.01066   0.00548  -0.1145   0.4555   0.8233
   6.500   1.2187   0.01089   0.00572  -0.1137   0.4382   0.8322
   6.750   1.2407   0.01121   0.00599  -0.1128   0.4177   0.8423
   7.000   1.2607   0.01155   0.00631  -0.1114   0.3906   0.8519
   7.250   1.2771   0.01211   0.00674  -0.1096   0.3540   0.8629
   7.500   1.2893   0.01288   0.00730  -0.1071   0.3090   0.8756
   8.000   1.3004   0.01468   0.00870  -0.0999   0.2184   0.9088
   8.250   1.2959   0.01538   0.00929  -0.0942   0.1865   0.9461
   8.500   1.3013   0.01640   0.01012  -0.0911   0.1502   1.0000
   8.750   1.3074   0.01758   0.01110  -0.0885   0.1188   1.0000
   9.000   1.3131   0.01880   0.01216  -0.0859   0.0937   1.0000
   9.250   1.3188   0.02006   0.01331  -0.0835   0.0744   1.0000
   9.500   1.3255   0.02133   0.01450  -0.0813   0.0610   1.0000
   9.750   1.3336   0.02257   0.01570  -0.0794   0.0530   1.0000
  10.000   1.3405   0.02394   0.01705  -0.0776   0.0476   1.0000
  10.250   1.3511   0.02511   0.01827  -0.0762   0.0442   1.0000
  10.500   1.3575   0.02663   0.01979  -0.0745   0.0412   1.0000
  10.750   1.3667   0.02800   0.02122  -0.0732   0.0389   1.0000
  11.000   1.3759   0.02941   0.02268  -0.0720   0.0368   1.0000
  11.250   1.3806   0.03124   0.02453  -0.0706   0.0348   1.0000
  11.500   1.3870   0.03298   0.02634  -0.0694   0.0331   1.0000
  11.750   1.3958   0.03457   0.02799  -0.0685   0.0314   1.0000
  12.000   1.4014   0.03648   0.02994  -0.0676   0.0298   1.0000
  12.250   1.4003   0.03909   0.03260  -0.0664   0.0283   1.0000
  12.500   1.4086   0.04088   0.03447  -0.0657   0.0272   1.0000
  12.750   1.4147   0.04292   0.03658  -0.0651   0.0259   1.0000
  13.000   1.4188   0.04523   0.03894  -0.0645   0.0249   1.0000
  13.250   1.4159   0.04834   0.04209  -0.0639   0.0240   1.0000
  13.500   1.4193   0.05090   0.04474  -0.0635   0.0232   1.0000
  13.750   1.4248   0.05327   0.04722  -0.0632   0.0224   1.0000
  14.000   1.4293   0.05583   0.04985  -0.0631   0.0217   1.0000
  14.250   1.4329   0.05852   0.05260  -0.0630   0.0211   1.0000
  14.500   1.4352   0.06144   0.05558  -0.0631   0.0205   1.0000
  14.750   1.4341   0.06482   0.05901  -0.0632   0.0200   1.0000
  15.000   1.4338   0.06816   0.06241  -0.0633   0.0195   1.0000
  15.250   1.4386   0.07097   0.06534  -0.0636   0.0191   1.0000
  15.500   1.4425   0.07393   0.06841  -0.0640   0.0186   1.0000
  15.750   1.4460   0.07699   0.07156  -0.0644   0.0182   1.0000
  16.000   1.4490   0.08017   0.07483  -0.0650   0.0178   1.0000
  16.250   1.4518   0.08341   0.07814  -0.0657   0.0174   1.0000
  16.500   1.4540   0.08675   0.08155  -0.0665   0.0171   1.0000
  16.750   1.4557   0.09021   0.08507  -0.0673   0.0168   1.0000
  17.000   1.4569   0.09368   0.08859  -0.0681   0.0165   1.0000
  17.250   1.4580   0.09701   0.09197  -0.0685   0.0161   1.0000
  17.500   1.4592   0.10071   0.09581  -0.0696   0.0160   1.0000
  17.750   1.4600   0.10449   0.09972  -0.0709   0.0158   1.0000
  18.000   1.4607   0.10830   0.10366  -0.0722   0.0156   1.0000
  18.250   1.4605   0.11231   0.10779  -0.0737   0.0154   1.0000
  18.500   1.4601   0.11636   0.11197  -0.0753   0.0152   1.0000
  18.750   1.4593   0.12048   0.11622  -0.0770   0.0150   1.0000
  19.000   1.4578   0.12480   0.12066  -0.0790   0.0149   1.0000
  19.250   1.4557   0.12923   0.12521  -0.0811   0.0147   1.0000
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